PLATE L COMPARATIVE MAGNITUDES OF THE PLANETS, 1, MERCURY. 5. URANUS. 2, MARS. 6, NEPTUNE. 3, VENUS 7, SATURN. 4, EARTH 8. JUPITER. THE ELEMENTS THEORETICAL AND DESCRIPTIVE ASTRONOMY, the tt BY CHARLES J. WHITE, A.M., / 1 ASSISTANT PROFESSOR OF MATHEMATICS IN HARVARD COLLEQB FOURTH EDITION, REVISED. PHILADELPHIA: CLAXTON, EEMSEN & HAFFELFINGER. 1880. NA/S Entered according to Act of Congress, in the year 1869, by CHARLES J. WHITE, ir> the Clerk's Office of the District Court of the United States for the District, of Maryland. PREFACE TO THE THIRD EDITION. first edition of this work was published in 1869, to meet the requirements of the students of the United States Naval Academy. In preparing it, I endeavored to present the main facts and principles of Astronomy in a form adapted to the elementary course of instruction in that science which is com- monly given at colleges and the higher grades of academies. I selected those topics which seemed to me to be the most important and the most interesting, and arranged them in the order which experience had led me to believe to be the best. The third edi- tion of the book is issued with no change in the general plan, and with only those changes which the advance of astronomical knowledge in the last six years renders necessary. In the descriptive portions of the work, I have endeavored to give the latest information upon every topic which is introduced. On not a few points the opinions of competent observers are by no means the same ; and on these points I have endeavored to give, as far as possible, the various opinions which now exist. The distances and the dimensions of the heavenly bodies are given to correspond with the value of the solar parallax which is at present adopted in the American Ephemeris ; the recent theories upon the connection of comets and meteors, the principles of spectroscopic observation, and the conclusions concerning the IV PREFACE. constitution and the movements of the heavenly bodies which such observation induces, are given, it is hoped, in sufficient detail. No clear conception of the processes Dy which most of the fundamental truths of Astronomy have been established can be attained without some knowledge of Mathematics. I have en- deavored, however, to confine the theoretic discussions within the limits of such moderate mathematical knowledge as may fairly be expected in those readers for whom the treatise is intended. Certain definitions and formulae, with which the student may possibly not be familiar, will be found in the Appendix ; and, with this aid, I believe that every portion of the work can be read without difficulty. In the preparation of the work, many authorities have been consulted ; the principal ones being Chauvenet's Manual of Spherical and Practical Astronomy, and Chambers's Descriptive Astronomy. The treatise has been used as a text-book in the United States Naval Academy, the Massachusetts Institute of Technology, Harvard College, and other institutions ; and I am indebted to officers of these institutions for many valuable sug- gestions as to errors and improvements. I trust that this new edition will be found to be free from mistakes, and that it will be useful, not only to the class of students for whom it is especially prepared, but to others who may wish to know the general prin- ciples and the present state of the science of Astronomy. Harvard College, Cambridge, Mass., 1875. CONTENTS. The Greek Alphabet PAGE ix CHAPTER I. GENERAL PHENOMENA OF THE HEAVENS. DEFINITIONS. THE CELESTIAL SPHERE. The heavenly bodies. Astronomy. Form of the earth. Diurnal mo- tions of the heavenly bodies. Eight, parallel, and oblique spheres. Definitions. Theorems. The astronomical triangle. Spherical co- ordinates. Vanishing lines and circles. Spherical projections 11 CHAPTER II. ASTRONOMICAL INSTRUMENTS. ERRORS. The clock : its error and rate. The chronograph. The transit instru- ment: its construction, adjustment, and use. The meridian circle. The reading microscope. Fixed points. The mural circle. The altitude and azimuth instrument. Method of equal altitudes. The equatorial. The sextant. The artificial horizon. The vernier. Other astronomical instruments. Classes of errors 28 CHAPTER III. REFRACTION. PARALLAX. DIP OF THE HORIZON. General laws of refraction. Astronomical refraction. Geocentric and heliocentric parallax. The dip of the horizon 51 CHAPTER IV. THE EARTH. ITS SIZE, FORM, AND ROTATION. Measurement of arcs of the meridian by triangulation. Spheroidal form of the earth. Its dimensions. Its volume, density, and weight. Rotation of the earth. Change of weight in different latitudes. Centrifugal force. The trade-winds. Foucault's pendu- lum experiment. Linear velocity of rotation 59 Vi CONTENTS, CHAPTEK V. LATITUDE AND LONGITUDE. Four methods of finding the latitude of a place. Latitude at sea. Reduction of the latitude. Longitude. Greenwich time by chro- nometers, celestial phenomena, and lunar distances. Difference of longitude by electric and star signals. Longitude at sea. Compa- rison of the local times of different meridians PAGE 72 CHAPTEK VI. TIIE SUN. THE EARTH'S ORBIT. THE SEASONS. TWILIGHT. THE ZODIACAL LIGHT. The eciiptic. Distance of the sun from the earth determined by transits of Venus. Magnitude of the sun. The earth's orbit about the sun. The seasons. Twilight. Rotation of the sun, and its constitution. The zodiacal light 83 CHAPTER VII. SIDEREAL AND SOLAR TIME. EQUATION OF TIME. THE CALENDAR. The sidereal and the solar year. Relation of sidereal and solar time. The equation of the centre. The equation of time. Astronomical and civil time. The calendar 100 CHAPTER VIII. UNIVERSAL GRAVITATION. PERTURBATIONS IN THE EARTH'S ORBIT. ABERRATION. The law of universal gravitation. The mass of the sun. The earth's motion at perihelion and aphelion. Kepler's laws. Precession. Nutation. Change in the obliquity of the ecliptic. Advance of the line of apsides. Diurnal and annual aberration. Velocity of light. Aberration a proof of the earth's revolution 107 CHAPTER IX. THE MOON. The orbit of the moon, and perturbations in it. Variation of the moon's^meridian zenith distance. Distance, size, and mass of the moon. Augmentation of the semi-diameter. The phases of the moon. Sidereal and synodical periods. Retardation of the moon. The harvest moon. Rotation ; librations and other perturbations. Tlu- lunar cycie. General description of the moon 120 CONTENTS. Vll CHAPTEK X. LUNAR AND SOLAR ECLIPSES. OCCULTATIONS. Lunar eclipses. The earth's shadow. Lunar ecliptic limits. Solar eclipses. The moon's shadow. Solar ecliptic limits. Cycle and number of eclipses. Occultations. Longitude by solar eclipses and occultations PAGE 135 CHAPTEK XI. THE TIDES. Cause of the tides. Effect of the moon's change in declination. General laws. Influence of the sun. Priming and lagging of tides. The establishment of a port. Cotidal lines. Height of tides. Tides in bays, rivers, &c. Four daily tides. Other phenomena 146 CHAPTER XII. THE PLANETS AND THE PLANETOIDS. THE NEBULAR HYPOTHESIS. Apparent motions of the planets. Heliocentric parallax. Orbits of the planets. Inferior planets. Direct and retrograde motion. Sta- tionary points. Evening and morning stars. Elements of a planet's orbit. Heliocentric longitude of the node. Inclination of the orbit. Periodic time. Mercury. Venus. Transits of Venus. Superior planets: their periodic times and distances. Mars. The minor planets. Bode's law. Jupiter: its belts, satellites, and mass. Saturn and its rings. Disappearance of the rings. Uranus. Neptune. The nebular hypothesis 155 CHAPTEE XIII. COMETS AND METEORIC BODIES. General description of comets. The tail. Elements of a comet's orbit. Number of comets and their orbits. Periodic times. Motion in their orbits. Mass and density. Periodic comets. Encke's comet. Winnecke's or Pons's comet. Brorsen's comet. Biela's comet. D' Arrest's comet. Faye's comet. Mechain's comet. Halley's comet. Remarkable comets of the present century. The great comet of 1811. The great comet of 1843. Donati's comet. The great comet of 18G1. Meteoric bodies. Shooting stars. The No- vember showers. Height and orbits of the meteors. Detonating meteors. Aerolites. Connection of comets and meteoric bodies 187 Viii CONTENTS. CHAPTEK XIV. THE FIXED STARS. NEBULA. MOTION OF THE SOLAR SYSTEM. REAL MOTIONS OF THE STARS. Proper motions of the fixed stars. Magnitudes. Constellations. Constitution of the stars. Distance of the stars. Bessel's differen- tial observations. Heal magnitudes of the stars. Variable and tem- porary stars. Double and binary stars. Colored stars. Clusters. Kesolvable and irresolvable nebulae. Annular, elliptic, spiral, and planetary nebulae. Nebulous stars. Double nebulae. The Ma- gellanic clouds. Variation of brightness in nebulre. The milky way. Number of the stars. Motion of the solar system in space. Real motions of stars detected with the spectroscope PAGE 213 APPENDIX. Mathematical definitions, theorems, and formulae 242 Kirkwood's law 247 Chronological history of astronomy 248 Sketch of the history of navigation 255 Table I. Elements of the planets, the sun, and the moon 256 II. The earth... 257 " III. The moon 257 " IV. Elements of the satellites 258 . " V. The minorplanets 259 " VI. Schwabe's observations of the solar spots 261 " VII. Elements of the periodic comets 261 " VIII. Transits of the inferior planets 262 " IX. Stars whose parallax has been determined 262 " X. The constellations 263 " XI. Examples of variable stars 266 " XII. Examples of binary stars 267 [NDEX .. 269 THE GKEEK ALPHABET. The following table of the small letters of this alphabet is given for the use of those readers who are unacquainted with the Greek language. a Alpha. V Nu. P Beta. 5 Xi. v Gamma. Omicron. $ Delta. 7t Pi. e Epsilon. P Rho. ? Zeta. (7 Sigma. n Eta. * Tau. $or Theta. U Upsllon. i Iota.
Fig. 9.
36 FIXED POINTS.
divisions, then will one revolution of the screw correspond to an
arc of 1' ; and if we further suppose that the head of the screw
is divided into 60 equal parts, then each division on the head
will correspond to an arc of V . In such a case, the complete
reading of the limb is obtained to the nearest second. By in-
creasing the power of the microscope, the fineness of the screw,
and the number of the graduations on the screw-head, the read-
ing of the limb may be obtained with far greater precision.
29. Fixed Points. The meridian circle, being also a transit
instrument, may be used as such; but the object for which it is
specially used is the measurement of arcs of the meridian. In
order to facilitate such measurement, certain fixed points of re-
ference are determined upon the vertical circle. The most im-
portant of these points are the horizontal point, by which is
meant the reading of the instrument when the axis of the tele-
scope lies in the plane of the horizon ; the polar point, which is
the reading of the instrument when the telescope is directed to
the elevated pole ; the zenith point, and the nadir point.
30. The Horizontal Point. As the surface of a fluid, when at
rest, is necessarily horizontal, and as, by the laws of Optics, the
angles of incidence and reflection are equal to each other, the
image of a star reflected in a basin of mercury will be depressed
below the horizon by an angle equal to the altitude of the star
at that instant. If, then, we take the reading of the vertical
circle when a star which is about to cross the meridian is on the
first vertical thread of the reticule, and then, depressing the
telescope, take the reading of the circle when the reflected image
of the star crosses the last vertical thread, and, by means of
small corrections, reduce these readings to what they would have
been, had both star and image been on the meridian when
the observations were made, the mean of these two reduced
readings will be the horizontal point. The horizontal point
having been thus determined, the zenith point and the nadir point,
being situated at intervals of 90 from it, are at once obtained.
Knowing the horizontal and the zenith point, we are able to
measure the meridian altitude or the meridian zenith distance
of any celestial body which comes above our horizon. And
further, as the latitude is equal to the altitude of the elevated
NADIR POINT.
37
Fig. 10.
pole, if tlie latitude of the place is accurately known, we can at
once obtain the polar point by applying the latitude to the
horizontal point.
31. Nadir Point. The nadir point may be independently
obtained in the following manner. Let the
telescope, represented in Fig. 10 by AJ3, be
directed vertically downwards towards a basin
of mercury, CD. The observer, placing his
eye at A, will see the cross-wires of the tele-
scope, and will see also the image of these
wires reflected into the telescope from the
mercury. By slowly moving the telescope,
the cross-wires and their reflected image may
be brought into exact coincidence, and the
reflected image will then disappear. The
line of sight of the telescope is now vertical,
and the reading of the vertical circle' will be
the nadir point, from which the other points can readily be found.
There is a variety of methods by which each of these points
can be obtained, without reference to any other; and by com-
paring the results which these different independent methods
give, the errors to which each result is liable may be very con-
siderably diminished.
32. Use of the Meridian Circle. The meridian circle may be
used in connection with the sidereal clock, to find the right
ascension and declination of any celestial body. The telescope
is directed towards the body as it crosses the meridian, and the
time of transit as shown by the clock, and the reading of the
vertical circle, are both taken. We have already seen how the
right ascension of the body is obtained from the clock time of
transit. The difference between the reading of the circle, which
we suppose to have been taken, and the polar point, is the polar
distance of the body, the complement of which is the declina-
tion. Or we may obtain the declination still more directly by
previously establishing the equinoctial point of the instrument,
the reading, that is to say, of the vertical circle when the tele-
scope lies in the plane of the equinoctial.*
* As the direction in which a star appears to lie is not, owing to refruc-
4
38 MURAL CIRCLE.
On the other hand, if we ma ke the same observations upon a
Btar whose right ascension and declination are known, we can
determine the latitude and the sidereal time of the place of
observation.
THE MURAL CIRCLE.
33. The mural circle is, in construction, adjustment, and use,
essentially a meridian circle. The only important difference
between the two instruments is in the manner in which they are
mounted. The horizontal axis of the mural circle, instead of
being supported at both extremities, is supported only at one,
which is let into a stone pier or wall. Owing to the lack of
symmetrical support, and also to the fact that the instrument
does not admit of reversal (which is an important element in the
adjustment of the meridian circle, and consists in lifting it out
of the Ys, and turning the horizontal axis end for end), the
mural circle can be regarded only as an inferior type of the
meridian circle.
THE ALTITUDE AND AZIMUTH INSTRUMENT.
34. The general principles on which the altitude and azimuth
instrument is constructed are seen
in Fig. 11. Through the centre of
a graduated circle, C'6", and per-
pendicular to its plane, is passed an
axis, A A. At right angles to this
axis is a second axis, one extremity
of which is represented by B. This
second axis carries the telescope, TT,
and also a second graduated circle,
(7(7, whose plane is perpendicular to
that of the circle C" C' '. The tele-
scope admits of being moved in the plane of each circle, and
tion and other causes, which will be explained in Chap. III., the direction
in which it really lies, certain small corrections must be applied to the
reading of the circle to obtain the reading which really corresponds to the
direction of the star.
ALTITUDE AND AZIMUTH INSTRUMENT. 39
microscopes or verniers are attached to the instrument, by means
of which arcs on either circle can be read.
If this instrument is so placed that the principal axis, AA,
lies in a vertical direction, we shall have an altitude and azimuth
instrument, sometimes called an altazimuth. The circle C'C f
will then lie in the plane of the horizon, and the axis AA, in-
definitely prolonged, will meet the surface of the celestial sphere
in the zenith and the nadir. The circle (7(7, as it is moved
with the telescope about the axis AA } will continually lie in a
vertical plane.
35. Fixed Points. Altitudes maybe measured on the vertical
circle, when we know the horizontal or the zenith point, the de-
termination of which has already been described in Arts. 30 and
31. In order to measure the azimuth of any celestial body, we
must, in like manner, establish some fixed point of reference on
the horizontal circle, as, for instance, the north or the south
point, by which is meant the reading of the horizontal circle
when the telescope lies in the plane of the meridian.
36. Method of Equal Altitudes. One of the most accurate
methods of obtaining the north or the
south point of the horizontal circle is
called the method of equal altitudes.
Let Fig. 12 represent the projection of
the celestial sphere on the plane of the
celestial horizon, NESW. Z is the
projection of the zenith, P of the pole,
and the arc AA' the projection of a
portion of the diurnal circle of affixed
star, which is supposed to have the
same altitude when it reaches A', west
of the meridian, which it had at A, east of the meridian.
Now, in the two triangles PAZ, PA'Z, we have PZ common,
PA' equal to PA (since the polar distance of a fixed star re-
mains constant), and ZA equal to ZA', by hypothesis ; the two
triangles are therefore equal in all their parts, and hence the
angles PZA and PZA' are equal. But these' two angles are the
azimuths of the star at the two positions A and A f . We may
40 EQUATORIAL.
say, then, in general, that equal, altitudes of a fixed star corre-
spond to equal angular distances from the meridian.
Now, let the telescope be directed to some fixed star east of the
meridian, and let the reading of the horizontal circle be taken.
When the star is at the same altitude, west of the meridian, let
the reading of the horizontal circle again be taken ; the mean of
these two readings is the reading of the horizontal circle when
the axis of the telescope lies in the plane of the meridian.
37. Use of the Altitude and Azimuth Instrument. This instru-
ment is chiefly used for the determination of the amount of re-
fraction corresponding to different altitudes. Refraction, as will
be seen in the next chapter, displaces every celestial body in a
vertical direction, making its apparent zenith distance less than
its true zenith distance. At the instant of taking the altitude
of a celestial body, the local sidereal time is noted, from which,
knowing the right ascension of the body, we can obtain its hour
angle from the theorem in Art. 9. We shall then have in the
astronomical triangle, PZA (Fig. 3), the hour angle ZPA, the
side PA, or the polar distance of the body, and the side PZ, the
co-latitude of the place of observation. We can, therefore, com-
pute the side ZA, which is the true zenith distance of the body
observed ; and the difference between this and the observed zenith
distance, (corrected for parallax, [Art. 55,] and instrumental
errors,) will be the amount of refraction for that zenith distance.
The construction of the instrument enables us to follow a
celestial body through its whole course from rising to setting,
measuring altitudes and noting the corresponding times to any
extent that we choose; and the amount of refraction correspond-
ing to each altitude can afterwards be computed at our leisure.
THE EQUATORIAL.
38. The equatorial is similar in general construction to the
altitude and azimuth instrument. It is, however, differently
placed, the plane of the principal graduated circle, C' C', coin-
ciding, not with tKe plane of the horizon, but with that of the
celestial equator, from which peculiarity of position comes the
EQUATORIAL. 4 1
name of equatorial. The circle C'C', when thus placed, is called
the hour circle of the instrument, and the axis A, at right angles
to it, is called the hour or polar axw. It is evident that the axis
is directed towards the poles of the heavens. The circle CO,
the plane of which is perpendicular to the plane of the circle
C" C' t will lie continually in the plane of a circle of declination,
as the instrument is turned about the polar axis, and is hence
called the declination circle. The axis on which this latter circle
is mounted is called the declination axis.
39. Use of the Equatorial. The equatorial is employed prin-
cipally in that class of observations which require a celestial
body to remain in the field of view during a considerable length
of time. The manner in which this
requirement is met is explained
in Fig. 13. Let A A' be the polar
axis of an equatorial, directed to-
wards the pole of the heavens, P.
Let ss*s" be the diurnal circle in
which a star appears to move
about the pole. Suppose the tele-
scope, TT, to be turned in the di-
rection of the star when at , and Fig. is.
to be moved until the intersection of the cross-wires and the star
coincide, and then clamped. Now, if the instrument is made to
revolve about the axis AA' t with an angular velocity equal to
that of the star about the pole, it is plain that, since the angle
which the axis of the telescope makes with the polar axis remains
unchanged, and is continually equal to the angular distance of
the star from the pole, the coincidence of the cross-wires and the
star will remain complete.
A clock-work arrangement, called a driving-clock, is now usually
connected with large equafHrials, by which the instrument may
be moved uniformly about its polar axis, at the required rate, so
that the observer has ample time to measure the angular diameter
of a celestial body, to measure the angular distance between two
stars which are near each other, and to make other micrometric
observations of a similar character.
42
SEXTANT.
THE SEXTANT.
40. The sextant is an instrument by which the angular dis-
tance between two visible objects may be measured. It is used
chiefly by navigators ; but its portability gives it great value
wherever celestial observations are required. The angles for
the measurement of which it is used are the altitudes of celestial
bodies, and the angular distances between celestial bodies or
terrestrial objects.
Fig. 14 is a representation of the sextant. Its form is that
of a sector of a circle, the arc of which comprises 60. A movable
arm, CD, called the index-bar, revolves about the centre of the
sector. This bar carries at one extremity a vernier, D. At the
other extremity of the index-bar, and revolving with it, is placed
a silvered mirror, C, the surface of which must be perpendicular
to the plane of the instrument. This glass is called the index-
glass. Another glass, N, called the horizon- glass, is attached to
the frame of the instrument, and only its lower half is silvered.
SEXTANT. 43
This glass is immovable, and its surface must be perpendicular
to the plane of the instrument. T is a telescope, directed to-
wards the horizon-glass, with its line of sight parallel to the
plane of the instrument. F and E are two sets of colored
glasses, which may be used to protect the eye when the sun is
observed. M is a magnifying glass, to assist the eye in reading
the vernier. G is a tangent screw, which gives a slight motion to
the index-bar, and is used in obtaining an accurate coincidence
of the images.
41. Optical Principle of Construction. The sextant is con-
structed upon a principle in Optics which may be stated thus :
The angle between the first and the last direction of a ray which
has suffered two reflections in the same plane is equal to twice the
angle which the tivo reflecting surfaces make with each other.
To prove this: In Fig 15,
let A and B be the two re-
flecting surfaces, supposed to
be placed with their planes
perpendicular to the plane of
the paper. Let SA be a ray
of light from some body, S,
which is reflected from A to
B, and from Bin the direction
BE. Prolong SA until it meets Fig 15
the line BE. Then will the
angle SEB be the angle between the first and the last direction
of the ray SA. At the points A and B let the lines AD and
jBObe drawn perpendicular to the reflecting surfaces, and pro-
long AD until it meets BC. The angle DCB is equal to the
angle which the two surfaces make with each other. We have
then to prove that the angle SEB is double the angle DCB.
Now since the angle of incidence always equals the angle of
reflection, SAD and DAB are equal, and so are ABC and CBE.
We have, by Geometry,
SEB = SAB ABE
= 2 (DAB ABC),
= 2 DCB.
42. Measurement of Angular Distances. Suppose, now, that
44
SEXTANT.
Fig. 16.
we wish to measure the angular* distance between two celestial
bodies, A and B (Fig. 16). The instrument is so held that its
plane passes through the two bodies, and the fainter of them,
which in this case we suppose to
be B, is seen directly through the
horizon-glass and the telescope.
B is so distant that the rays B' C
and Bm, coming from it, may be
considered to be sensibly parallel.
Let ab and CI be the positions of
the index-glass and index-bar when
~D the index-glass and the horizon-
glass are parallel. Then will the
ray B'C be reflected by the two
glasses in a direction parallel to
itself, and the observer, whose eye is
at D, will see both the direct and the
reflected image of in coincidence. Now let the index-bar be
moved to some new position, CI', so that the ray from the second
body, A, shall be finally reflected in the direction of ml). The
observer will then see the direct image of B and the reflected
image of A in coincidence; and the angular distance between
the two, bodies is evidently equal to the angle between the first
and the last direction of the ray A C, which angle has already
been shown to be equal to twice the angle which the two glasses
now make with each other, or to twice the angle ICI'. If, then,
we know the point Jon the graduated arc at which the index-bar
stands when the glasses are parallel, twice the difference between
the reading of that point and that of the point /' will be the
angular distance of the two bodies.
To avoid this doubling of the angle, every half degree of the
arc is marked as a whole degree, when the graduation is made ;
so that, in practice, we have only to subtract the reading of /
from that of /' to obtain the angle required.
43. Index Correction. The point of reference on the arc from
which all angles are to be reckoned is, as we have already seen,
the reading of the sextant when the surfaces of the index-glass
and the horizon-glass are parallel. This point may fall either
ARTIFICIAL HORIZON. 45
at the zero of the graduation, or to the left or to the right of it;
and to provide for the last case, the graduation is carried a short
distance to the right of the zero, this portion of the arc being
called the extra arc. The reading of this point of parallelism
is called the index correction, and is positive when it falls to the
right of the zero, and negative when it falls to the left. Suppose,
for instance, that the instrument reads 2' on the extra arc when
the glasses are parallel : all angles ought then to be reckoned
from the point 2', instead of from the zero point; in other words,
2' is a constant correction to be added to every reading.
There are several methods of finding the index correction.
One method, which can readily be shown from Fig. 16 to be a
legitimate one, is to move the index-bar until the direct and the
reflected image of the same star are in coincidence, and then
take the reading, giving it Its proper sign according to the rule
above stated. Another method, generally more convenient, in
which the sun is used, may be found in Bowditch's Navigator,
and in most treatises on Astronomy : where also may be found
the methods of testing the adjustments of the sextant.
44. The Artificial Horizon. In order to obtain the altitude
of a celestial body at sea, the sextant is held in a vertical posi-
tion, and the index-bar is moved until the reflected image of the
body is brought into contact with the visible horizon seen through
the telescope of the sextant. The sextant reading is then cor-
rected for the index correction; arid corrections must also be
applied for parallax, refraction, and the dip of the horizon, as
will be explained in the next Chapter. If the body observed is
the sun or the moon, either its upper or its lower limb is brought
into contact with the horizon, and the value of its angular
semi-diameter (given in the Nautical Almanac) is subtracted or
added.
On shore, use is made of the artificial horizon, already alluded
to in Art. 30. This commonly consists of a shallow, rectangular
basin of mercury, the surface of which is protected from the
wind by a sloping roof of glass. The observer so places himself
that he can see the image of the body whose altitude he wishes
to measure reflected in the mercury. He then moves the index-
bar of the sextant until the image of the body reflected by the
46
VERNIER.
sextant is in coincidence with Jhat reflected by the mercury.
.The sextant reading is then corrected for the whole of the index
correction. Half of the result will be, as shown in Art. 30,
the apparent altitude of the body, to which must be applied
the corrections for parallax and refraction to obtain the true
altitude. When the sun or the moon is observed, the upper or
the lower limb of the image reflected by the sextant is brought
into contact with the opposite limb of the image reflected by the
mercury, and the correction for semi-diameter also is applied.
45. The Vernier. ---The vernier is an instrument by which, as
by the reading microscope previously explained, fractions of a
division of a limb may be read.
In Fig. 17, let AB be an arc of
a stationary graduated circle,
and let CD be a movable arm,
carrying another graduated
arc at its extremity. The value
of each division of the limb
A B is one-sixth of a degree, or
10'. The arc on the arm CD
is divided into ten equal parts,
and the length of the arc be-
tween the points and 10 is
Fi - 17 - equal to the length of nine di-
visions of the arc AB. This arc, which the lirnb CD carries, is
called a vernier. Since the ten divisions of the vernier equal in
length nine divisions of the limb, it follows that each division
of the vernier comprises 9' of arc ; in other words, any division
of the vernier is less by V of arc than any division of the limb.
The reading of any instrument which carries a vernier is al-
ways determined by the position of the zero point of the vernier.
If, now, the zero point of the vernier exactly coincides with a
division of the limb, the point 1 of the vernier will fall V behind
the next division of the limb, the point 2 will fall 2' behind the
next division but one, and so on; and if, such being the case, the
vernier is moved forward through an arc of 1', the point 1 will
corne^nto coincidence with a division of the limb; if it is moved
forward through an arc of 2', the point 2 will come into coiiici-
VERNIER. 47
dence with a division on the limb ; and, in general, the number
of minutes of -arc by which the zero point of the vernier falls
beyond the division of the limb which immediately precedes it
will be equal to the number of that point of the vernier which
is in coincidence with a division of the limb. If, then, the zero
point falls between any two divisions of the limb, as 11 20' and
11 30', for example, and the point 2 of the vernier is found to
be in coincidence with any division of the limb, we know that
the zero point is 2' beyond the division 11 20', and that the com-
plete reading for that position of the vernier is 11 22'.
46. General Rules of Construction. In the construction of all
verniers similar to the one above described, the same rules of
construction must be followed : the length of the arc of the ver-
nier must be exactly equal to the length of a certain number
(no matter what) of the divisions of the limb, and the arc must
be divided into equal parts, the number of which shall be greater
by one than the number of these divisions of the limb. Following
these rules, and putting
D the value of a division of the limb,
d " " " " " vernier,
n = the number of equal parts into which the vernier is divided,
we have D d = as a general formula.
The difference D d is called the least count of the vernier.
If, in Fig. 17, we take the length of the vernier equal to 59
divisions of the limb, and divide it into 60 equal parts, we shall
have
which is the least count on most of the modern sextants.
Verniers are sometimes constructed in which the number of
equal parts on the vernier is less by one than the number of the
D
divisions of the limb taken. In this case we have d D = ~
')!/
and the only difference between this class of verniers and the
class above described is that the graduations of the limb and
the vernier proceed in this clas& in opposite directions.
48 SPECTROSCOPE.
OTHER ASTRONOMICAL INSTRUMENTS.
47. The zenith telescope, the theodolite, and the universal instrn'
ment are, in general principle, only modified forms of the port-
able altitude and azimuth instrument.
The octant (sometimes improperly called the quadrant} is
identical in construction with the sextant, excepting only that
its arc contains 45.
The prismatic sextant carries a reflecting prism in place of the
ordinary horizon-glass, and the graduated arc comprises a semi-
circumference.
The reflecting circle is still another modification of the sex-
tant, in which the graduated arc is an entire circumference, and
the index-bar is a diameter of the circle, revolving about the
centre, and carrying a vernier at each extremity. Sometimes
the circle has three verniers, at intervals of 120 of the gradu-
ated arc.
The spectroscope is an instrument which is used, as its name
indicates, -in the examination of the spectra both of terrestrial
substances and of the heavenly bodies. Its use as an instrument
of astronomical research is comparatively recent, but it has
already led to many interesting and remarkable discoveries con-
cerning the constitution of the heavenly bodies. It consists
essentially of three parts: a tube, a prism (or a set of prisms),
and a telescope. Rays of light from either a celestial body or
an artificial flame are made to enter the tube through an ex-
tremely narrow slit at its extremity. These rays pass through
the tube, and fall upon the prism. If necessary, lenses may be
placed within the tube, so that the rays, as they issue from it,
shall fall upon the prism in parallel lines. These rays are dis-
persed by the prism, and a spectrum is formed. This spectrum
is then examined by means of the telescope. There is also an
arrangement by .which rays of light from two substances or
bodies can be introduced through the slit without interfering
with each other, so that their spectra can be formed simul-
taneously, one above the other, and the points of resemblance or
difference between them can be accurately noted.
It is well known that the solar spectrum contains a large
KRRORS. 49
number of dark and narrow parallel lines, which are called
Fraunhofer's lines. The spectra of the stars and of artificial
lights also contain similar series of lines, differing from each
other, each series, however, being constant for the same body or
light. The spectra of chemical substances also present certain
peculiarities, so that each spectrum indicates with certainty the
substance which produces it. Hence, by a comparison of the
spectra of the heavenly bodies with those of known chemical
substances, the existence of many of those substances in the
heavenly bodies has been definitely established. Nor is this all ;
the inspection of any spectrum suffices to tell us whether the
light which forms it comes from a solid or a gaseous body, and
whether, if the light comes from a solid body, it passes through
a gaseous body before it reaches us.
The results of these investigations will be noticed when we
come to the description of the heavenly bodies ; and the method
of investigation will be further illustrated in the Article on the
constitution of the sun. (Art. 102.)
ERRORS.
48. However carefully an instrument may be constructed, how-
ever accurately adjusted, and however expert the observer may
be, every observation must still be regarded as subject to errors.
These errors may be divided into two classes, regular ami -irre-
gular errors. By regular errors we mean errors which remain
the same under the same combination of circumstances, and
which, therefore, follow some determinate law, which may be
made the subject of investigation. Among the most important
of this class of errors are instrumental errors: errors, that is to
say, due to some defect in the construction or adjustment of an
instrument. If, for instance, what we call the vertical circle of
the meridian circle is not rigorously a circle, or is imperfectly
graduated; or if the horizontal axis is not exactly horizontal,
or does not lie precisely east and west ; any one of these imper-
fections will affect the accuracy of the observation. The observer,
however, knowing what the construction and adjustment of the
instrument ought to be, can calculate what effect any given im-
.5
50 ERRORS.
perfection will produce upon his observation, and can thus de-
termine what the observation would have been had the imper-
fection not existed. Regular errors, then, may be neutralized
by determining and applying the proper corrections.
Irregular errors, on the contrary, are errors which are not
subject to any known law. Such, for example, are errors pro-
duced in the amount of refraction by anomalous conditions of
the atmosphere ; errors produced by the anomalous contraction
or expansion of certain parts of the instrument, or by an un-
steadiness of the telescope produced by the wind ; and, more par-
ticularly, errors arising from some imperfection in the eye or the
touch of the observer. Errors such as these, being governed
by no known law, can never be made the subject of theoretic
investigation; but being by their very nature accidental, the
effects which they produce will sometimes lie in one direction
and sometimes in another ; and hence the observer, by repeating
his observations, by changing the circumstances under which he
makes them, by avoiding unfavorable conditions, and finally by
taking the mean, or the most probable value of the results which
his different observations give him, can very much diminish the
errors to which any single observation would be exposed.
NOTE. For complete descriptions of the various astronomical instru-
ments, the student is referred to Chauvenet's Spherical and Practical As
tronomy; Loomis's Practical Astronomy; and Pearson's Practical Astronomy
(published in England).
REFRACTION. 51
CHAPTER III.
REFRACTION. PARALLAX. DIP OF THE HORIZON.
REFRACTION.
49. When a ray of light -passes obliquely from one medium
to another of different density, it is bent, or refracted, from its
course. If a line is drawn perpendicular to the surface of the
second medium at the point where the ray meets it, the ray is
bent towards this perpendicular if the second medium is the
denser of the two, and from it if the first medium is the
denser.
In Fig. 18, let A A, BB, represent two NEC
media of different density, the density of
BB being the greater. Let CD be a
ray of light meeting the surface of BB
at D. At D erect the line ND perpendi- /
cular to the surface of BB, and prolong ^
it in the direction DM. The ray CD is Fi s- 18 -
called the incident ray, and the angle ND C the angle of inci-
dence. When the ray enters the medium BB, it will still lie in
the same plane with CD and ND, but will be bent towards the
line DM, making with it some angle GDM, less than the angle
ND C. To an observer whose eye is at G, the ray will appear
to have come in the direction EG, which is therefore called the
apparent direction of the ray. DG is called the refracted ray,
and the angle GDM the angle of refraction. The angle EDC,
the difference between the directions of the incident and the
refracted ray, is called the refraction.
. It is shown in Optics that, whatever the angle of incidence
may be, there always exists a constant ratio between the sine
of the angle of incidence and that of the angle of refraction,
as long as the same two media are used and their densities are
unchanged. We have, then, in the figure,
REFRACTION.
sin NDQ __
sin GDM = '
k being a constant for the two media A A and BB.
If the second medium, instead of being of uniform density, is
composed of parallel strata, each one of which is of greater
density than the one immediately preceding, as is represented
c _ in Fig. 19, the path of the ray through
these several strata will be a broken
line, Dabc; and if the thickness of
~B each of these successive strata is sup-
posed to be indefinitely small, this
broken line will become a curve.
In the figures above used, the media are represented as sepa-
rated by plane surfaces; but the same phenomena are noticed,
and the same laws hold good, if the media are separated by
curved surfaces.
50. Astronomical Refraction. It is determined by experiment
that the density of the air gradually diminishes as we ascend
above the surface of the earth, and it is estimated that at a
distance of fifty miles above the surface the upper limit of the
air is reached ; or, at all events, that the density of the air is so
small at that distance that it exerts no appreciable refracting
power. We may, therefore, consider the air to be made up of
a series of strata concentric with the earth's surface, the thick-
ness of each stratum being in-
definitely small, and the den-
sity of each stratum being
greater than that of the stra-
tum next above it. Now, in
s Fig. 20, let the arc BD repre-
sent a portion of the earth's
surface, and the arc MN a por-
tion of the upper limit of the
atmosphere. Let 8 be a ce-
lestial body, and SA a ray of
light from it, which enters the
atmosphere at A. Let the
normal (or radius) AC be
REFRACTION 53
drawn. As the ray of light passes down through the atmos-
phere, it is continually passing from a rarer to a denser
medium, so that its path is continually changed, and becomes
a curve AL, concave towards the earth, and reaching the earth
at some point L. Since the direction of a curve at any point
is the direction of the tangent to the curve at that point, the
apparent direction of the ray of light at L will be repre-
sented by the tangent LS f , and in that direction will the body
S appear to lie, to an observer at L. If the radius OL'be
indefinitely prolonged, the point Z, where it reaches the celestial
sphere, will be the zenith of the observer at L, the angle ZLS'
will be the apparent zenith distance of the body 8, and the
angle which the line drawn from the body to the point L
makes with the line LZ will be the true zenith distance of S.
The effect, then, of refraction is to decrease the apparent zenith
distances, or increase the apparent altitudes of the celestial
bodies. Since the incident ray SA, the curve AL, and the
tangent LS' all lie in the same vertical plane, the azimuth of the
celestial bodies is not affected.
51. General Laws of Refraction. By an investigation of the
formulae of refraction, and by astronomical observations already
described (Art. 37), the amount of refraction at different alti-
tudes has been obtained, and is given in what are called "tables
of refraction." The following general laws of refraction will
serve to give the student some idea of its amount, and of the
conditions under which it varies:
(1.) In the zenith there is no refraction.
(2.) The refraction is at its maximum in the horizon, being
there equal to about 33'. At an altitude of 45 it amounts
to 57".
(3.) For zenith distances which are not very large, the re-
fraction is nearly proportional to the tangent of the zenith
distance. When the zenith distance is large, however, the ex-
pression of the law is much more complicated. No table of re-
fraction can be trusted for an altitude of less than 5.
(4.) The amount of refraction depends upon the density of the
air, and is nearly proportional to it. The tables give the re-
fraction for a mean state of the atmosphere, taken with the
54 PARALLAX.
barometer at 30 inches and the thermometer at 50. If the
temperature remains constant, and the barometer stands above
its mean height, or if the height of the barometer is constant,
and the thermometer stands below its mean height, the density
:)f the atmosphere is increased, and the refraction is greater
than its mean amount. Supplementary tables are therefore
given, from which, with the observed heights of both barometer
and thermometer as arguments, we may take the necessary cor-
rections to be applied to the mean refraction.
(5.) Since the effect of refraction is to increase the apparent
altitudes of the celestial bodies, the amount of refraction for
any apparent altitude is to be subtracted from that apparent
altitude, or added to the corresponding zenith distance.
52. Effects of Refraction. The apparent angular diameter of
the sun and of the moon being about 32', and the refraction iu
the horizon being 33', it follows that when the lower limb of
either body appears to be resting on the horizon, the body is m
reality below it. One effect, then, of refraction is to lengthen
the time during which these bodies are visible. Still another
effect is to distort the discs of the sun and the moon when near
the horizon : for since the refraction varies rapidly near the
horizon, the lower extremity of the vertical diameter of the
body will be more raised than the upper extremity, thus appa-
rently shortening this diameter, and giving the body an ellip-
tical shape. When the body comes still nearer the horizon, its
disc is distorted into what is neither a circle nor an elljpse, but
a species of oval, in which the curvature of the lower limb is
less than that of the upper one. The apparent enlargement of
these bodies when near the horizon is merely an optical delu-
sion, which vanishes when their diameters are measured with an
ii.strument.
PARALLAX.
53. The parallax of any object is, in the general sense of the
word, the difference of the directions of the straight lines drawn
to that object from two different points: or it is the angle at
the object subtended by the straight line connecting these two
points. In Astronomy, we consider two kinds of parallax : yco-
PARALLAX.
55
centric parallax, by which is meant the difference of the directions
of the straight lines drawn to the centre of any celestial body from
the earth's centre and any point on its surface, and heliocentric
parallax, or the difference of the directions of the lines drawn to
the centre of the body from the cen-
tre of the earth and the centre of the
sun. The former is the angle at the
body subtended by that radius of
the earth which passes through the s f
place of observation : the latter the
angle at the body subtended by the
straight line joining the centre of
the earth and that of the sun.
54. Geocentric Parallax. In Fig.
21, let Obe the centre of the earth,
and L some point on its surface, of which Z is the zenith. Let
S- be some celestial body. The geocentric parallax of the body
is the angle CSL. Let S> be the same body in the horizon.
The angle LS' C is the parallax of the body for that position,
and is called its horizontal parallax. If we denote this horizontal
parallax by P, the earth's radius by E, and the distance of the
body from the earth's centre by d, we have, by Trigonometry,
Fig. 21.
To find the parallax for any other position, as at S, we repre-
sent the angle LSC by p, and the apparent zenith distance
of the body, or the angle ZLS, by z, the sine of which is equal
to the sine of its supplement SLC. We have from the tri-
angle LSC, since the sides of a plane triangle are proportional
to the sines of their opposite angles,
sin p R
sin z d
Combining this equation with the preceding, we have,
sin p = sin Psin z.
Since P and p are small angles, we may consider them propor-
tional to their sines, and thus have, finally,
p P sin z.
The parallax, then, is proportional to the sine of the zenith
56 PARALLAX.
distance, and may be found for any altitude when the hori
zontal parallax is known. It evidently decreases as the alti-
tude increases, and in the zenith becomes zero.
55. Application of Parallax. In order that observations
made at different points of the earth's surface may be com-
pared, they must be reduced to some common point. Geocen-
tric parallax is applied to reduce any altitude observed at any
place to what it would have been had it been observed at the
earth's centre. We see from Fig. 21 that parallax acts in a
vertical plane, and that the zenith distance of the body as ob-
served from the earth's centre, or the angle ZC8, is less than the
observed zenith distance ZLS, by the parallax CSL. Parallax,
then, is always subtractive from the observed zenith distance,
and additive to the observed altitude.
The parallax above described is, strictly speaking, the paral-
lax in altitude. There is also, in general, a similar parallax in
right ascension, and in declination, formulae for deriving which
from the parallax in altitude are given in other works.
56. Heliocentric Parallax. It may sometimes happen that we
wish to reduce an observation from what it was at the centre
of the earth to what it would have been if it had been made
at the centre of the sun. Fig. 21, and the formulae obtained
from it, will apply equally well to this case, by making the
necessary changes in the description of the figure and in the
names of the angles.
Let S be still a celestial body, but let C be the centre of the
sun, and L that of the earth. The angle p will then represent
the heliocentric parallax, and the angle SLCihe angular dis-
tance of the body from the sun, as measured from the earth's
centre, or, as it is called, the body's elongation. The angle P
will be the greatest value of the heliocentric parallax, taken
when the body's elongation from the sun is 90, and is called
the annual parallax. We shall then find, from the formulae
of Art. 54, that the annual parallax has for its sine the ratio
of the distance of the earth from the sun to that of the body
from the sun, and that the parallax for any other position is
the product of the annual parallax by the sine of the body's
elongation.
DIP OF THE HOEIZON.
57
Fig. 22.
DIP OF THE HORIZON.
57. The dip of the horizon is the angular depression of the
visible horizon below the celestial hori- B
zon. In Fig. 22, let HG be a por-
tion of the earth's surface, and C
the earth's centre. Let a radius of
the earth, CA, be prolonged to some
point D, beyond the surface, and let
an observer be supposed to be at the
point D. At the point D let the line
BD be drawn perpendicular to the line
CD, and also the line DH, tangent to
the earth's surface at some point H. If these two lines be revolved
about the line CD, DB will generate the plane of the celestial
horizon (since we have seen that all planes passed perpendicular
to the radius will, when indefinitely extended, mark out the
same great circle on the celestial sphere), and DH will gene-
rate the surface of a cone, which will touch the earth in a
small circle. If we disregard for the present the effect of the
earth's atmosphere, this small circle will be the visible horizon
of the observer at D, and the angle BDHvfill be the dip. DA
is the linear height of the observer at D.
Now let a radius, CH, be drawn to the point of tangency H.
The angles BDH and HCD, having their sides mutually per-
pendicular, are equal. Represent the angle HCD by D, the
earth's radius by J2, and the observer's height, AD, by h. ID.
the triangle DHC, right-angled at H, we have,
since D is small, it is better to use the formula,
cos D = 1 2 sin 8 * D :
hence we have,
=1 28in f iD:
58
DIP OF THE HORIZON.
As the angle D is small, we mav take
sin \ D = J D sin 1" :
and as h is very small in comparison with JR, we may also
assume (E -{- h~) to be sensibly equal to E. Making these
changes in the above equation, and finding the value of D, we
have
Substituting in this expression the value of the earth's radius
in feet, we have, finally,
D = 63".8 y~h^
h being expressed in feet.
The dip, then, for a height of one foot is 63".8 ; and for
other heights it is proportional to the square root of the number
of feet in the height.
58. Effect of Atmospheric Refraction.
If the effect of atmospheric refrac-
tion is taken into consideration, the
G line HD must be a curved line, as is
represented in Fig. 23. The point H
will then appear to lie in the direc-
tion DH f , to the observer at D, and
the dip will be the angle BDH '. The
Fi s- 23 -* effect, then, of refraction is to decrease
the dip, the amount by which it is decreased being about -j-^th
of the whole.
59. Application of Dip. Tables have been computed in
which may be found the proper dip for different heights above
the surface of the earth. Dip constitutes one of the correc-
tions which are to be applied at sea to the observed altitude of
a celestial body to obtain its true altitude: its altitude, that is,
above the celestial horizon. Since the visible horizon lies below
the celestial horizon, this correction is evidently subtractive.
The curved line HD is tangent to the earth's surface at H.
MEASUREMENT OF THE EARTH. . r >9
CHAPTER IV.
THE EARTH. ITS SIZE, FORM, AND ROTATION.
60. HAVING seen what are the construction and the adjustments
of the principal astronomical instruments, to what uses each is
adapted, and what corrections are to be applied to the observa-
tions which are taken, we are now ready to proceed to the solu-
tion of some of the many questions of interest which the study
of Astronomy opens to us. And first of all, let us see how as-
tronomical observations will help us to a knowledge of the size
and the form of the earth. The question is one of the first im-
portance; for upon the determination of the size of the earth
depends in a great measure, as we shall see further on, the deter-
mination of the magnitudes and the distances of the other
heavenly bodies. Having seen the facts which seem to point to
the conclusion that the earth is spherical in form, w r e will start
with the assumption that this conclusion is correct, and proceed
to determine the magnitude of the earth, regarded as a sphere.
Now, we know from Geometry what is the ratio between the
radius of a sphere and the circumference of any great circle of
that sphere; and, therefore, if we can obtain the length of the
circumference of any great circle of the earth, of a meridian,
for instance, we can at once determine the radius of the earth.
And more than this : if we can measure the length of any known
arc of this meridian, of one degree, for instance, we can compute
the length of the entire circumference. The determination of
the earth's radius, then, depends only on our ability to satisfy
these two conditions:
(1.) We must be able to measure the linear distance on the
earth's surface between two points on the same meridian.
(2.) We must be able to measure the angular distance between
these same two points.
61. First Condition. A reference to Fig. 24 will explain how
00
MEASUREMENT OF THE EARTH.
Fig. 24.
the first of these two conditions may be satisfied. Let A and G
represent the two points on the same meridian the
distance between which we wish to measure. We
have already seen (Art. 36) how an altitude and
azimuth instrument may be so adjusted that the
sight-line of the telescope will lie in the plane of
the meridian. Let an instrument be so adjusted
at the point A. Let some convenient station B be
taken, visible at A, and let the distance AB be
carefully measured. This distance is called the
base-line. Now, by means of the telescope, adjusted
to the plane of the meridian, let some point C be
established on the meridian, which shall also be
visible from B, and let the angles CAB and ABC
be measured. We now know in the triangle ABC
two angles and the included side, and can compute the distances
AC and CB. We now take some suitable point D, measure
the angles DCB and DBC, and knowing CB, we can obtain the
distance CD. The instrument is now taken to the point C, and
again established in the plane of the meridian, either by the
method of Art. 36, or by sighting back, as it is called, to A, or by
both methods combined. A third point on the meridian, E,
visible from D, is then selected, the angles ECD and ED C are
measured, and the distances EC and ED computed. This pro-
cess is continued until the whole distance between A and G has
been obtained.
This method of measurement is called the method of triangu-
lation. The base-line, AB, is purposely taken under circum-
stances which favor its accurate measurement, and the rest of
the work consists in the determination of horizontal angles,
which presents no special difficulty, and in the solution of tri-
angles by computation.
Two things are to be noticed in reference to these triangles.
The first is that in selecting the points B, C, D, &c., care must be
taken so to choose them that the triangles ABC, BCD, &c., shall
be nearly equiangular; since triangles in which there is a great
inequality of the angles (ill-conditioned triangles, as they are
called) will be much more likely to cause some error in the work.
MEASUREMENT OF THE EARTH. 61
The second thing to be noticed is that these triangles are really
spherical triangles, and must therefore be solved by the formulae
of Spherical Trigonometry. If, for any reason, we are forced
to take any of the points C, E, &c., off the meridian, the cor-
responding distances can be reduced to the meridian by appro-
priate formulae.
The correctness of the result may be tested by measuring the
distance GF, and comparing its measured length with that ob-
tained by computation. The marvellous accuracy of this method
of measurement is shown by the fact that in an arc of the meri-
dian measured by the French at the close of the last century,
and which was several hundred miles in length, the discrepancy
between the measured and the computed length of the second
base-line was less than twelve inches.
62. Second Condition. The second condition requires that
the angle at the centre of the earth, subtended by the arc of the
meridian measured, shall be obtained. This angle is evidently
the difference of latitude of the two extremities of the arc, and
therefore all that is needed to satisfy this condition is that the
latitude of each extremity shall be determined by appropriate
observations.
Instead of determining the latitude of each place independently
of the other, we may, if we choose, obtain the difference of
latitude directly, by observing at each place the meridian zenith
distance of the same celestial body. In Fig. 25, let A and G be
the two extremities of the arc, C the centre
of the earth, and S the celestial body on
the meridian. If Z' is the zenith of the
point A, the meridian zenith distance of 8
at A, reduced to the centre of the earth, is
the angle Z' CS. In the same manner the
true meridian zenith distance of S at G is
the angle ZCS. The difference of these two
zenith distances, or the angle ZCZ\ is evi-
dently the difference of latitude of G and A. Fi s- 25 -
If the celestial body crosses the meridian between the l\vo
zeniths, as at $', the difference of latitude is numerically the
sum of the two meridian zenith distances.
62 FORM OF THE EARTH.
63. Results. By the process ajbove described, or by processes
of a similar character, arcs of different meridians, and in differ-
ent latitudes, have been carefully measured. The sum of the
arcs thus measured is more than 60, and the length of a degree
of the meridian has been found to be, on the average, 69.05 miles.
Multiplying this by 360, we obtain 24,858 miles for the circum-
ference of a meridian, and dividing this circumference by -,
(3.1416) we find the length of the earth's diameter to be 7912
miles.
64. Spheroidal Form of the Earth. One remarkable fact is
noticed when we compare the lengths of the degrees of the meri-
dian, measured in different latitudes ; and that is, that the length
of the degree is not the same at all parts of the meridian, but sen-
sibly increases as we leave the equator. The length of a degree
at the equator is found to be 68.7 miles, whilst at the poles it is
computed to be 69.4 miles. The conclusion drawn from this
fact is that the figure of the earth is not rigorously that of a
sphere, since a spherical form necessarily implies an absolute
uniformity in the length of a degree in all parts of a great circle.
In order to determine the exact geometrical figure of the earth,
we must bear in mind that the curvature of a line is always pro-
portional to the change in the direction of the tangents drawn
at successive points of that line. Now, since the altitude of the
elevated pole at any place is equal to the latitude of that place,
it follows that an advance towards the pole of one degree in lati-
tude is accompanied by a depression of one degree in the plane of
the horizon. If, therefore, in order to effect a change of one de-
gree in our latitude, we are forced to advance a greater number
of miles at the pole than at the equator, we conclude that the cur-
vature of the meridian is less at the pole than at the equator. Now,
this same inequality in its curvature is
also a peculiarity of the ellipse : and hence
we infer that the form of the earth's me-
ridians is not that of a circle, but that
of an ellipse, as represented in Fig. 26.
The axis of the earth, Pp, corresponds
to the minor axis of an ellipse, at the
extremities of which the curvature is the
DENSITY. 63
least; and the equatorial diameter of the earth, EQ, corresponds
to the major axis of an ellipse, at the extremities of which the
curvature is the greatest.
The form of the earth, then, is that of the solid which would
be generated by the revolution of an ellipse about its minor
axis, which solid is called in Geometry an oblate spheroid. A
more common but less accurate name given to the form of the
earth is that of a sphere, flattened at the poles.
65. Dimensions of the Earth. The following are the dimen-
sions of the earth, when its spheroidal form is taken into con-
sideration. The determination is that of Sir G. B. Airy, the
Astronomer Royal of England.
Polar diameter ......................... 7899.170 miles.
Equatorial diameter ................... 7925.648 miles.
These values are believed to be within a quarter of a mile of the
true values. They differ from the results obtained by the astro-
nomer Bessel by only about o^th of a mile.
The compression, or oblateness, of an oblate spheroid is the
ratio of the difference between the major and the minor axis
of the generating ellipse to its major axis. The compression of
the earth is therefore ' . : which is about th.
If a and b represent the semi-major and the semi-minor axis
of the generating ellipse, the expression for the volume of the
oblate spheroid is $xa' 2 b. Substituting in this expression the
values of a and b, we find the earth's volume to be about 260
billions of cubic miles.
66. Density of the Earth. There are various methods of de-
termining the mean density of the earth. The following is a
brief summary of the method of determining it by means of the
torsion balance. This balance consists of a slender wooden rod,
supported in a horizontal position by a very fine wire at its
centre. To the extremities of this rod are attached two small
leaden balls. If left free to move, this horizontal rod will of
course come to rest when the supporting wire is free from
rorsion. Two much larger leaden balls are now brought near
the two suspended balls, and on opposite sides, so that the
attractions of both balls may combine to twist the wire in
64 ROTATION.
same direction. The smaller balls will be sensibly attracted
by the larger ones, and the horizontal rod will change the
direction in which it lies. The amount of this deflection is
very carefully measured, and from it is computed the attraction
which the large balls exert on the small ones. But we know
the attraction which the earth exerts on the small balls, it being
represented by their weight: and we know also the volumes
of the earth and the attracting balls. Finally, we know the
density of lead: and from these data it is possible to compute
the mean density of the earth.
A series of over 2000 experiments of this nature was con-
ducted in England, in 1842, by Sir Francis Baily. The mean
density of the earth, obtained from these experiments, was 5.67 :
the density of water being the unit. Other methods of deter-
mining the density of the earth have been employed, the main
principle in each method being the comparison of the at-
traction exerted by the earth upon some object with that ex-
erted by some other body, whose density can be ascertained,
upon the same object. The results of these experiments do not
differ materially from the results of the experiments with the
torsion balance.
The volume and density of the earth being known, what is
commonly called its weight can be computed. It is found to
be about six sextillions of tons.
ROTATION OF THE EARTH.
67. Up to this point we have assumed the earth to be at
rest, and the apparent diurnal motions of the heavenly bodies
to be real motions. By careful observation of the sun, the
moon, and the most conspicuous of the planets, astronomers
have demonstrated that each of these bodies rotates upon a
fixed axis. Analogy, therefore, points to a similar rotation of
our own planet: and besides this, there are many phenomena
which are inexplicable if the earth is at rest, but which are
fully accounted for on the supposition that it rotates upon an
axis. We will now examine the principal of these phenomena.
68. The weight of the same body is not the same in different
latitudes. Careful experiments made in different latitudes show
CENTRIFUGAL FORCE. 65
that the weight of the same body is not constant at all parts
of the earth's surface, but increases with the latitude. A body
which weighs 194 pounds at the equator will weigh 195 pounds
if taken to either pole ; that is to say, the weight of any body is
increased by j^th of itself when carried from the equator to
the pole. This experiment cannot be made with the ordinary
balances in which bodies are weighed : since it is obvious that
the same cause, whatever it may be, which affects the weight
of the body will also affect that of the weights by which it is
balanced, and by the same amount, so that the scales will still
remain in equilibrium. If, however, we test the weight of a
body (the force, that is to say, with which it tends to the earth's
centre) by the effect which it has in stretching a spring, the
increase of weight will be found to be as stated above.
Part of this increase of weight is due to the spheroidal form
of the earth, since a body when at the pole is nearer the centre
of the earth than when at the equator. The amount of increase
due to this cause has been calculated to be about ^ih; hence
the difference between j^th and g^o^ n J which is 2^-gth, still re-
mains to be accounted for. We shall now see how it is com-
pletely accounted for by the supposition that it is the effect of
the centrifugal force which is induced by a rotation of the earth
upon its polar axis.
69. Centrifugal force. The tendency which a body has, when
revolving about any point as a centre, to recede from that centre,
is called its centrifugal force. The formula for the centrifugal
force may be found in any treatise on Mechanics, and is as
follows :
in which / is the centrifugal force, r the
radius of the circle of revolution, and t the
veriodic time, or the time in which the
revolution is performed. Now, in Fig. 27
let the earth be supposed to rotate about
its polar axis, Pp, once in every sidereal
day, which, as we have already seen
(Art. 7), is 3m. 56s. less than the mean
66 CENTRIFUGAL FOIICE.
solar day, and therefore contains 86,164s. Substituting thi.
value of t in the formula given al>ove, and substituting for r the.
value of the earth's equatorial radius in feet, and computing
the value of/, we shall find that the centrifugal force at the
equator is .1113 feet. Now the actual force of gravity at the
equator is found, by Mechanics, to be 32.09 feet. If the earth
were at rest, the force of gravity at the equator would evidently
be 32.09 + -1H3 feet. Hence the diminution of gravity at
the equator, due to centrifugal force, (in other words, the loss
of weight), is equal to y^f^, or 5 |^th.
Since the periodic time (t in the formula) is constant for all
places on the earth's surface, it is evident, from the formula, that
the centrifugal force at any place L is to the centrifugal force
at the equator as the radius of revolution at L, or LM, is to CQ
But we have in the figure,
ML ML
-QQ~ = ~QL cos <& C cos Latitude.
Denoting, then, the centrifugal force at the equator by C,
and that at L by c, we have,
c = C cos L:
or the centrifugal force varies with the cosine of the latitude.
The centrifugal force at L acts in the direction of the radius
of revolution ML. Let its amount be represented by LB,
taken on LM prolonged. This force may be resolved into two
forces : LA, in the direction from the centre of the earth, and AB,
at right angles to LA. The force LA, being directly opposed
to the attraction of the earth, has the effect of diminishing the
weight of bodies at L, and may therefore be taken to represent
the loss of weight at L.
Denoting the loss of weight by w, and the centrifugal force
at L by c, as before, we have, from the triangle ABL,
w = c cos L.
But we have already,
c = C cos L :
/. w = C cos 2 L.
Now, at the equator, as is evident from the figure, the whole
effect of the centrifugal force is exerted to diminish the weight
of bodies, and C therefore also represents the loss of weight at
TRADE WINDS. 07
the equator. We. have then, finally, that the loss of weight of a
body at any latitude, due to centrifugal force, is equal to the pro-
duct of -.j^th of the weight multiplied by the square of the cosine
of the latitude.
70. Spheroidal Form of the Earth due to Centrifugal Force.
We see, then, that the supposition that the earth rotates upon its
axis fully explains the observed difference in the weight of the
same body in different latitudes. But this is not all : for if we
assume that the particles of matter of which the earth is com-
posed were formerly in a fluid or molten condition, and there-
fore free to move, the spheroidal form of the earth is itself a
proof of the earth's rotation. Numerous experiments may be
made to show that, for a fluid body at rest, the form of equili-
brium is that of a sphere : and that, for a fluid body which
rotates, the form of equilibrium is that of a spheroid, the oblate-
ness of which increases with the velocity of rotation. Knowing
the volume and the density of the earth, and assuming the time
of rotation to be twenty-four sidereal hours, it is possible to
calculate the form of equilibrium which a fluid mass under
these conditions will assume : and this form is found to be that
of a spheroid, with an oblateness very nearly identical with the
known oblateness of the earth.
This tendency of a fluid mass to assume a spheroidal form
under rotation may also be shown in Fig. 27. The centrifugal
force LB was resolved into the two forces LA and AJB, the
former of which forces has already been discussed. The effect
of the latter force, AB, is evidently a tendency in the particle
L to move towards the equator EQ; and a similar force acting
upon all the particles of matter on the earth's surface, excepting
those at the poles and at the equator, will cause them all to
move in the direction of the equator, and thus give a spheroidal
form to the mass.
71. Trade Winds. The trade winds are permanent winds
which prevail in and sometimes beyond the torrid zone. These
winds are northeasterly in the northern hemisphere and south-
easterly in the southern hemisphere. The air within the torrid
zone being, in general, subject to a greater degree of heat than
the air at other portions of the earth's surface, rises, and its
68 PENDULUM EXPERIMENT.
place is filled by air which comes in from the regions beyond the
tropics. If the earth were at res*t, these currents of air would
manifestly have simply a northerly and a southerly direction.
Now, we all know that, when we travel in any direction on a
still day, or even when the wind is moving in the same direc-
tion with us, but with a less velocity, the wind seems to come
from the point towards which we are going. We see from Fig.
27 that, if the earth is rotating upon its polar axis, the linear
velocity of rotation decreases as the latitude increases. Hence,
the air from beyond the tropics, having at the start only the
linear velocity of the place which it leaves, will, as it moves
towards the equator, have continually a less velocity than that
of the surface over which it passes, and will seem to come from
the quarter towards which those places are moving. If, then,
the earth is rotating from west to east, these currents of air will
have an apparent motion from the east, which motion, when
compounded with the motion from the north and the south,
before mentioned, will give us the northeasterly and south-
easterly winds which we call the Trades.
72. The Pendulum Experiment* The last and decidedly the
most satisfactory proof of the earth's rotation which we shall
notice, is that which comes from the apparent rotation of the
plane of a freely-suspended pendulum, when made to vibrate
at any point on the earth's surface except the equator.
It is an established law in Mechanics that a pendulum, freely
suspended from a fixed point, always vibrates in the same plane ;
and also that if we give the point of support a slow movement
of rotation about a vertical axis, the plane of vibration will still
remain unchanged. If, for instance, we suspend a ball by a
string, and, having caused it to vibrate, twist the string, the ball
will rotate about the axis of the string, while the plane in which
it vibrates will not be affected.
Now, let us suppose that a pendulum is suspended at the north
pole, and is made to vibrate: and let us further suppose that the
earth rotates from west to east, once in 24 hours. The line in
which the plane of vibration intersects the plane of the horizon
* This is called FoucaulCs experiment. A full discussion of it is given in
the American Journal of Science, 2d series, vols. XII-XIV.
PENDULUM EXPERIMENT. 69
will move about in the plane of the horizon, in a direction oppo-
site to that in which the earth is rotating, and with an equal
velocity, thus completing one revolution in 24 hours. In Fig.
28, let AGED be the horizon of the ob-
server at the north pole, and let the earth
rotate in the direction indicated by the ( \\y \\
arrows. Let the pendulum at P be set
swinging in the direction of some diameter,
AB, of the horizon. At the end of an hour,
the rotation of the earth will have carried
this diameter to some new position A'B',
at the end of the next hour to some new position A"J3", &c. :
while the pendulum will still swing in the original direction AB.
To the observer, then, unconscious of the earth's rotation, the
plane of vibration, which really remains unchanged, will appear
to rotate in a direction opposite to that in which the earth is
rotating.
At the south pole, under the same suppositions, a similar phe-
nomenon will be noticed, except that the plane of vibration will
apparently move in the opposite direction. Thus, if at the north
pole the apparent motion of the plane is like that of the hands
of a clock, as we look on its face, the apparent motion at tho
south pole will be the opposite to this.
Again, if a pendulum is made to* vibrate in the plane of a
meridian at the equator, there will be no apparent change in the
plane of vibration, since it will always coincide with the plane
of the meridian, and hence the pendulum will continue to
swing north and south during the entire period of the earth's
rotation. The condition that the pendulum shall here swing in
the plane of a meridian is entirely unnecessary, and is made
only for the sake of illustration ; for there will be no apparent
change in the plane of vibration, whatever may be the direction
in which the pendulum is made to vibrate.
The apparent rotation, then, of the plane of vibration of the
pendulum is 360 in 24 hours at the poles, and nothing at the
equator. At places lying between the equator and the poles,
the apparent angular motion of the plane of vibration will be
between these two limits; in other words, less than 360 in
70 LINEAR VELOCITY OF ROTATION.
24 hours. Appropriate investigations show that the apparent
angular motion of the plane of* vibration at any place in any
interval of time is equal to the angular amount of the earth's
rotation in that time, multiplied by the sine of the latitude of
the place.* Thus, at Annapolis, we have for the angular motion
in one hour,
15 sin 38 59' = 9 26':
so that the plane of vibration will make one apparent rotation
at Annapolis in 38h. 09m.
Such is the theory of the pendulum experiment. Now, nume-
rous experiments have been made in different latitudes, and in
every case an apparent rotation of the plane of vibration from
east to west has been observed, with a rate agreeing very closely
with that demanded by the theory ; and the conclusion is irre-
sistible that the earth rotates on its polar axis, from west to east,
once in every sidereal day.
73. Linear Velocity of Rotation. Taking the equatorial cir-
cumference of the earth to be 24,900 miles, we have a linear
velocity of over 1000 miles an hour, and over 17 miles a minute.
This is the velocity at the equator. The linear velocity at other
points on the earth's surface is less than this, since the circum-
ferences of the parallels of latitude are less than the circumfer-
ence of the equator. Since the circumference of any parallel is
* This formula may be obtained by the principles of the resolution of ro-
tation, given in treatises on Mechanics. Thus, in the
figure, the rotation of the point L about the axis of
the earth, PO, may be resolved into two rotations,
one about the radius LO, and the other about the
radius MO, drawn perpendicular to LO. If v re-
presents the angular velocity of L about the axis
PO (or 15 in one hour), and v f and v" the angular velocities about the
axes LO and MO, we have, from Mechanics,
v' = v cos LOP, and v" v cos POM.
NOAV, the rotation about the axis OM will have no effect in changing the
apparent position of the plane of vibration of the pendulum, since it is
analogous to the case at the equator considered in the text ; while the rota-
tion about the axis LO, being analogous to the case at the pole, will pro-
duce a similar effect. The apparent angular motion, then, of the plane
of vibration will be v cos LOP, or v sin Lat.
LINEAR VELOCITY OF ROTATION. 71
to that of the equator as the radius of the parallel is to the
radius of the equator, the linear velocity will diminish as we
leave the equator in the same ratio that the radii of the succes-
sive parallels diminish : in the ratio, that is, of the cosine of the
latitude, as was proved in Art. 69. For instance, the cosine of
60 being J, the linear v o looHv nt thst latitude is on'y 8
a minute.
72 LATITUDE.
CHAPTEK V.
LATITUDE. LONGITUDE.
LATITUDE.
74. THE latitude of any place on the earth's surface has been
proved, in Articles 10 and 11, to be equal to either the altitude
of the elevated pole or the declination of the zenith at that
place. We shall now proceed to explain the principal methods
by which either one or the other of these arcs may be found.
75. First Method. Let Fig. 29 represent a projection of the
celestial sphere on the plane of the celestial
meridian, RZHN, of some place. HR is
the celestial horizon at that place, Z the
zenith, P the elevated pole, and EQ the
equator. Let s represent some circumpolar
star, whose declination is known, at its
lower culmination. Let its meridian alti-
tude be observed, and corrected for instru-
mental errors and refraction. (For all celestial bodies except the
sun, the ( moon, and the planets, the corrections for parallax and
semi-diameter will be inappreciable.) To this corrected altitude
add the star's polar distance, the complement of the star's known
declination. The sum is the altitude of the elevated pole, or
the latitude.
If the circumpolar star is at its upper culmination, as at $',
the polar distance is to be subtracted from the corrected altitude.
If Ti r and h denote the corrected altitudes at the upper and
the lower culmination, p' and p the corresponding polar dis-
tances, and L the latitude, we have evidently
L = h'p'
L = h + /; :
whence L = 2 (k' -f //.) -f } (/> p)-
LATITUDE. 1
In this formula the value of the latitude does not depend on the
absolute value of either polar distance, but merely on the chart ye
of the polar distance between the two transits, which is usually
s?o small as to be neglected. This method, then, is free from any
error in the declination, and is used at all fixed observatories.
76. Second Method. When the star is at its upper culmina-
tion, it will, in general, be more convenient to find the declina-
tion of the zenith from the meridian zenith distance of the star.
Taking the star s', for instance, and denoting its meridian zenith
distance by z, and its declination by d, we have
L = ZQ = Qs' Zs' ^d z. (a)
For the star s", we have
L = Zs" + Qs" = z + d, (b)
and for the star s"
L = Zs" Qs" = z d. (c)
From these three formulae a general rule may be deduced, appli-
cable to the upper culmination of every star. We notice that
in the formulae (a) and (6), where d is positive, the stars s' and
s" are on the same side of the equator with the elevated pole;
that is to say, their declinations have the same name as the ele-
vated pole; while in the formula (c) the declination has the
^.opposite name. We also notice that in the formulae (6) and (r,} t
where z is positive, the stars are on the opposite side of the zenith
from the elevated pole; in other words, their bearing has the op-
posite name to that of the pole : while the bearing of the star ',
in the formula for which z is negative, has the same name as the
elevated pole. The general rule, then, for all these stajs will be
the following: If the star bears south, mark the zenith distance
lorth; if it bears north, 'mark the zenith distance south; mark
the declination north or south, as the star is north or south of
vJie equator, and combine the zenith distance and the declina-
tion, thus marked, according to their names.
77. Third Method. A very successful adaptation of the pre-
ceding method is made by using two stars which culminate at
nearly the same time, but on opposite sides of the zenith, as s'
and s" in Fig. 29. These two stars are so selected that the dif-
ference of theii zenith distances is very small, and can be mea-
74 LATITUDE.
sured directly by means of a micrometer. By the formulae of
the preceding article we have for a',
L^d z,
and for s", denoting its meridian zenith distance and declinatioii
by z' and d',
L = d' + z',
whence we have,
L = J (d + d") -f i- (z r z\
The determination of the latitude is thus made free from any
error in the graduations of the vertical circle, and depends only
on the known declinations of the two stars, and on the difference
of their zenith distances. Errors in the refraction are also very
nearly eliminated.
This is the principle of what is called Talcott's Method, a
method very commonly used by the United States Coast Survey.
The instrument employed is the zenith telescope, a modification
of the altitude and azimuth instrument. The two stars are so
selected that the difference of their zenith distances is less than
the breadth of the field of the telescope. The instrument is set
in the plane of the meridian to the mean of the two zenith dis-
tances, and for the star which culminates first. When this star
crosses the meridian, it is bisected by the micrometer wire, and
the micrometer is read. The instrument is then turned 180 in
azimuth, and the process is repeated with the second star. The
difference of the zenith distances is then obtained from the dif-
ference of the two micrometer readings, and added to the half
sum of the two declinations, according to the formula.
78. Fgurth Method. When the local time (either solar or
sidereal) is known, the latitude may be obtained from altitudes
which are not measured on the meridian. Let Fig. 30 be a pro-
jection of the celestial sphere on the plane
of the horizon. Z is the zenith of the place,
P the elevated pole, PZthe co-latitude, and
S a star, whose altitude is measured. SPZ
is the hour angle of the star, which can be
obtained from the local time noted at the
instant the altitude is observed. PS is the
star's known polar distance. In the triangle
REDUCTION OF THE LATITUDE.
SPZ, we have the sides ZS and SP, and the angle SPZ, and can
therefore compute the value of the co-latitude, PZ, by the for-
mulae of Spherical Trigonometry.
An analytical investigation of the formulae by which this pro-
blem is solved shows that errors in the observed altitude and the
time have the less effect upon the result the nearer the body is
to the meridian.
79. Methods of Finding the Latitude at Sea. The second and
the fourth of the methods above described are the methods most
commonly employed in finding the latitude at sea. The sun is
the body which is generally used, its altitude above the sea
horizon being measured with a sexta*nt or an octant. The time of
noon being approximately known, the observer begins to measure
the altitude of the lower limb of the sun a few minutes before
noon, and continues to measure it until the sun ceases to rise, or
"dips," as it is called. The greatest altitude which the sun
attains is considered to be the meridian altitude, although, rigor-
ously speaking, it is not. The proper corrections for index-error,
dip, refraction, parallax, and semi-diameter are next applied to
the sextant reading, and the result is the sun's true meridian
altitude, from which the latitude is obtained by the rule given in
Art. 76.
When cloudy weather prevents the determination of the meri-
dian altitude of either the sun or any other celestial body, an
altitude obtained within an hour of transit, on either side of the
meridian, maybe used to find the latitude by the fourth method,
Art. 78. Bowditch's Navigator contains special tables by which
the computation, particularly when the sun is observed, may bo
greatly facilitated.
80. Reduction of the Latitude.
Owing to the spheroidal form of the
earth, the vertical line at any point
of the surface, as Z' 0' in Fig. 31,
which corresponds exactly with
the normal drawn at that point,
does not coincide with the radius of
the earth, LO, passing through the
point, excepting at the equator
76 LONGITUDE.
and the poles. It is necessary, Jhen, in refined observations, to
distinguish between the geographical zenith, Z 1 ', the point where
the vertical line, when prolonged, meets the celestial spheie, and
the geocentric zenith, Z, the point in which the radius meets the
sphere. Since there are two zeniths, there are also two lati-
tudes : Z' 0' Q, the geographical latitude, and ZOQ, the geocentric
latitude. The geographical latitude is evidently greater than
the geocentric, by the angle OLO', which is called the reduction
of the latitude. Formulae and tables for finding this reduction
are given in Chauvenet's Astronomy. It is only considered in
cases where the highest accuracy in the results is required.
LONGITUDE.
81. Let Fig. 32 represent a projection of the celestial sphere
on the plane of the equinoctial ABCG. P is the projection of
the elevated pole, and PG, PA, and PB are
projections of arcs of great circles of the
sphere passing through the pole. L?t PG
represent the projection of the meridian of
Greenwich, PA that of the meridian of some
other place on the earth's surface, and PJ>
that of the circle of declination passing
Fi - 32 - through some celestial body S. Then will
the angle CPA represent the longitude of the meridian PA
from Greenwich, GPU will represent the Greenwich hour angle
of the body S, and APB will represent its hour angle from the
meridian PA. The difference between these two hour angles is
evidently equal to the longitude of any place on the meridian
PA. The longitude, then, of any place on the earth's surface
is equal to the difference of the hour angles of the same celestial
Lody at that place and at Greenwich, at the same absolute instant
of time. When the Greenwich hour angle is the greater of these
two hour angles, reckoned always to the west, the longitude of
the place is west : when it is the smaller, the longitude is east.
If PB is the hour circle passing through the sun, the longi-
tude of the place is the difference of the solar times at the place
and at Greenwich: if it is the hour circle passing through the
CHRONOMETERS. 77
vernal cqainox, the longitude is the difference of the two side-
real times. In order, then, to determine the longitude of any
place, we nmst be able to determine both the local and the
Greenwich i/me (either sidereal or solar) at the same instant.
There are- various methods of obtaining the local time, one
of which hhs already been described (Art. 20). It may be
noticed here that we are always able, by means of the Nautical
Almanac, to convert sidereal time into solar time, or solar into
sidereal (Art. 105). It remains, then, to determine the Green-
wich time, either sidereal or solar, to do which several distinct
methods may 6e employed.
82. Greenw.ck Time by Chronometers. If a chronometer is
accurately regulated to Greenwich time, that is to say, if the
amount by which it is fast or slow at Greenwich on any day,
and its daily .gain or loss, are determined by observation, the
chronometer can be carried to any other place the longitude
of which is desired, and the Greenwich time which the chrono-
meter gives can be directly compared with the time at that place.
This would be a perfectly accurate method, if the rate of the
chronometer remained constant during the transportation; but,
in fact, the rate of a chronometer while it is carried from place
to place is very rarely exactly the same that it is while the
chronometer is at rest. By using several chronometers, however,
and by transporting them several times in both directions be-
tween the two places, and finally by taking a mean of all the
results, the error may be reduced to a very minute amount.
For instance, the longitude of Cambridge, Mass., was deter-
mined by means of fifty chronometers, which were carried three
times to Liverpool and back, and from them the longitude was
obtained with a probable error of only 4th of a second of time.
83. Greenwich Time by Celestial Phenomena. There are cer-
tain celestial phenomena which are visible at the same absolute
instant of time, at all places where they can be seen at all. Such
are the beginning and the end of a lunar eclipse ; the eclipses
of the satellites of the planet Jupiter by that planet ; the
transits of these satellites across the planet's disc, and their nc-
cultations by it. The Greenwich times at which these various
phenomena will occur arc computed beforehand, and are pub-
78 LUNAR DISTANCES.
Jished in the Nautical Almanac. . The observer, then, to obtain
his longitude, has only to note the local time at which any one
of these phenomena occurs, and to compare that time with the
corresponding Greenwich time given in the Almanac. The dif-
ficulty of determining the exact instant at which these phe-
nomena occur, however, diminishes to some extent the accuracy
of the results. On the other hand, the times of solar eclipses
mid of occultations of stars by the moon, although not identical
at different places, can be very accurately determined : and
iicnce these phenomena are often employed in obtaining longi-
tudes. (Art. 164.)
84. Greenwich Time by Lunar Distances. By the lunar distance
of a celestial body is meant its true angular distance from the
centre of the moon, as it would be seen at the centre of the
earth. The lunar distances of the sun, of the four brightest
planets, and of nine bright stars are given in the Nautical
Almanac, computed for every third hour of Greenwich solar
time. An observer, then, who wishes to determine his longitude,
measures the apparetd angular distance of the moon from some
one of these bodies, and also notes the local time at which the
observation is made. He then finds from this apparent distance,
by means of appropriate formulae and tables, the true geocentric
angular distance, at the time of observation, between the two
bodies. He then enters the table of lunar distances in the
Almanac with this distance, and finds the corresponding Green-
wich time, from which, and the local time noted, he can deter-
mine his longitude.
85. Difference of Longitude by Electric Telegraph. When two
stations, the difference of longitude of which is desired, are
connected by an electro-telegraphic wire, the difference of longi-
tude may be determined by means of signals made at either
station, and recorded at both. Suppose, for instance, there are
two stations A and B, of which A is the more easterly, and
that each station is provided with a clock regulated to its own
local time. Let the observer at A make a signal, the time of
which is recorded at each station. Let A denote the difference
of longitude of the two stations, T the local time at A at which
the signal is made, and T' the corresponding time at B. Since
ELECTRIC SIGNALS. 79
A is to the east of B, its time is greater at any instant tlinn
that of B. We have then, supposing the signal to be recorded
simultaneously at the two stations,
A^r r.
Experience proves, however, that the records of the signal
are not exactly simultaneous, since time is required for the
electric current to pass over the wire. In the example above
given, then, if we denote the time required by the electric fluid
to pass from A to B by x, the time recorded at B will evidently
be, not T', but T' -|- * ; so that the expression for the difference
cf longitude will be
l'=T T' x.
Now let us suppose that instead of the signal's being made
by the observer at .4, it is made by the observer at B, at the
time T'. The corresponding time recorded at A will not be I 7 ,
but T -\- x. In this case, then, the expression for the difference
of longitude will be
r= T+ x r.
Taking the mean of the values of A' and /', we have
I ()! _|_ ;/') = - T T'=L
Any error, therefore, which is caused by the time consumed
by the electric current in passing between two stations is elimi-
nated by determining the difference of longitude by signals made
at both stations, and taking the mean of the results.
86. Difference of Longitude by "Star Signals." The " method
of star signals" is a modification of the method describe^ in
the preceding paragraph, which is extensively used in the
United States Coast Survey. The principle on which this
method rests is that, since a fixed star makes one apparent revo-
lution about the earth in exactly twenty-four sidereal hours,
the difference of longitude between two meridians is equal to
the interval of sidereal time in which any fixed star passes from
one of these meridians to the other. The clock by which this
interval of time is measured may be placed at either station,
or indeed at any place which is in telegraphic communication
with both stations. Two chronographs, one at each station, are
connected with the wire and the clock, and upon them are
SO LONGITUDE AT SEA.
recorded, by breaks in the circuit as explained in Art. 22, the
successive beats of the clock. A transit instrument is adjusted
to the meridian at each station. As the star crosses the several
threads of the reticule of the transit instrument at the eastern
station, the observer, by means of a break-circuit key, records
the instants upon both chronographs. The same process is
repeated as the star crosses the wires at the western station.
Now, it is evident that the elapsed time between the transits at
the two meridians has been recorded upon each chronograph.
Each of these values of the elapsed time is to be corrected for
instrumental errors, errors of observation, and for the gain or
loss of the clock in the interval ; and the mean of the two
values, thus corrected, is taken as the difference of longitude of
the two places.
By making similar observations on several stars on the same
night, by repeating the observations on subsequent nights, by
exchanging observers and using different clocks, and, finally,
by taking a mean of the results, a very accurate determination
of the difference of longitude may be secured.
87. Method of Finding the Longitude at Sea. The method of
finding the longitude at sea which is usually employed is the
method of Art. 82. The Greenwich time is given by chro-
nometers regulated to Greenwich time, and the local time is
obtained from the observed altitudes of celestial bodies. The
sun is the body the altitude of which is most commonly used
for this purpose; but altitudes of the most conspicuous of the
placets and the fixed stars may also be successfully employed.
Altitudes of the moon are to be avoided, except in cases where
no other body is available. At the instant when the altitude
of any celestial body is observed, the time shown by a watch is
noted. This \vatch, either shortly before or after the observa-
tion, is compared with the Greenwich chronometer, and by
means of this comparison the Greenwich time of the observa-
tion is obtained from the time given by the watch. The neces-
sary corrections are applied to the sextant reading to obtain
the body's true altitude. We shall then have, in the triangle
PZS, Fig. 33, the side ZS, the zenith distance of the body, PS
its polar distance, obtained from the Nautical Almanac, and
COMPARISON OF LOCAL TIMES. 81
PZthe co-latitude of the place of observation ;
the latitude being determined by some one of
the methods already given (Art. 79), and being
reduced to the time of observation by the run z>|
of the ship given by the log. In the triangle
PZS, then, having the three sides given, we
can compute the angle SPZ, which is the hour
angle of the body. From this hour angle the Fig 33-
local time can be readily found, from which, and the Greenwich
time already obtained, the longitude may be determined.
In case there is no chronometer on board, the method of
lunar distances is the only regularly available method of deter-
mining the Greenwich time. At the present day, however,
lunar distances are mainly employed as checks upon the chro-
nometer, since any change in the rate of a chronometer will
cause a discrepancy between the Greenwich time shown by the
chronometer and that deduced from observation.
It can be shown, by proper methods of investigation, that
an error in the assumed latitude, or in the body's altitude,
causes the less error in the resulting hour angle the nearer
the body is to the prime vertical. It is best, then, in observing
the altitude of any celestial body for the purpose of obtaining
the local time, to observe it w T hen the body bears nearly east or
west, provided the altitude is not so small as to be sensibly
affected by errors in the refraction. It may also be shown that
in selecting celestial bodies for observations of this character, it
is best, if the other conditions are satisfied, to take those bodies
which have the smallest declinations.
88. Comparison of the Local Times of Different Meridians.
Since the local time, either solar or sidereal, is the greater
at the more easterly of any two meridians, it follows that a
watch or chronometer which is regulated to the time of any
one meridian will appear to gain when carried to the west,
and to lose when carried to the east: the amount of gain or
loss in any case being the difference of longitude, in time,
of the two meridians. A watch, for instance, which gives the
correct solar time at Boston will, even if it really is running
accurately, appear to gain nearly twelve minutes when taken
82 COMPARISON OF LOCAL TIMES.
to New York. If, then, a watch which is regulated to the solar
time of any meridian is carried to the east, the difference of
longitude in time between the meridian left and that arrived
at must be added to the reading of the watch, to obtain tho
time at the second meridian: if it is carried to the west, th<>
difference of longitude must be subtracted.
ECLIPTIC.
THE SUN.
CHAPTER VI.
THE EARTH'S ORBIT. THE SEASONS.
THE ZODIACAL LIGHT.
TWILIGHT.
89. The Ecliptic. IF a great circle on any globe is assumed
to represent the celestial equator, and any point of that circle
is taken to represent the vernal equinox, the relative positions
of all bodies, the right ascension and declination of which are
known, can be plotted upon this globe, and we shall have a
representation of the celestial sphere. The poles of the great
circle will represent the poles of the celestial sphere, and all
great circles passing through these poles will represent circles
of declination. We have seen, in the chapter on Astronomical
Instruments, in what manner the right ascension and the decli-
nation of any celestial body can be determined at any time by
observation. If we thus determine the position of the sun from
day to day, and mark the corresponding points upon our celes-
tial globe, we shall find that the sun appears to move in a great
circle of the sphere from west to east, completing one revolution
in this circle in 365d. 6h. 9m. 9.6s. of our ordinary solar time.
This interval of time is called the sidereal year. The great circle
in which the sun appears to move is called the ecliptic, and the
two points in which it intersects the celestial equator are called
the vernal and the autumnal equinox.
Let Fig. 34 be a representation of
the celestial sphere. EA Q Fis the equi-
noctial, Pp is the axis of the sphere, and
P the north pole. The circle A CVD re-
presents the ecliptic, V the vernal, and
A the autumnal equinox. The sun is
at the vernal equinox on the 21st of
March It thence moves eastward and
northward, and reaches the point C,
84- DISTANCE OF THE SFX.
where it has its greatest northern declination, on the 2 1st of June.
This point is called the northern summer solstice. From this point
it moves eastward and southward, passes the autumnal equinox
A on the 21st of September, and reaches the point D, called the
northern winter solstice, on the 21st of December. It thence
moves towards V, which it reaches on the 21st of t March.
The obliquity of the ecliptic to the equinoctial is the angle
CVty, measured by the arc CQ. This angle or arc is evidently
equal to the greatest declination, either north or south, which
the sun attains, and is found by observation to be about 23 27'.
90. Definitions. The latitude of a celestial body is its angular
distance from the plane of the ecliptic, measured on a great circle
passing through its poles, and called a circle of latitude. In Fig.
34 the arc Ks is the latitude of the body s. The longitude of a
celestial body is the arc of the ecliptic intercepted between the
vernal equinox and the circle of latitude passing through the
body. Thus VK is the longitude of the body s. Longitude is
properly reckoned towards the east.
The hour circle which passes through the solstices, the circle
DHCB, is called the solstitial colure. The hour circle which
passes through the equinoxes is called the equinoctial colure.
91. Signs. The ecliptic is divided into twelve equal parts,
called signs t which begin at the vernal equinox, and are named
eastward in the following order: Aries, Taurus, Gemini, Cancer,
Leo, Virgo, Libra, Scorpio, Sagittarius, Capricornus, Aquarius,
Pisces. Hence the vernal equinox is called the first point of
Aries.
The Zodiac is a zone or belt on the celestial sphere, extend-
ing about 9 on each side of the ecliptic.
DISTANCE OF THE SUN FROM THE EARTH.
92. Relative Distances of the Earth and Venus from the Sun.
It is found by observation that the mean value of the sun's
angular semi-diameter remains constant from year to year,
being always 16' 2". Since any increase or decrease in the
distance of the earth from the sun will evidently be accom-
panied by a corresponding decrease or increase in the sun's
angular semi-diameter, we conclude that the mean distance of
DISTANCE OF THE SUN.
85
the earth from the sun is also constant from year to year. The
distance of tne earth from the sun is obtained by determining
the sun's horizontal parallax from certain observations made
upon the planet Venus. This planet revolves in a nearly cir-
cular orbit about the sun, in a plane only 3 inclined to the
plane of the ecliptic. Its distance from the sun is less than
that of the earth from the sun, and hence it sometimes passes
between the earth and the sun, and is seen apparently moving
across the sun's disc. This phenomenon is called a transit of
Venus. As a preliminary to the determination of the earth's
distance from the sun from one of these transits, it is neces-
sary to obtain the relative distances of Venus and the earth
from the sun. To do this, in Fig. 35 let S
be the sun, E the earth, and W V" V" the
orbit of Venus about the sun. It is evident
that the greatest angular distance (or elon-
gation) of Venus from the sun, the greatest
value, that is, of the angle VES, will occur
when the line from the earth to Venus is
tangent to the orbit of Venus, as repre-
sented in the figure. The orbit of Venus is
not really a circle, but an ellipse, and hence
the distance VS is slightly variable. So,
also, is the distance SE; hence the greatest
elongation is also variable, being found to lie between the limits
of about 45 and 47. Assuming its mean value to be 46, we
have in the right-angled triangle VSE,
VS = SE sin 46 .72 SE.
Neglecting the inclination of the orbit of Venus to the plane
of the ecliptic, we shall have, at the time of a transit, when
Venus is at V'
V'E = .28 SE.
Hence at the time of a transit the distance of Venus from the
sun is to that of Venus from the earth as about 72 to 28.*
* If we know the periodic time of Venus and that of the earth, the ratio
of the distances of these two planets from the sun can be obtained by Kepler's
Third Law (Art. 117), that "the squares of the periodic times of any two
planet* are proportional to the cubes of their mean distances from the sun."
8
86 DISTANCE OF THE SUN.
93. Transit of Venus. In Fig. .36, let S denote the centre of
the sun, and CADN its disc : let V be Venus, and E the centre
Fig. 36.
of the earth. Let HK be that diameter of the earth which is
perpendicular to the plane of the ecliptic, and let an observer be
supposed to be stationed at each extremity. In order to simplify
the explanation, let us neglect the rotation of the earth during
the observation, and suppose Venus to move in the plane of the
ecliptic. To the observer at If, Venus will appear to move
across the sun's disc in the chord CD, and to the observer at JT,
in the chord AB. Regarding VHK and VFG as similar tri-
angles, we have, by Geometry,
FG:HK= GV: 7ff = 72:28
=- HK.
Again, we can obtain the angle which the line FG subtends
at the earth's centre in the following manner. Let the observer
at H note the interval of time in which the planet crosses thf
sun's disc in the chord CD, and the observer at K HIQ interval
in which it moves through the line AB. Since there are tables
which give us the angular velocity, as seen from the earth, both
of the sun and of Venus, we can deduce the angles at the earth's
centre subtended by the chords FB and GD, and knowing also
the angular semi-diameter of the sun, in other words, the angle
at the earth's centre subtended by SB or SD, we can compute
the angles at the earth's centre subtended by FS and GS t and,
finally, the angle subtended by FG.
We have now determined the angle subtended by the line FG,
at a distance equal to that of the earth from the sun, and also
the ratio of FG to the earth's diameter. It is evidently easy to
obtain from these values the angle at the sun subtended by the
.MAGNITUDE OF THE SUN. 87
earth's radius, which angle is the sun's horizontal parallax, ;u*
we have already seen in Art. 54.
Although we have assumed in this discussion that the two ob-
servers are stationed at the extremities of the same diameter, it
is really only necessary that they shall be at two places whose
difference of latitude is large. The earth's rotation and other
things which we have here neglected must be taken into con-
sideration in the practical determination of the sun's parallax.
94. Distance of the Earth from the Sun. The last two transits
of Venus were in 1769 and 1874, and from observations in 1769,
the sun's horizontal parallax was determined to be 8". 6. Later
observations of a different character have given a horizontal
parallax of 8".848,* which is here used. The results of the exten-
sive observations in 1874 cannot yet be given.
From Art. 54, we have for the distance in miles of the earth
from the sun,
d = E cosec P = 3962.8 cosec 8".848 = 92,400,000 miles.
95. Magnitude of the Sun.
The length of the sun's radius
can be at once obtained as soon
as we know its distance from
the earth. Thus, in Fig. 37,
let S be the centre of the sun, ri s- 37 -
and E that of the earth. The angle AES is the apparent semi-
diameter of the sun, which we obtain by observation, its mean
value being, as already stated, 16' 2". We have then, in the
right-angled triangle AES,
SA = 92,400,000 sin 16' 2" = 431,000 miles.
The sun's linear radius, then, is equal to nearly 109 of the earth's
radii; and since the volumes of spheres are proportional to the
cubes of their radii, the volume of the sun bears to that of the
earth the enormous ratio of 1,286,000 to 1.
By observations and calculations which will be described in
fhe Chapter on Gravitation (see Art. 114), the mass of the sun is
found to be about 327,000 times that of the earth; or about 670
times the sum of ihe masses of all the planets of the solar system.
* Determination of Professor Simon Newcomb, Tjnited States Navy. TU
value obtained by Leverrier is 8 x/ .95.
88
ORBIT OF THE EARTH.
THE EARTH'S ORBIT.
96. Revolution of the Earth about the Sun. Up to this point
we have spoken of the apparent animal motion of the sun in the
ecliptic from west to east, as though the earth were really at rest,
and the sun revolved about it in its orbit. But when we take
into consideration the immense mass of the sun compared with
that of the earth, we are almost irresistibly led to conclude that
the apparent annual revolution of the sun is the result, not of the
actual revolution of the sun about the earth, but of that of the
earth about the sun. Such a revolution of the earth, from west
to east,* would give to the sun precisely that apparent motion
in the ecliptic which has been ob-
served. This may be seen in Fig.
38. Let S be the sun, EE'E" the
earth's orbit, and the outer circle
S'S"S'" the great circle in which
the plane of the ecliptic, indefi-
nitely extended, meets the celestial
sphere. When the earth is at E,
the sun will be projected in $';
when the earth is at E', the sun
will be projected in S", &c. ; that
is to say, while the earth moves
Fig. 38.
* Whatever the absolute motion of any celestial body moving in a circle
or an ellipse may be, the appearance presented in that motion will be re-
versed if the spectator moves from one side of the plane in which the
motion is performed to the other. Thus, the apparent daily motion to the
westward of any celestial body is the same as the motion of the hands of a
clock as we look upon its face, to an observer who is on the north side of
the plane of the diurnal circle in which the body moves, as is seen in any
latitude north of 23 27' in the motion of the sun ; while the same west-
ward motion presents the opposite appearance if the ohserveristo the south
of the plane of motion, as may be seen in these latitudes in the case of the
Great Bear. The appearance presented by a motion from west to east is
of course the reverse of this ; hence when we say that the earth or any
other body moves about the sun from west to east, we mean that, to an ob-
server situated to the north of the plane of motion, the body appears to movein a
direction opposite to that in which the hands of a dock move.
ORBIT OF THE EARTH. 89
about the sun in the direction EE'E", the sun will apparently
move about the earth in the same direction, S'S"S'".
Against this theory, then, of the earth's revolution there is
nothing to urge; and analogy gives us a strong argument in
favor of it. Almost every celestial body in which any motion
at all can be detected is found to be revolving about some other
body, larger than itself. The moon revolves about the earth;
the satellites of the planets revolve about the planets ; and the
planets themselves, some of which are much larger than the
earth, and at a much greater distance from the sun, revolve
about the sun. Henceforward, then, we shall include the earth
in the list of planets, and consider the sidereal year to be -the
interval of time in which the earth makes one complete revolu-
tion about the sun.
97. Linear Velocity of the Earth in its Orbit. The number of
miles in the circumference of the earth's orbit, considered as a
circle, is obtained by multiplying the radius of the orbit by 2*.
If we then divide this product by the number of seconds in a
year, we shall have, in the quotient, the number of miles through
which the earth moves about the sun in a second of time. It
will be found to be about 18.4 miles.
98. Elliptical Form of the Earth's Orbit. Although, as has
already been stated, the mean value of the sun's angular semi-
diameter remains constant from year to year, careful measure-
ments of the semi-diameter show that it varies in magnitude
during the year, being greatest about the first of January, and
least about the first of July. The evident conclusion from this
fact is that the distance between the earth and the sun also varies
during the year, being greatest when the sun's semi-diameter is
the least, and least when it is the greatest. The truth of this
conclusion may be seen in Fig. 37, in which we have
AS
sm
As AS of course remains constant, ES will vary inversely as sin
AE/S, or since the sines of small angles are proportional to
the angles themselves, inversely as the angle AES itself. The
angular semi-diameter of the sun is 16' 17". 8, the least
90 ORBIT OF THE EARTH.
is Jo' 45".5: hence the ratio of tfce greatest to the least distance
is that of 16' 17".8 to 15 45".5, or of 1.034 to 1.
Let us now assume any line, SA in Fig. 39, for instance, as our
unit of measure, and prolong it until
SH is to SA as 1.034 is to 1. Then if S
denotes the sun, SA and SH will repre-
sent the relative distances of the earth
from the sun on about the first of Janu-
ary and the first of July. On certain
^ ^ D days throughout the year, let the advance
Fi r 39. of the sun in longitude since the time
when the earth was at A be determined, and let the angular
semi-diameter of the sun on each of these days be measured.
Lay off the angles ASB, ASC, &c., equal to these advances in
longitude. Since, as may readily be seen in Fig. 38, the appa-
rent advance of the sun in longitude is caused by the advance
of the earth in its orbit, and is equal to it, the angles ASB, ASC t
&c., will represent the angular distances of the earth from the
point A on the days when the different observations were made.
Let us next take the lines SB, SC, &c., of such lengths that
each line may be to SA in the inverse ratio of the corresponding
semi-diameters. If, then, we draw a line through the points
A, B, C, &c., we shall have a representation of the orbit of the
earth about the sun. The curve is found to be an ellipse, the
sun being at one of the foci. The point A, where the earth is
nearest to the sun, is called the perihelion, the point H, the aphe-
lion; and the angular distance of the earth from its perihelion
is called its anomaly.
The eccentricity of the ellipse, or if is the centre of the
ellipse, the ratio of OS to OA, is evidently equal to about T ?oV?>
or -g-^th. A more accurate value of it is .0167917. This eccen-
tricity is at present subject to a diminution of .000041 a
century ; but Leverrier, a French astronomer, has proved that
after the eccentricity has diminished to a certain point it w'H
begin to increase again.
THE SEASONS.
99. The change uf seasons on the earth is caused by the
SEASONS.
91
inequality of the days and nights, and this inequality is a result
of the inclination of the plane of the equinoctial to that of the
ecliptic. The relative positions of the sun and the earth at dif-
ferent parts of the year are represented in Fig. 40. S represents
Fig. 40.
the sun, and ABCD the orbit of the earth. Pp is the axis of
rotation of the earth, and EQ the equator. The plane of this
equator is supposed to intersect the plane of the ecliptic in the
line of equinoxes A C. Since, as we have already seen, the sun
appears to be on this line on the 21st of March and the 21st of
September, the earth itself must also be on this line at the same
time. Suppose, then, the earth to be at A on the 21st of March.
The sun will evidently lie in the direction AS, and will be pro-
jected on the celestial sphere at the vernal equinox. Now, since
a line which is perpendicular to a plane is perpendicular to every
line in that plane which is drawn to meet it, the axis Pp at A,
being perpendicular to the equator, is also perpendicular to the
line AS, which is common to both the plane of the equator and
92 SEASONS.
the plane of the ecliptic. Half of each parallel of latitude on
the earth will therefore lie in light and half in darkness ; and
hence, as the earth rotates on the axis Pp, every point on its
surface will describe half of its diurnal course in light and
half in darkness : in other words, day and night will be equal
over the whole earth. Since the direction of the axis of rota-
tion remains unchanged, the same condition of things will occur
when the earth is at C, on the 21st of September. Let the
earth be at B on the 21st of June. Here we see that, as the
earth rotates on its axis Pp, every point on its surface within
the circle ab will lie continually in the light, and will hence
have continual day, while within the corresponding circle a'b'
the night will be continual. We see also that at the equator
the days and nights will be equal, and that every point between
the equator and the circle ab will describe more of its diurnal
course in light than in darkness, and will thus have its days
longer than its nights ; while between the equator and the circle
ab' the nights will be longer than the days. Similar phenomena
will occur when the earth is at D, on the 21st of December,
except only that it will then be the southern hemisphere in
which the days .are longer than the nights, and the southern
pole at which the sun is continually visible.
Such, then, is the inequality of the days and nights caused
by the inclination of the plane of the equinoctial to that of the
ecliptic. As the sun apparently moves from either equinox,
the inequality of day and night continually increases, reaches
its maximum when the sun arrives at either solstice, and then
continually decreases as the sun moves on to the equinox : the
day being longer than the night in that hemisphere which is
on the same side of the equator with the sun. Now, any point
on the earth's surface receives heat during the day and radiates
it during the night : and hence, when the days are longer than
the nights, the amount of heat received is greater than the
amount radiated, and the temperature increases ; while, on the
contrary, when the days are shorter than the nights, the tempe-
rature decreases : and thus is brought about the change of sea-
eons on the earth.
Another fact, depending on the same cause, and tending to
SEASONS. 93
the same result, must also be taken into consideration; and
that is that the temperature at any place depends on the ob-
liquity of the sun's rays : on the altitude, in other words, which
the sun attains at noon. Now we have, from Art. 76,
z = L d:
from which we see that, the latitude remaining constant, the sun
attains the greater altitude, the greater its declination when it
has the same name as the latitude, and the less its declination
when it has the opposite name : so that the nearest approach to
vertically in the sun's rays will occur at the same time that
the day is the longest. An exception, however, must be noticed
to this general rule, in the case of places within the tropics :
since at these places, as may be seen from the formula, the sun
passes through the zenith when its declination is equal to the
latitude, and has the same name.
100. Effect of the Ellipticity of the Earths Orbit on the Change
of Seasons. The elliptic form of the earth's orbit has very
little to do with the change of seasons. For although the earth
is nearer to the sun on the 1st of January than on the 1st of
July, yet its angular velocity at that time is found by observa-
tion to be greater, and to vary throughout the whole orbit in-
versely as the square of the distance. Now it may readily be
shown that the amount of heat received by the earth at different
parts of its orbit also varies, other things being equal, inversely
as the square of the distance : so that equal amounts of heat
are received by the earth in passing through equal angles of
its orbit, in whatever part of its orbit those angles may be
situated. Still, although the change in distance does not mate-
rially affect the annual change of seasons, it does affect the
relative intensities of the northern and the southern summer.
The southern summer takes place when the earth's distance is
only about f|jths of what it is at the time of the northern
summer: hence, the intensity at the former period will be to
that at the latter in the ratio of about (|$) 2 to 1, or about }| to
1 : in other words, the intensity of the heat of the southern sum-
mer will be y^th greater than that of the heat of the northern
summer.
94 TWILIGHT.
TWILIGHT.
101. If the earth's atmosphere did not contain particles of
dust and vapor, which serve to reflect the rays of light, the
transition from day to night would be instantaneous, and the
intermediate phenomenon of twilight would have no existence.
This phenomenon
is explained in
Fig. 41, in which
ABC represents
B<^ / x \ a portion of the
earth's surface,
Fig- 4i. & and EDF a por-
tion of the atmosphere. Let the sun be supposed to lie in the
direction AS, and to be in the horizon of the place A. All of the
atmosphere which lies above the horizontal plane SD will then
receive the direct rays of the sun, and A will receive twilight
from the whole sky. The point B will, on the contrary, be illu-
minated only by the smaller portion of the atmosphere included
within the planes EB and AD and the curved surface ED; and
at the point C the twilight will have wholly ceased. Strictly
speaking, the lines AS, BE, &c., should be slightly curved, owing
to the effects of refraction, but the omission involves no change
in the explanation.
It is computed that twilight ceases when the sun is about 18
below the horizon, measured on a vertical circle. The more
nearly perpendicular to the horizon is the diurnal circle in
which the sun appears to move, the more rapid will be the sun's
descent below the horizon ; hence, the length of twilight dimin-
ishes as we approach the equator and increases as we recede
from it. Furthermore, we see in Fig. 2 that the greater the
declination of the sun, the smaller is the apparent diurnal circle
in which it moves, and the greater will be the length of time
required for the sun to reach the depression of 18 below the
horizon. The shortest twilight, therefore, occurs at places on the
equator, when the sun is on the equinoctial, and its length is
then Ih. 12m. Near the poles the length of twilight is at times
very great. Dr. Hayes, in his last expedition towards the North
APPEARANCE OF THE SUN. 95
P^le, wintered at latitude 78 18' N., so far above the circle ab,
Fig. 40, that the sun was continually below the horizon from the
noddle of October to the middle of February; but at the begin-
ning and the end of this interval twilight lasted for about nine
hours. At the poles twilight lasts nearly a month and a half.
GENERAL DESCRIPTION OF THE SUN.
102. When the sun is observed with a telescope, spots are
noticed upon its surface. These spots appear to cross the sun's
disc from east to west, and with different rates, the rate of
motion of spots at the sun's equator being the greatest. We
therefore conclude that these spots have not only an apparent
rsotion, caused by the sun's rotation, but also a proper motion
of their own. By appropriate investigation of these motions,
it is found that the sun rotates from west to east upon a fixed
axis, in a plane inclined at an angle of about 7 to the plane of
the ecliptic. The period of this rotation is about 25 days.
Much uncertainty exists as to the nature of these spots. Un-
til recently, it was held that the sun is surrounded by two
atmospheres, of which only the outer one (called the photo-
sphere} is luminous, and that the spots are rents in these
atmospheres through which the solid body of the sun is seen.
These spots are for the most part confined to a zone, extending
about 35 on each side of the sun's equator. They differ widely
iii duration, sometimes lasting for several months, and some-
times disappearing in the course of a fe^ hours. They are
sometimes of an immense size. One was seen in 1843, with
a diameter of nearly 75,000 miles : it remained in sight for
a week, and was visible to the naked eye. In 1858, a much
larger one was seen, its diameter being over 140,000 miles. As
a general thing, each dark spot, or umbra, as it is called, has
within it a still darker point, called the nucleus, and is sur-
rounded by a fringe of a lighter shade, called the penumbra.
Sometimes several spots are inclosed by the same penumbra;
and occasionally spots are seen without any penumbra at all.
On the theory of two atmospheres, the existence of the
penumbra is explained by supposing the aperture in the outer
and luminous stratum to be wider fb;.n that in the inner one,
96 APPEARANCE OF THE SUN.
and that portions of the inner ^tratum, being subjected to a
strong light from above, are rendered visible: the umbra itself
being, as already remarked, the solid body of the sun seen through
both strata. According to Mr. J. N. Lockyer, "sun-spots are
cavities qr hollows eaten into the photosphere, and these different
shades [the penumbra, umbra, and nucleus] represent different
depths." [See Note, page 99.]
One very curious and interesting discovery in relation to these
spots is that of a periodicity in their number. This discovery
was made by Schwabe, of^Dessau, whose researches and obser-
vations on this subject covered a period of more than twenty-five
years. The number of groups of spots which he observed in a
year varied from 33 to 333, the average being not far from 150.*
He found the period from one maximum to another to be about
ten years. Professor Wolf, of Zurich, after tabulating all the ob-
servations of spots since 1611, decided that the period varied from
eight to sixteen years, its mean value being about eleven years.
Recent investigations show that this periodicity is in some way
connected with the action of the planets, of Jupiter and Venus
particularly, upon the sun's photosphere. It is a curious fact that
magnetic storms and the phenomenon called Aurora or Northern
Lights have a similar period, and are most frequent and most
striking when the number of the solar spots is the greatest.
Still other phenomena which are seen upon the sun's disc are
the faculce, which are streaks of light seen for the most part in
the region of the spots, and which are undoubtedly elevations or
ridges in the photosphere: and the luculi, which are specks of
light scattered over the sun's disc, giving it an appearance not
unlike that of the skin of an orange, though relatively much less
rough. The cause of these lucuii is unknown.
At the time of a total eclipse of the sun by the moon, the disc
of the sun is observed to be surrounded by a ring or halo of light,
which is called the corona. The breadth of this corona is more
than equal to the diameter of the sun. Many theories have been
advanced to explain this phenomenon, one of which is that it is
due to the existence of still another atmosphere, exterior to the
* A table of Schwnbe's observations is given in the Appendix.
CONSTITUTION OF THE SUN. 97
photosphere. Another theory is that this corona consists of
streams of luminous matter, radiating in all directions from the
sun. Rose-colored protuberances, sometimes called red flamea,
are also seen, which are usually of a conical shape, and are
sometimes of great height. In the total eclipse of August 17th,
1868, one was observed with an apparent altitude of 3', corre-
sponding to a height of about 80,000 miles. These protuberances
were formerly supposed to be similar in character to our terres-
trial clouds; but Dr. Jannsen, the chief of the French expedi-
tion sent out to the East to observe the total eclipse of August,
1868, examined their light with the spectroscope, and found them
to be masses of incandescent gas, of which the greater part was
hydrogen. Dr. Jannsen also made the interesting discovery that
these protuberances can be examined at any time, without wait-
ing for the rare opportunity afforded by a total eclipse. He
observed them for several successive days, and found that great
changes took place in their form and size. Mr. Lockyer, of
England, who has since examined them, pronounces them to be
merely local accumulations of a gaseous envelope completely
surrounding the sun : the spectrum peculiar to these protuber-
ances appearing at all parts of the disc.
It has already been stated (Art. 47) that the spectroscope en-
ables us to establish the existence of certain chemical substances
in the sun, by a comparison of the spectra of these substances
with that of the sun ; or, more precisely, by a comparison of the
lines, bright or dark, by which these different spectra are dis-
tinguished. The number of the parallel dark lines in the solar
spectrum which have been detected and mapped exceeds 3000;
and careful examination also shows that some of these are double.
3ome of the more prominent of these lines have received the
names of the first letters of the alphabet; D, for example, is a
very noticeable double line in the orange of the spectrum. When
certain chemical substances are evaporated, either in a flame or
by the electric current, the spectra which they form are also
characterized by lines, which, however, are not dark, but bright.
If, for instance, sodium is introduced into a flame, its incan-
descent vapor produces a spectrum which is characterized by a
brilliant double band of yellow; and it is especially noticeable
98 CONSTITUTION OF THE SUN.
that this yellow band coincides, exactly in position with the
dark line D of the solar spectrum. In the same way the
spectrum of zinc is found to contain bands of red and blue-
that of copper contains bands of green: and, in general, the
spectrum of each metal contains certain bright bands or lines,
peculiar to itself, and readily recognized. We may therefore
conclude that an incandescent gas or vapor emits rays of a certain
refrangibility and color, and those rays only.
Again, it is proved by experiment that if a ray of white light
be allowed to pass through an incandescent vapor, the vapor
will absorb precisely those rays which it can itself emit. If, for
instance, a continuous spectrum be formed by a ray of intense
white light from any source, and if the vapor of sodium be intro-
duced in the path of this ray, between the prism and the source
of light, a dark band will appear in the spectrum, identical in
position with the bright yellow band which we have already
noticed in the spectrum of sodium, and which we found to be
identical in position with the dark line D of the solar spectrum.
We are now ready to apply the principles established by
these experiments to the case of the sun. The sun is, as we
saw above, a sphere surrounded by a vaporous envelope. This
sphere would of itself emit all kinds of rays, and therefore
give a continuous spectrum ; but the photosphere which sur-
rounds it absorbs those of the sun's rays which it can itself
emit. The dark line D of the solar spectrum shows, as in the
experiment above described, that sodium has been introduced
in the path of the sun's rays : in other words, that sodium is in
the sun's photosphere. In the same way, Professor Kirchhoff,
to whom we owe this remarkable discovery, has established the
existence in the photosphere of iron, calcium, magnesium, chro-
mium, and other metals. In the case of iron, more than 450
bright lines have been detected in its spectrum : and for every
one of these lines there is a corresponding dark line in the solar
spectrum.
We also see, from the preceding experiments, how the presence
of bright lines in the spectrum of the rose-colored protuberances
could prove to Dr. Jannsen that these protuberances were not
masses of cloud.?, reflecting the light of the sun, but masses of
ZODIACAL LIGHT. 99
ircandescent vapor. We shall see another instance of the same
description when we come to examine some of the nebulae.
THE ZODIACAL LIGHT.
103. At certain seasons of the year a faint nebulous light,
not unlike the tail of a comet, is seen in the west after twilight
has ended, or in the east before it has begun. This is called
the Zodiacal Light. Its general shape is nearly that of a cone,
the base of which is turned towards the sun. The breadth of
the base varies from 8 to 30 of angular magnitude. The apex
of the cone is sometimes more than 90 to the rear or in advance
of the sun. According to Humboldt, it is almost always visible,
at the times above stated, within the tropics: in our latitudes it
is seen to the best advantage in the evening near the first of
March, and in the morning near the middle of October.
Of the many theories proposed to account for the zodiacal
light, the one which seems to be most widely accepted is that it
consists of a ring or zone of rare nebulous matter encircling
the sun, which reaches as far as the earth, and perhaps extends
beyond it. According to another theory, it is a belt of meteoric
bodies surrounding the sun. A very interesting and valuable
series of observations upon the. Zodiacal Light was made by
Chaplain Jones, United States Navy, in the years 1853-5, in
latitudes ranging from 41 N. to 53 S, The conclusion which
he drew from his observations was that the light was a nebulous
ring encircling the earth, and lying within the orbit of the moon.
NOTE. The surface of the sun is now the object of assiduous observa-
tion and study. The shining surface of the sun, whence come our light
and heat, is called the photosphere. Outside of this is the chromosphere, to
which the red flames belong, and which is largely composed of hydrogen
and the vapors of metals. Outside of the chromosphere lies the corona.
Modern research has disproved much that was formerly believed concern-
ing the physical constitution of the sun and its envelope; but it has by no
means established what that constitution really is.
SIDEREAL AND SOLAR TIMES.
CHAPTER VII.
SIDEREAL AND SOLAR TIME. THE EQUATION OF TIME. THE
CALENDAR.
104. Sidereal and Solar Days. IT is important to distin-
guish between the apparent annual motion of the sun in the
ecliptic, from west to east, and the apparent diurnal motion
towards the west, which the rotation of the earth gives to all
celestial bodies and points. A sidereal day is the interval of
time between two successive transits of the vernal equinox over
the same branch of the meridian. A solar day is the interval
between two similar transits of the sun. But the continuous
motion of the sun towards the east causes it to appear to move
more slowly towards the west than the vernal equinox moves.
The solar day is therefore longer than the sidereal day, the
average amount of the difference being 3m. 55.5s. And fur-
thermore, in the interval of time in which the sun makes one
complete revolution in the ecliptic, the number of daily revo-
lutions which it appears to make about the earth will be less
by one than the number of daily revolutions made by the
equinox. The sidereal year, then (Art. 89), which contains
865d. 6h. 9m. 9.6s. of solar time, contains 366d. 6h. 9m. 9.6s.
of sidereal time. [See Note, page 154.]
105. Relation of Sidereal and Solar Times. Since the side-
real day is shorter than the solar day (and, consequently, the
sidereal hour, minute, &c., than the solar hour, minute, &c.), it
is evident that any given interval of time will contain more
units of sidereal than of solar time. The relative values of the
sidereal and the solar days, hours, &c., are obtained as follows:
We have from the prec2ding article,
366.25G36 sidereal days = 365.25636 solar days:
one sidereal day = (5.99727 solar day,
one sidereal hour = 0.99727 solar hour, &c.
EQUATION OF TIME. 101
Having, therefore, an interval of time expressed in either solar
or sidereal units, we may easily express the same interval in
units of the other denomination. This is called the conversion
of a solar into a sidereal interval, and the reverse : and tables
for facilitating this conversion are given in the Nautical Al-
manac.
Again, knowing the sidereal time at any instant, the hour-
angle, that is to say, of the vernal equinox, the corresponding
solar time, or the hour-angle of the sun, is readily obtained by
subtracting from the sidereal time the sun's right ascension.
This is indeed a corollary of the theorem proved in Art. 9,
from which we see that the sum of the sun's right ascension
(which can always be found in the Nautical Almanac), and
its hour-angle, is the sidereal time. Either of these times, then,
may be converted into the other. \ "* /
THE EQUATION O
106. Inequality of Solar Days. Observation shows that the
length of the solar day is not a constant quantity, but varies at
different seasons of the year, and, indeed, from day to day. A
distinction must therefore be made between the apparent or
actual solar day, and the mean solar day, which is the mean
of all the apparent solar days of the year. A uniform measure
of time may be obtained from the apparent diurnal motion
with reference to our meridian of a fixed celestial body or
point. It may also be obtained from the apparent diurnal
motion of a celestial body which changes its position in the
heavens, provided that two conditions are satisfied ; first, the
plane in which the body moves must be perpendicular to the
plane of the meridian: and second, its motion in that plane
must be uniform. Both these conditions are so very nearly
satisfied by the motion of the vernal equinox, that any two
sidereal days may be considered to be sensibly equal to each
other; but neither condition is satisfied by the motion of the
sun. It moves in the ecliptic, the plane of which is not, in
general, perpendicular to the plane of the meridian : and its
motion in this plane is not uniform. We have, therefore, two
102 EQUATION OF TIME.
causes of the inequality of the soltir days, the effect of each of
which we will now proceed to examine.
107. Irregular Advance of the Sun in the Ecliptic. Observa-
tion shows that the sun's motion in longitude is not uniform.
The mean daily motion is, of course, obtained by dividing 360
by the number of days and parts of a day in a year, and is
59' 8."3. But the daily motion about the first of January is
61' 10", while about the first of July it is only
57' 12". In Fig. 42, let the circle AM'M"
represent the apparent orbit of the sun in
the ecliptic about the earth E, and let the
sun be supposed to be at the point A where
its daily motion is the greatest, on the first
of January. Let us also suppose a fictitious
^si^n (which we will call the first mean sun)
to niqye in the ecliptic with the uniform rate of 59' 8". 3 daily,
iik.H'l t ; > )>o ul, the. jximj.4 a ^ tne sanie time that the true sun is
there. On the next day the mean sun will have moved eastward
to some point M, while tli3 true sun, whose daily motion is at this
time greater than that of the mean sun, will be found at some
point T, to the east of M. The true sun will continue to gain on
the mean sun for about three months, at the end of which time
the mean sun will begin to gain on the true sun, and will finally
overtake it at the point B, on the first of July. During the
second half of the year the mean sun will be to the east of the
true sun, and at the end of the year the two suns will again be
together at A.
The angular distance between the two suns, represented in
the figure by the angles TEN, T'EM', &c., is called the Equa-
tion of the Centre. It is evidently additive to the mean longi-
tude of the sun while it is moving from A to B, and subtractive
from it while it is moving from B to A. Its greatest value is
about 8 minutes of time.
Since the rotation of the earth gives to both these bodies a
common daily motion to the west, it is plain that from January
to July the mean sun will cross the meridian before the true
sun, and that from July to January the true sun will cross the
meridian before the mean sun.
EQUATION OF TIME. 103
108. Obliquity of trie Ecliptic to the Meridian. Even if the
sun's motion in the ecliptic were uniform, equal advances of the
sun in longitude would not be accompanied by equal advances
in right ascension, in consequence of the obliquity of the
ecliptic to the meridian. The truth of this may be seen in
Fig. 43. Let this figure represent
the projection of the celestial sphere
on the plane of the equinoctial co-
lure PApH. A and H are the
equinoxes, P and p the celestial
poles, AeH the equinoctial, and
A EH the ecliptic. Let the ecliptic
be divided into equal arcs, AB, BC,
&c., and through the points of divi-
sion, B, C, &c., let hour-circles be
drawn, meeting the equinoctial in
the points b, c, &c. Now, since all great circles bisect each
other, AEH is equal to AeH, and if Pep is the projection of an
hour-circle perpendicular to the circle PApH, AE and Ae are
quadrants, and equal. The angle PBC is evidently greater
than PAB, PCD is greater than PBC, &c. : in other words, the
equal arcs AB, BC, &c., are differently inclined to the equi-
noctial. The effect of this is that the equinoctial is divided
into unequal parts by the hour-circles Pb, PC, &c., be being
greater than Ab, cd than be, &c. It is to be noticed, further,
that the points B and b, being on the same hour-circle, will be
on the meridian at the same instant of time: and the same is
true of C and c, D and d, &c.
Now, if A is the vernal equinox, the first mean sun, moving
in the ecliptic with the constant daily rate of 59' 8". 3, will
pass through that point on the 21st of March. Let another
fictitious sun (called the second mean sun) leave the point A at
the same time, and move in the equinoctial with the same uni-
form daily rate. Since BAb is a right-angled triangle, Ab is
less than AB. Hence, when the first mean sun reaches B, the
second mean sun will be at some point m, to the east of b:
when the first mean sun is at C, the second mean sun will be to
the east of c, &c. : and the second mean sun will continue to
104 EQUATION OF TIME.
lie to the east of the first mean sun until the 21st of June (the
summer solstice), when both suns will be at the points E and e
at the same instant of time, and will therefore come to the
meridian together. In the second quadrant, the second mean
sun will lie to the west of the first mean sun, and both suns
will reach H, the autumnal equinox, on the 21st of September.
The relative positions in the third and the fourth quadrant will
be identical with those in the first and the second.
From the 21st of March, then, to the 21st of June, the second
mean sun, being to the east of the first mean sun, will come
later to the meridian ; and the same will also be true from the
21st of September to the 21st of December. In the two other
similar periods the case will be reversed, and the second mean
sun will come earlier to the meridian than the first mean sun.
The greatest difference of the hour-angles of these two mean suns
is about 10 minutes of time.
109. Equation of Time. It is by means of these two fictitious
suns that we are able to obtain a uniform measure of time from
the irregular advance of the sun in the ecliptic. The second
mean sun satisfies the two conditions stated in Art. 106, and
therefore its hour-angle is perfectly uniform in its increase.
This hour-angle is the mean solar time of our ordinary watches
and clocks. The hour-angle of the true sun is called the ap-
parent solar time: and the difference at any instant between the
apparent and the mean solar time is called the equation of time.
Let Fig. 44 be a projection of the
celestial sphere on the plane of the
horizon. Z is the zenith, P the
pole, EVQ the equinoctial, CL the
ecliptic, and Fthe vernal equinox.
Let T be the position of the true
sun in the ecliptic, and M that of
second mean sun in the equinoctial.
The angle TPM is evidently the
equatioi of time. This angle is mea-
sured by the arc AM, or VM VA :
the difference, that is, of the right ascensions of the true and
tbe second mean sun. But since the angular advance of the
JALEKDAR. 105
second mean sun in the equinoctial is, by hypothesis, as shown
in the previous article, equal to the angular advance of the first
mean sun in the ecliptic, it follows that the right ascension of
the second mean sun is always equal to the longitude of the
first mean sun, or, as it is usually called, the true sun's mean
longitude. The equation of time, then, is the difference of the
sun's true right ascension and mean longitude; and thus com-
puted is given in the Nautical Almanac for each day in the
year. It reduces to zero four times in the year, and passes
through four maxima, ranging in value from 4 minutes to 16
minutes.
110. Astronomical and Civil Time. The mean solar day is
considered by astronomers to begin at mean noon, when the
second mean sun (usually called simply the mean sun) is at its
upper culmination. The hours are reckoned from Oh. to 24h.
The mean solar day, so considered, is called the astronomical day.
The civil day begins at midnight, twelve hours before the
astronomical day, and is divided into two parts of twelve hours
each, called A.M. and P.M.
We must, therefore, carefully distinguish between any given
civil time and the corresponding astronomical time. For in-
stance, January 3d, 8 A.M., in civil time, is the same as Janu-
ary 2d, 20h., in astronomical time.
THE CALENDAR.
111. Owing to causes which will be explained further on, the
position of the vernal equinox is not absolutely stationary, but
moves westward along the ecliptic, with an annual rate of about
50". 2. The sun, then, moving eastward from the equinox, will
reach it again before it has made one complete sidereal revo-
lution about the earth. This interval of time in which the sun
moves from and returns to the equinox is called a tropical year,
and consists of 365d. 5h. 48m. 47.8s. The Julian Calendar
was established by Julius Csesar, 44 B.C., and by it one day was
inserted in every fourth year. This was the same thing as as-
suming that the length of the tropical year was 365d. 6h.,
instead of the value given above, thus introducing an accumu-
lative error of llm. 12s. overy year. This calendar was
106 CALENDAR.
adopted by the Church in 325 A.p., at the Council of Nice, and
the vernal e juinox then fell on the 21st of March. In 1582,
the annual error of llm. 12s. caused the venial equinox to fall
on the llth of March, instead of the 21st. Pope Gregory XIII.
therefore ordered that ten days should be omitted from the year
1582, and thus brought the vernal equinox back again to the
21st of March. Furthermore, since the error of llm. 12s. a year
amounted to very nearly three days in 400 years, it was decided
to leave out three of the inserted days (called intercalary days)
every 400 years, and to make this omission in those years which
were not exactly divisible by 400. Thus of the years 1700,
1800, 1900, 2000, all of which are leap years according to the
Julian calendar, only the last is a leap year according to the
reformed or Gregorian calendar. By this calendar the annual
error is only 24 seconds, and will not amount to a day in much
less than 4000 years.
This reformed calendar was not adopted by England until
1752, when eleven days were omitted from the calendar. The
two calendars are now often called the old style and the new style.
For instance, April 26th, O.S., is the same as May 8th, N.S. In
Russia the old style is still retained, though it is customary to
give both dates ; as 1868, ^?. All other Christian countries
have adopted the new style.
UNIVERSAL GRAVITATION. 107
CHAPTER VIII.
LAW OF UNIVERSAL GRAVITATION. PERTURBATIONS IN THE
EARTH'S ORBIT. ABERRATION.
112. The Law of Universal Gravitation. The earth, as we
have seen in Chapter VL, revolves about the sun in an elliptical
orbit, with a linear velocity of eighteen miles a second. At every
point of its orbit the centrifugal force induced by this revolution
must create in the earth a tendency to leave its orbit, and to go
off in the direction of a tangent to the orbit at that point. To
counteract this centrifugal force, there must constantly exist a
centripetal force, by which the earth is at every instant deflected
from this rectilinear path which it tends to follow, and is drawn
towards the sun ; and in order that the orbit of the earth may
remain unchanged in form, as observation shows that it does
remain, these two forces must be in constant equilibrium. Ad-
mitting, then, the existence of such a centripetal force, it remains
to determine the nature of the force, and the laws under which
it acts.
The force is believed to be identical in nature with that force
which causes all bodies, free to move, to tend towards the earth's
centre, and which we call the force of gravity. At whatever
height above the surface of the earth the experiment may be
made, this attractive force of the earth is found to exist ; and
there is no good reason for assuming any finite limit beyond
which this force, however much its effects may be lessened by
other and opposing forces, does not have at least a theoretic
existence. And, furthermore, as the sun and the other heavenly
bodies are all masses of matter like the earth, there is every
reason for concluding that they too, as well as the earth, possess
this power of attracting other bodies towards their centres. Nor
is this attractive power a characteristic of large bodies alone : for
108 UNIVERSAL GRAVITATION.
we have already seen in the experiment with the torsion balance,
described in Art. 66, that small globes of lead exert a sensible
attraction upon still smaller globes. We may therefore assume
that what is true of each of these masses, large and small, as a
whole, is no less true of the separate particles of which it is com-
posed, and that every particle of matter in the universe has an
attractive power upon every other particle.
In order to determine the laws under which this attractive
power is exerted, we have only to assume that the laws which
are shown by experiment to obtain at the earth's surface hold
equally good throughout the universe; so that whatever the
masses of bodies may be, or whatever the distances by which
they are separated from each other, the forces with which any
two bodies attract a third will be directly proportional to the
masses of the two attracting bodies, and inversely proportional
to the squares of their distances from the third body.
This, then, is Newton's Law of Universal Gravitation. Every
particle of matter in the universe attracts every other particle,
ivith a force directly proportional to the mass of the attracting
particle, and inversely proportional to the square of the distance
between the particles. In applying this general law to the par-
ticles which compose the masses of the heavenly bodies, Newton
has demonstrated that the attraction exerted by a sphere is pre-
cisely what it would be if all the particles in the sphere were
collected at its centre, and constituted one particle, with an at-
tractive power equal to the sum of the powers of these different
particles.
113. Verification of the Law in the Case of the Moon. The
moon is shown by observation to revolve about the earth in a
period of 27.32 days, at a mean distance from the earth of 238,800
miles. If we take the formula for centrifugal force given in
Art. 69,
and substitute for r the moon's distance in feet, and for t its
period of revolution in seconds, we shall find for the centrifugal
force,
/= 0.0089 feet:
)
MASS OF THE SUN. 109
that is to say, in one second the earth tends to give the moon a
velocity towards itself of 0.0089 feet. Now the force of gravity
on the eartn's surface at the equator is 32.09 feet; and if the law
of gravitation is assumed to be true, the force of gravity at the
32 09
distance of the moon will be - feet, since the distance of
(oO.Zo7)
the moon from the earth is equal to 60.267 of the earth's radii.
The value of this expression is found to be 0.0088 feet. The two
results vary by only joio^h of a foot: and it is therefore fair to
conclude that the centrifugal force of the moon in its orbit is
really counteracted by the earth's attraction.
In whatever way the law of gravitation is tested in connection
with the observed motions of the heavenly bodies, the facts which
come by observation are always found to be in close agreement
with the results which the law demands ; and it is safe to say
that the truth of this law is as satisfactorily demonstrated as is
that of the laws of refraction, of the laws of sound, or of the
many other natural laws which depend upon observation and
experiment for their ultimate proof.
114. The Mass of the Sun. Let A denote the attraction ex-
erted by the sun on the earth, and a that exerted by the earth
on a body at its surface. Let If denote the mass of the sun, m
that of the earth, r the radius of the earth, and R the radius
of the earth's orbit. We have, then, by the law of gravitation,
A M r 2
a m R 2
But A must equal the earth's centrifugal force in its orbit, or
. 8 in which t is 365.256 days, reduced to seconds, and R is
expressed in feet. We have also a equal to 32.09 feet. Substi-
tuting these values, we have,
m ~ 32.09f r 2
Substituting the known values of the different quantities, we
shall have
= 327,000:
m
or the- mass of the sun is equal to that of 327,000 earths.
Jo
110 MOTION OF THE EARTH
The. density of the sun, compared with that of the earth, being
327,000
equal to the mass divided by the volume, is ro
density is therefore equal to about Hh of that of the earth, and
to about f ths of that of water.
115. Weight of Bodies at the Surface of the Sun. The weight
of the same body at the surface of the earth and at that of the
sun will be directly as the masses of the two spheres and inversely
as the squares of their radii. We shall find that the weight
of a body at the sun is about 27.7 times its weight at the earth;
so that a body which exerts a pressure of 10 pounds at the earth
would exert a pressure at the sun equal to that of 277 of the
same pounds; and a man whose weight is 150 pounds would,
if transported to the sun, be obliged to support in his own body
a weight equivalent to about two of our tons.
116. The Earth's Motion at Perihelion and Aphelion. We
have already seen that the angular velocity of the earth in its
orbit is the greatest at perihelion, when the earth is the nearest to
the sun, and is the least at aphelion, when the earth is the farthest
from the sun. This irregularity of motion is a consequence of
the attraction exerted by the sun on the earth, as may be seen in
Fig. 45. In this figure, let S be the sun,
P the perihelion of the earth's orbit, and
A the aphelion. Let the earth move
from A to P, and suppose it to be at the
point E. The attraction of the sun on
the earth, along the line ES, may be re-
solved into two forces, one of which,
acting in the direction of the tangent EB,
B will evidently tend to increase the velo-
Fig. 45. city of the earth in its orbit. At the
point E", on the contrary, where the earth is moving toward A,
the effect of the sun ? s attraction is to diminish the earth's velocity.
lu general, then, the earth's velocity will increase as it moves
from aphelion to perihelion, and decrease as it moves from peri-
helion to aphelion.
KEPLER'S LAWS. Ill
KEPLER S LAWS.
117. In the early part of the seventeenth century, more than
tifty years before the announcement by Newton of the law of
universal gravitation, the astronomer Kepler, by an examination
of the observations which had been made upon the motions of the
planets, and which had shown that the planets revolved about
the sun, discovered the following laws :
(1.) The orbit of every planet is an ellipse, having the sun at
one of its foci.
(2.) If a line, called a radius vector, is supposed to be drawn
from the sun to any planet, the areas described by this line, as
the planet revolves in its orbit, are proportional to the times.
(3.) The squares of the times of revolution of any two planets
are proportional to the cubes of their mean distances from the sun.
These laws were verified by Newton in his Principia, in a
course of mathematical reasoning, the foundation of which was
his theory of universal gravitation. With regard to Kepler's
first law, he showed that any two spherical bodies, mutually at-
tracted, describe orbits about their common centre of gravity,
and that these orbits are limited in form to one or another of the
four conic sections, the circle, the ellipse, the parabola, and the
hyperbola. For instance, in the case of the earth and the sun,
the earth does not describe an ellipse about the sun at rest, but
both earth and sun revolve about their common centre of gravity.
It is shown in Mechanics that the common centre of gravity of
any two globes is at a point on the straight line joining their in-
dependent centres of gravity, so situated that its distances from
the centres of the two globes are inversely as the masses of the
globes. Hence the distance of the common centre of gravity
of the earth and the sun from the centre of the sun is ' '
oJ7,U()0
miles, or only about 280 miles ; so that the sun may practically
bo considered to be at rest.
With regard to Kepler's second law, Newton further showed
that the angular velocity with which the radius vector moves
must be inversely proportional to the square of its length.
112 PRECESSION.
Finally, he proved also the tru^h of the third law, provided
only that a slight correction is introduced when the mass of the
planet is not so small as to be inappreciable in comparison with
that of the sun. If t and t' denote the times of revolution of
any 'two planets, m and m' their masses (the mass of the sun
being unity), and d and d' their mean distances from the sun,
Newton showed that we shall always have the following pro-
portion :
I + m' 1 + m'
If m and m' are so small that they may be omitted without
sensible error, this proportion becomes identical with Kepler's
third law.
PERTURBATIONS IN THE EARTHS ORBIT.
118. Precession. Although the absolute positions of the
planes of the ecliptic and the equinoctial in space, and their re-
lative positions to each other, remain very nearly the same from
year to year, there are nevertheless certain small perturbations
in these positions which are made evident to us by refined and
extended observations. The principal of these perturbations is
called precession.
The latitudes of all the fixed stars remain very nearly the
same from year to year, and even from century to century: and
we therefore conclude that the position of the ecliptic with
reference to the celestial sphere remains very nearly unchanged.
But the longitudes of the stars are all found to increase by an
annual amount of 50".2: and hence the line of the equinoxes
must have an annual westward motion of the same amount.
This westward motion is called the precession of the equinoxes.
Since the ecliptic remains stationary in the heavens (or at least
so nearly stationary that the latitudes of the stars only vary
by half a second of arc in a year), this precession must be con-
sidered to be a motion of the equinoctial on the ecliptic.
In Fig. 46, let EQ represent the equinoctial, and LC the eclip-
tic. .BFis the line of the equinoxes, which moves about in the
plane of the ecliptic, taking in course of time the new position
B'V. Perhaps the clearest conception of this motion is ob-
PRECESSION.
113
tained by considering P, the pole of
the equinoctial, to revolve about A,
the pole of the ecliptic, in the circle
PG (the polar radius of which, AP,
is 23 27'), moving westward in this
circle with the annual rate of 50".2,
and completing its revolution in
25,817 years.
A general explanation of the
cause of precession may be given by
means of Fig. 47. The earth may
be regarded as a sphere surrounded by a spheroidal shell, as
represented in the
figure by EPQp,
and the matter in
this shell may be
considered to form
a ring about the
earth in the plane
of the equator, as
shown in E'FQ'p'.
It is to the attrac-
tion of the sun and
the moon on this
ring, combined with
the earth's rotation,
that the precession
of the equinoxes is
due. In the figure
let S be the sun, the
circle ABV the ecliptic, and E"Q" this equatorial ring of the
earth. Let J.CTbe the plane of the equinoctial, meeting the
plane of the ecliptic in the line of equinoxes A V. This plane
ij> by definition determined at each instant by the position of
the earth's equator. The attraction exerted by the sun upon
the different particles of the ring in that half of it which is
nearer the sun (the particle E", for instance), may be resolved
into two forces, one acting in the plane of the equator, and the
Fig. 47.
114 PRECESSION.
other in a direction perpendicular 4;o that plane, or in the direc-
tion E"d. The sun's attraction upon the nearer half of the
ring, then, tends to draw the plane of the ring nearer to the
plane of the ecliptic. On the other hand, the sun's attraction
upon the farther half of the ring tends to bring about the
opposite result ; but since, by the law of attraction, the latter
effect is less than the former, we may consider the whole result
of the sun's attraction upon the ring to be a tendency in the
plane of the ring to come nearer to the plane of the ecliptic.
Therefore, if the ring did not rotate, the plane of the earth's
equator would ultimately come into coincidence with the plane
of the ecliptic.
But the ring does rotate, about an axis perpendicular to its
own plane ; and the combined result of this rotation and of the
rotation about the line of the equinoxes, above described, is
that the plane of the equinoctial, while it preserves constantly
its inclination to the plane of the ecliptic, moves about in a
westerly direction: the line of intersection of the two planes
also moving about in the same direction, and thus giving rise to
the precession of the equinoxes.
Similar results will evidently follow if S represents the moon
instead of the sun. Owing to the greater proximity of the
moon to the earth, however, the results of its attraction are
more than double those of the attraction of the sun. There is
still another perturbation in the position of the line of the equi-
noxes which is a result of the mutual attraction between the
earth and the other planets. This attraction tends to draw the
earth out of the plane of the ecliptic, without affecting in any
way the position of the plane of the equinoctial. The result is
an annual movement of the equinoxes towards the east. This
perturbation is exceedingly minute, being only about yth of a
second of arc in a year. The value 50". 2 is the algebraic sum
of all these perturbations.
119. Results of Precession. One result of precession is to
make the interval of time between two successive returns of the
sun to the vernal equinox less than the time of one sidereal
revolution, by the time required by the sun to pass over 50". 2,
which is 20m. 21.8s. Hence we have the tropical year, to which
NUTATION. 115
reference has already been made in Art. 111. Another result
is that the signs of the Zodiac (Art. 91) no longer coincide with
the constellations after which they are named, but have retreated
towards the west by about 28, or nearly one sign : so that the
constellation of Aries now lies in the sign of Taurus. Still
another result is that the same star is not the pole-star in dif-
ferent ages. Referring to Fig. 46, the pole of the heavens, P,
will have revolved about A to the position G, in the course of
about 13,000 years; and a star of the first magnitude, called
Vega, which is now about 51 from the pole, will at that time be
less than 5 from the pole, and will be the pole-star.
120. Nutation. Since precession is the result of the tendency
of the sun to change the position of the plane of the equator, it
is evident that there will be no precession when the sun is itself
in the plane of the equator, in other words, at the equinoxes,
and that the precession will be at its maximum when the sun is
the farthest from the plane of the equator: that is to say, is at the
solstices. The amount of precession due to the influence of the
moon is subject, to a similar variation, being the greatest when
the moon's declination is the greatest. The result is that the
pole of the heavens has a small oscillatory motion about its
mean place. This motion is called nutation. If the effect of
nutation could be separated from that of precession, the pole
would be found to move in a very minute ellipse, having a
major axis of 18". 5, and a minor axis of 13". 7, the period of
one revolution in this ellipse being about nineteen years. Since,
however, these two perturbations co-exist, the result is that the
pole of the heavens revolves about the pole of the ecliptic, not
in a circle, but in an undulating curve, as
represented in Fig. 48 : the amount of the
deviation being very much exaggerated in
the figure.
121. Change in the Obliquity of the Eclip-
tic. It was stated in Art. 118 that the lati-
tudes of the stars were found to vary from
year to year by a very minute amount.
This change in the latitudes is due to a change in the position
of the plane of the ecliptic, involving a change in the obliquity
116 ABERRATION.
of the ecliptic. The obliquity .of the ecliptic in 1878 was
23 27' 18": and the annual amount of diminution to which it
is now subject is 0".46. Mathematical investigations show that
after certain moderate limits have been reached this diminution
will cease, and the obliquity will begin to increase. The arc
through which the obliquity oscillates is about 1 21', and the
time of one oscillation is about ten thousand years.
122. Advance of the Line of Apsides. The line connecting
the earth's perihelion and aphelion is called the line of ajisides.
This line revolves from west to east, with an annual rate of 11". 8;
a perturbation due to the attraction exerted on the earth by the
superior planets. The time in which the earth moves from peri-
helion to perihelion is called the anomalistic year (from anomaly,
Art. 98). It is evidently longer than the sidereal year, and is
found to contain 365d. 6h. 13m. 49.3s.
ABERRATION.
123. The apparent direction of a celestial body is determined
by the direction of the telescope through which it is observed.
In consequence of the motion of the earth, and the progressive
motion of light, the telescope is carried to a new position while
the light is descending "through it, and therefore the apparent
direction of the body will differ from its true direction.
\? In Fig. 49, let OF be the posi-
tion of the axis of a telescope at
the instant when the rays of light
from the star S reach the object
glass 0. The rays, after passing
through the glass, begin to con-
verge towards a fixed point in
space, with which, at this instant,
the intersection of the cross-wires
Fig. 49. coincides. Let the earth be moving
in the direction FA. Since the transmission of light is not
instantaneous, time is required for the light to pass from to
the fixed point in space, and in that time the earth will carry
the axis of the telescope to some new position 0'F f . The cross-
wires will then be at F' t while the rays, whose motion in space
ABERRATION. 117
is en f irely independent of any motion of the telescope, will tend
to meet at the point F. In order, then, to have the image of the
star coincide with the intersection of the wires, the telescope
must be so moved that its axis will lie in the position O'F. The
star will then appear to lie in the direction FSi, while its true di-
rection is of course FS: and the angle which these two directions
make with each other, or the angle F' O'F, is called the aberra-
tion. Representing this angle by A, and the angle OFF' , the
angle between the apparent direction of the star and the direc-
tion in which the earth is moving, by I, we shall have,
sin 4: BinI=FF f : O'F'.
But the ratio FF' : O'F' is the ratio between the velocity of
the earth and that of light : so that the sine of the aberration is
equal to the ratio of the velocity of the earth to that of light,
multiplied by the sine of the angle J.
124. Diurnal Aberration. Aberration causes the celestial
bodies to appear to be nearer than they really are to that point
of the celestial sphere towards which the motion of the earth
is directed at the instant of observation. As a correction, then,
it is to be applied in the opposite direction. There is evidently
no aberration when the motion of the earth is directly towards
the star, and the greatest amount of aberration occurs when
the direction of the earth's motion is at right angles to the
direction of the star.
Aberration is of two kinds, corresponding to the daily and
the yearly motion of the earth. The diurnal aberration tends
to displace all bodies in the direction in which the earth is
carrying the observer : that is to say, in an easterly direction.
It evidently varies -with the linear velocity of the observer, and
is therefore the greatest at the equator and zero at the poles.
Owing to the minuteness of the velocity of any point of the
earth's surface about the axis in comparison with the velocity
of light, the diurnal aberration is extremely small, its greatest
value being less than Jd of a second of arc.
125. Annual Aberration. The displacement of a star occa-
sioned by the motion of the earth in its orbit about the sun is
called the annual aberration. The effect which it has on the mo-
tion of any body will depend on the relative situation of that body
118
ABERRATION.
to the plane of the ecliptic, as ma^r be seen in Fig 50. In thia
figure /S represents the sun, ABCD the orbit of the earth, and K
the pole of the ecliptic. Suppose a star to be at K. As the earth
moves through A, in the direction indicated by the arrow, the
star will be displaced from Kiv a; as the earth moves through
B, the star will be seen
at b, &c. Since the
direction of this star is
always at right angles
to the direction in
which the earth is
moving, the aberra-
tion will continually
be at its maximum,
as shown in the pre-
vious article, and the
star will describe a
circle about its true
place as a centre. If
the star is in the plane
of the ecliptic, as at s, there will be no aberration when the
earth is at A or (7, and the aberration will be at its maximum
when the earth is at B or D. The star will therefore during
the year describe the arc b'd', equal in value to twice the maxi-
mum of aberration, and having the true place of the star at its
middle point. If the star is situated between the pole and the
plane of the ecliptic, it will describe an ellipse, the semi-major
axis of which is the maximum of aberration, and the semi-
minor axis of which increases with the latitude of the star.
126. Velocity of Light. The maximum value of aberration is
the same for all bodies, and may be obtained by observing the
apparent motion of a fixed star during the year. Its value
has thus been obtained, and is 20". 4. Now, since the maximum
of aberration occurs when the angle J, in the formula in Art.
123, is 90, we shall have, denoting this maximum by A' t
A> FF '
sin A - - Q,p,-
But FF' is the velocity of the earth in its orbit, or 18.4 miles
ABERRATION. H9
a second. Hence, the velocity of light in a second is 18.4
miles multiplied by the cosecant of 20".4, which will be found
to be 185,600 miles. Experiments of a totally different character
have given almost precisely the same result ; and it is believed
that this estimate is within a thousand miles of the true velocity.
If we divide the disr.uice of the earth from the sun by this
velocity, we find that it requires 8m. 18s. for light to pass over
that distance. When we look at the sun, therefore, we see it,
not as it is at the time of observation, but as it was 8m. 18s.
previously; and in the same way every other celestial body
appears to be in a different position from that which it really
occupies at the instant we observe it. It may be well to notice
here, that the time required for light to pass from any celestial
body to the earth is an element in the computation of the appa-
rent place of that body given in the Nautical Almanac. In
the case of a body which changes its actual position on the celes-
tial sphere, as a planet, for instance, allowance must also be made
for what is called planetary aberration ; since even if the earth
were stationary, the apparent position of the body would be
behind its true position by the amount of its motion in the time
required for light to come from the body to the earth.*
127. Aberration a Proof of the Earth's Revolution about the
Sun. The existence of the phenomenon of aberration, as de-
scribed in Art.. 125, is a matter of undoubted observation : and
when the close agreement of the velocity of light obtained in
the preceding article with the velocity obtained by independent
philosophical experiments is taken into consideration, it is fair
to regard the existence of aberration as a strong direct proof of
the revolution of the earth about the sun. Another proof, simi-
lar in many respects to this, will be noticed when we come to
the subject of the eclipses of Jupiter's satellites.
* Herschel suggests (Outlines of Astronomy, % 385) that this might be
called the equation of light, in order to prevent its being confounded with tho
real aberration of light.
120 ORBIT OF THE ITOCXN.
CHAPTER IX.
THE MOON.
128. The Orbit of the Moon. While the moon, in common
with all the celestial bodies, has the apparent westward motion
which is due to the rotation of the earth, it also changes its rela-
tive position to the other bodies, and is continually falling behind,
or to the east of them, in this diurnal motion. In other words,
it has an independent motion, either real or apparent, from west
to east. This eastward motion is so rapid, that we only need to
observe the relative situations of the moon and some conspicuous
star, during a few hours on any favorable night, to notice a per-
ceptible change in their angular distance. If the right ascension
and the declination of the moon are determined from day to day,
precisely as the same elements of the sun's position were deter-
mined (Art. 89), and the corresponding positions are laid down
upon a celestial globe, we shall find that the moon makes a com-
plete revolution in the heavens, about the earth as a centre, in
an average period of 27d. 7h. 43m. 11.5s. We shall also find
that the plane of the moon's orbit intersects the plane of the
ecliptic at an angle whose mean value is 5 8' 44", and in a line
which, like the earth's line of equinoxes, is continually revolving
towards the west : so that the apparent orbit of the moon is not
a circle, but a kind of spiral. This revolution is much more
rapid, however, in the case of the moon, the amount of retro-
gradation being about 1 27' in a month, and the complete revo-
lution being effected in 18.6 years.
The movement of the moon in its orbit is represented in Fig.
51. Let E be the earth, and the circle MANC the plane of the
ecliptic. Let the moon be at J/at any time. Then will MN be
the line in which the plane of the moon's orbit intersects the
plane of the ecliptic. This liiie is calk d the line of the nodes. That
ORBIT OF THE MOON. 121
extremity of the line through which the moon passes in moving
from the southern to the northern
side of the ecliptic is called the
ascending node, the other the de-
scending node. Let the moon
move on from M in the arc MB.
When it descends to the ecliptic,
it will meet it, not at the point N,
but at some point N'. and the line
of the nodes will take the new posi-
tion N'M'. The moon moves on to the other side of the ecliptic,
passes through the arc N'D, and when it again returns to the
ecliptic, will meet it, not at M f , but at some point M", and the
line of the nodes will take the position M"N". The revolution
of the line of the nodes is evidently in an opposite direction to
that in which the moon itself revolves, and is therefore from
east to west.
129. Cause of the Retrogradation of the Nodes. This retro-
grade movement of the moon's nodes is similar in character to
the precession of the equinoxes, and is due to the attraction
which the sun exerts upon the moon. Since the plane of the
moon's orbit is inclined to the plane of the ecliptic, the attrac-
tion of the sun will, in general, tend to draw 7 the moon out of its
orbit towards the ecliptic. The only exceptions to this rule will
occur when the moon is at one of its nodes, and is therefore i.i
the plane of the ecliptic, and also when the line of the moon's
nodes passes through the sun, at which time the attraction of the
sun is exerted along this line, and consequently in the plane of
the moon's orbit. In Fig. 51 let the moon be at B, and the sun
anywhere in the ecliptic except on the line of the nodes. As the
moon moves on, the sun is continually drawing it down to the
ecliptic, and it will hence meet the ecliptic, not at N, but at jY'.
The same effect will be seen at every other position of the moon
in its orbit, with only the exceptions already mentioned.
130. Change in the Obliquity of the Moon's Orbit. It is evi-
dent from the same figure that the angle which the arc BN'
makes with the plane of the ecliptic is greater than the angle
which an arc drawn through B and N would make. The obli-
11
122 ORBIT OF THE MOOX.
quity of the plane of the moon's orbit is therefore increased a*
the moon approaches the node. It may be shown in the same way
that the obliquity is diminished as the moon recedes from the node.
The extreme limits which this angle attains are 5 20' 6" and
4 57' 22".
131. Elliptical form of the Moon's Orbit. The angular dia-
meter of the moon varies at different points of its orbit, while
its mean value remains the same from month to month ; we there-
fore conclude, as we concluded in the case of the sun, that its
distance from the earth is not constant, the greatest distance cor-
responding to the least diameter, and the least distance to the
greatest diameter. If we neglect the retrogradation of the
moon's nodes, and represent graphically the moon's orbit by a
method identical with the method employed in representing the
earth's orbit (Art. 98), we shall find the orbit to be an ellipse,
with the earth at one of the foci. The eccentricity of the ellipse
is 0.0549, or very nearly -j^th.
132. Line of Apsides. That point in the moon's orbit where
it is the nearest to the earth is called the perigee, and that point
where it is the farthest from the earth, the apogee. The line
connecting these two points is called the line of apsides. It is
also the major axis of the moon's orbit. This line revolves in the
plane of the moon's orbit from west to east, making a complete
revolution in very nearly nine years.
The following description of the moon's orbit, and of the
changes to which it is subject, is given by Herschel in his Out-
lines of Astronomy. " The best way to form a distinct conception
of the moon's motion is to regard it as describing an ellipse about
the earth in the focus, and at the same time to regard this ellipse
itself to be in a twofold state of revolution; 1st, in its own
plane, by a continual advance of its own axis in that plane;
and 2dly, by a continual tilting motion of the plane itself,
exactly similar to, but much more rapid than, that of the earth's
equator."
133. Variation in the Moons Meridian Zenith Distance. From
the formula in Art. 76 we have,
z--=L d
At any place, then, the latitude remaining constant, the least
DISTANCE OF THE MOON.
123
meridian zenilh distance will occur when the moon's declination
has the same name as the latitude, and is at its maximum ; and
the greatest will occur when the declination has the opposite
name, and is also at its maximum. Since the plane of the
moon's orbit is inclined, at the most, 5 20' to the plane of the
ecliptic (Art. 130), the greatest value of the declination, either
north or south, is 5 20' -f- 23 27'. The variation in the meri-
dian altitude will therefore be double this amount, or 57 34'. At
Annapolis, in latitude 38 59' N., the greatest altitude is 79 48',
the least 22 14'. There is an exception to this general rule in
the case of those places whose latitude is less than 28 47': since
at those places the greatest altitude occurs when the moon is in
the zenith, or, as is evident from the formula, when the declina-
tion is equal to the latitude, and has the same name.
The new moon is in the same part of the heavens that the sun
is in (Art. 139), and the full moon is in the opposite part. Since
the sun attains its least altitude in winter and its greatest in
summer, new moons will run low in winter and full moons will
run high : while in summer the opposite of this will take place.
DISTANCE, SIZE, AND MASS OF THE MOON.
1 34. Since the sine of the moon's horizontal parallax is the
ratio of the radius of the earth to the distance of the nioon from
the earth, it is evident that we can determine this distance as
soon as we obtain the horizontal parallax. The horizontal
parallax may be found in the following manner: In Fig. 52, let
be the centre of the earth, EQ its equator, and A and B the
positions of two observers on the same meridian, whose zeniths
124 DISTANCE OF THE MOON.
are Z and Z '. Let M be the mood's position when crossing the
meridian. The apparent zenith distance at A, corrected for
refraction, is the angle ZAM, the geocentric zenith distance is
ZOM, and the difference of these two angles, the angle A MO,
is the parallax in altitude. In the same way OMB is the pa-
rallax at B. Represent the parallax at A by p, that at B by
p, the horizontal parallax by P, the apparent meridian zenith
distance at A by z, and that at B by z'.
We have, by Geometry,
p = z A M,
p' = z' BOM,
and, consequently,
" p + p f = z + z' AOB.
We have also, from Art. 54,
p = P sin z,
p' = P sin z',
and, therefore,
p -f- p' = P (sin z -f sin z').
Combining the two equations, and finding the expression for P,
_ g + z' A OB
sin z -j- sin z'
But A OB is evidently the difference of latitude of A and B.
We have, then, as our method of finding the moon's horizontal
parallax, to subtract the difference of latitude of the two places
from the sum of the apparent zenith distances, and to divide
the remainder by the sum of the sines of the two zenith dis-
tances.
It is important that the two places of observation shall
differ widely in latitude. It is not, however, necessary that
they shall be on the same meridian, since, either from tables
of the moon's motion, or from actual observation on successive
days before and after the time of observation, we can obtain
the change of meridian zenith distance corresponding to any
known difference of longitude, and thus reduce the two observed
zenith distances to the same meridian.
135. The Moon's Horizontal Parallax. By observations simi-
lar to those above described, the mean value of the moon's
equatorial horizontal parallax is found to be 57' 3". The mean
MAGNITUDE AND MASS. 125
distance of the moon from the earth is therefore 3962.8 miles
multiplied by the cosecant of 57' 3", or 238,800 miles. The hori-
zontal parallax varies between the limits of 61' 32" and 52' 50",
and the distance between 257,900 and 221,400 miles. It must
be noticed that by the mean value of the horizontal parallax
given above is not meant the half sum of the two extreme
values, but the value which the parallax has when the moon is
at its mean distance from the earth.
136. Magnitude of the Moon. The angular semi-diameter of
the moon at its mean distance from the earth is found to be
15' 33."5. Its linear semi-diameter is therefore obtained by
multiplying the mean distance by the sine of 15' 33". 5, and
is found to be 1080.8 miles, or about T 3 T ths of the radius of the
earth. The volumes of two spheres being to each other as the
cubes of their radii, the volume of the moon will be found to
be about ^th of that of the earth.
137. Mass of the Moon. The mass of the moon is obtained
by the following considerations. If the sun does not affect the
gravity of the moon to the earth, and the mass of the moon is
inappreciable in comparison with that of the earth, then the
centrifugal force of the moon in its orbit ought exactly to equal
the attraction of the earth on the moon. But if the moon has
a sensible mass, it will, by the law of gravitation, attract the
earth, and its centrifugal force must be sufficient to counter-
balance the sum of the mutual attractions of the earth and
the moon. Now, if we refer to what was demonstrated in Art.
113, we find that the moon's actual centrifugal force is greater,
by -g^th, than the attraction of the earth at the distance of the
moon. This would make the mass of the moon -^gth of that of
the earth. But it is found that the sun diminishes sensibly the
gravity of the moon to the earth. This, therefore, must also be
taken into account, and the resulting value of the mass of the
moon is found to be about -g-'jSt of that of the earth.
The density of the moon, being directly as the mass, and
inversely as the volume, will be |f, or about |ths of the density
of the earth.
138. Augmentation of the Moon's Semi-Diameter. If at any
lime we measure the angular semi-diameter of the moon, we
126 PHASES.
shall find that it increases with the moon's altitude, being least
when the moon is in the horizon and greatest when in the
zenith. This increase is explained in Fig. 53. Let E be the
centre of the earth, and
M that of the moon. With
the distance between jand
M as a radius, describe the
semi-circumference AM' B.
When the moon is in the
horizon of the point C, its
distances from C and from
E are very nearly equal.
53. But as the moon rises, the
distance CM continually decreases, while EM, the distance of the
moon from the earth's centre, remains sensibly constant. When
the moon is in the zenith, or at M', the distance CM' is less than
EM' by the radius of the earth. Now, the angular semi-diame-
ter of the moon will increase, as shown in Art. 98, very nearly
as the distance of the moon from the observer decreases. But
the earth's radius is about ^ O th of the distance of the moon
from the earth's centre: therefore the semi-diameter of the
moon in the zenith will be greater than the semi diameter in
the horizon by -g-^th of itself, or by about 15". This increase
is called the augmentation of the moon's semi-diameter.
THE MOON'S PHASES.
139. Two bodies are said to be in conjunction when they have
the same longitude. They are said to be in opposition when
their longitudes differ by 180 ; and in quadrature when their
longitudes differ by either 90 or 270.
The moon is an opaque body, which is rendered visible to
us by the rays of light which it reflects from the sun. The
phases of the moon are due to the different relative positions
to the sun and the earth which it has while revolving about
the earth.
In Fig. 54 let #be the earth, and the circle ACFH the orbit
of the moon. Since the inclination of the plane of the moon's
orbit to the plane of the ecliptic is only a few degrees, we may
PHASES.
127
neglect it in this case, and suppose the two planes to coincide.
Let the sun lie in the direction ES. Since the distance of the
Fig. 54.
sun from the earth is about 387 times the distance of the moon
from the earth, the lines JES, ff/S, J3S, &c., drawn to the sun
from different points of the moon's orbit, may be considered to be
sensibly parallel. Let us first suppose the moon to be in con-
junction with the sun at the point A. Here only the dark
portion ot the moon is turned towards the earth, and the moon
is therefore invisible. This is called new moon. As the moon
moves on towards B, the enlightened part begins to be visible,
and when it reaches C, 90 in longitude from the sun, half the
enlightened part is visible, and the moon is at its first quarter.
When the moon is at F, in opposition to the sun, all the illumi-
nated part is turned towards the earth, and the moon is full.
The moon wanes after leaving F, passes through its laat quarter
at ff, and finally becomes again invisible.
Between A and C the moon is crescent, as represented at L,
and between C and F it is gibbous, as represented at N. The
same terms are also applied to the appearance of the moon be-
tween H and A and between F and H.
140. Phases of the Earth to the Moon. It is evident from Fig.
54 that the earth presents phases to the moon identical in cha-
racter with those presented by the moon to the earth, although
128
SIDEREAL AND SYNODICAL PERIODS.
similar phases are Dot presented by each body at the same time.
Thus at the time of new moon tlie earth is full to the moon :
and the light which it then reflects to the moon renders the
unenlightened part of the moon faintly visible to the earth. As
the moon moves on to its first quarter, the earth reflects less and
less light to it, until finally the unenlightened portion disappears.
SIDEREAL AND SYNODICAL PERIODS.
141. The sidereal period of the moon is the interval of time
in which it makes one complete revolution in its orbit about
the earth. The synodieal period (or lunation) is the interval
between two successive conjunctions or oppositions. Owing to
the earth's revolving about the sun, and carrying the moon with
it, the synodieal period is longer than the sidereal period, as may
be seen in Fig. 55.
Let S be the sun, E the
earth, and MANB the or-
bit of the moon. Let the
moon be at M, in conjunc-
tion with the sun. As the
moon moves about E in
the curve MANB, the
earth also moves about the
sun in the direction EE'.
The next conjunction will
therefore not occur until the
moo;n reaches M". Now,
if through E' we draw the
line M'N' parallel to MN t the sidereal period of the moon is
completed when the moon reaches M'. The synodieal period is
therefore greater than the sidereal period by the time required
by the moon to pass through the angle M'E'M". This angle is
evidently equal to the angle ESE', which is the angular advance
of the earth in its orbit in the period of one synodieal revo-
lution of the moon. In one lunar month, then, the angular ad-
vance of the moon in its orbit is greater by 360 than the angu-
lar advance of the earth in its orbit. If, therefore, we denote
the moon's sidereal period in days by P, its synodieal period by
Fig. 55.
SIDEREAL AND SYNODICAL PERIODS. 129
S, and the earth's sidereal period, or one sidereal year, by T, we
shall have,
360
- = the earth's daily angular velocity,
360
p = the moon's daily angular velocity,
360
- = the moon's daily angular gain on the earth,
Hence we shall have,
360 360 360.
>
P T S
ST
~ S+T
The sidereal period of the moon is therefore obtained by mul-
tiplying the sidereal year by the moon's synodical period, and
dividing the product by the sum of the sidereal year and the
synodical period.
142. Values of the Synodical and Sidereal Periods. The value
of the synodical period is not constant, but varies from month
to month. A mean value may, however, be obtained by divid-
ing the interval of time between two oppositions, not conse-
cutive, by the number of synodical revolutions in that interval.
Now, the day, the hour, and even the probable minute, at which
an opposition of the moon occurred in the year 720 B.C., were
recorded by the Chaldseans; and by comparing this time with
the results of recent observations, an extremely accurate value
of the mean synodicaT period is obtained It is found to be
29d. 12h. 44m. 3s. We have, then, for the value of the side-
real period, by the formula in the preceding article,
_ 365.256 X 29.53
~ 3657256 -r- 29.53 JS
whence we obtain the value already given in Art. 128.
143. Retardation of the Moon, and the Harvest Moon. The
mean daily motion of the moon towards the east is about 13,
while that of the sun is, as we have already seen, about 1:
hence the moon is continually falling to the rear of the sun in
apparent westward motion, and the interval of time between any
two successive transits of the moon is greater than the similar
1<50 ROTATION OF THE MOON.
interval in the case of the sun. r he moon, therefore, rises later,
and sets later, day by day. This is called the retardation of the
moon. Its amount varies considerably in value, but is on the
average about fifty minutes.
The less the angle which the plane of the moon's orbit makes
with the plane of the horizon, the less does the advance of the
moon carry it with reference to the horizon, and, consequently,
the less is the retardation of the moon in rising. Now, since
the moon's orbit very nearly coincides with the ecliptic, the
retardation in rising will in general be the least, when the
ecliptic makes the least angle with the horizon. By reference
to a celestial globe, it will be seen that the ecliptic makes the
least angle with the horizon when the vernal equinox is in the
eastern horizon. The least retardation in rising, therefore,
occurs in each month when the moon is near the sign of Aries.
This least retardation is especially noticeable when it occurs at
the time of full moon. Now, when the moon is in Aries, and
full, the sun must be in Libra, or near the autumnal equinox.
This occurs about the 21st of September. About the time, then,
of the full moon which occurs near the 21st of September, the
moon will rise, for two or three nights, only about half an hour
later each night. Usually this small retardation is noticed at
the times of two full moons, one in September and the other in
October. The first is called the Harvest Moon, the second the
Hunter's Moon. All this relates to the Northern Hemisphere.
ROTATION. LIBRATIONS AND OTHER PERTURBATIONS.
144. Rotation of the Moon. By observation of the spots upon
the disc of the moon, it is found that very nearly the same
surface of the moon is turned continually towards the earth.
The conclusion drawn from this fact is that the moon rotates
upon an axis in the same time in which it revolves about the
earth, or in 27.3 days. The plane in which this rotation is
performed makes an angle of about 1 32' with the plane of the
ecliptic.
If there are any inhabitants of the moon, their day will be
equal in length to about twenty-nine of our days, and their
ni^ht to about twenty-nine of our nights. Since the plane of
LIBRATIONS OF THE MOON.
131
the moon's equator is so nearly coincident with the plane of tho
ecliptic, there will hardly be any sensible change of seasons :
or if there is, the lunar day will be the lunar summer, and the
night the winter. To the inhabitants of one hemisphere the
earth will be perpetually invisible, while to the inhabitants of
the other hemisphere it will present the appearance of a. body
very nearly stationary in their sky, exhibiting phases similar
to those which we see in the moon, with a radius nearly four
times that of the moon, and a surface about thirteen times that
of the moon.
145. Librations. By libration is meant an apparent oscilla-
tory movement of the moon, which enables us, in the course of
its revolution, to see something more than an exact hemisphere.
The libration in longitude is due to the fact that the moon's
rotation on its axis is perfectly uniform, while its motion about
the earth is not. Hence the line drawn from the centre of the
Fig. 56.
earth to that of the moon does not always intersect the surface
of the moon at the same point, and we are able at times to look
132 OTHER PERTURBATIONS.
a few degrees, east or west, beyond the mean visible border. If,
in Fig. 56, ABCD represents the earth, E its centre, and R
the centre of the rnoon, the dotted lines at iV denote the limits
between which, as the moon revolves about the earth, the visible
border may deviate from its mean position.
The libration in latitude is due to the fact that the axis of the
moon, remaining constantly parallel to itself, is not perpen-
dicular to the plane of the moon's orbit, but is inclined to it at an
angle of about 83 19'. We are therefore able at certain times
to see about 6 41' beyond the north pole of the moon, and at
other times the same amount beyond the south pole. Thus in
Fig 56, when the moon is at M, we can see beyond the pole P,
and when the moon is at 0, beyond the pole p: since in each
case we can see nearly that portion of the moon which lies be-
tween the earth and the circle ab, whose plane is perpendicular
to the plane of the moon's orbit.
The diurnal libration is due to the difference between that
hemisphere of the moon which is turned towards the centre of
the earth and that which is turned towards any point on the
surface. When, for instance, the moon is at Z/, an observer at
C will see the same hemisphere which is turned towards the
earth's centre, while an observer at G will see a different one.
The hemisphere which is turned towards any observer when
the moon is rising will also be different from the one which is
turned towards him when the moon is setting. It is evident in
the figure that the amount of this libration varies with the angle
ERG; that is to say, with the moon's parallax.
Notwithstanding all these librations, we are able to see in all
only about fV ths of the moon's surface, according to Arago:
the remainder being continually concealed from our view.
146. Other Perturbations. Besides these librations, and the
perturbations already mentioned (Art. 132), there are other per-
turbations in the moon's longitude of which only a very brief notice
can here be given. The greatest of these perturbations is called
evection, and was discovered by Ptolemy in the second century.
It arises from the variation in the eccentricity of the moon's
orbit, and from the fluctuations in the general advance of the
line of the apsides. By it the moon's mean longitude is alternately
LUNAR CYCLE. 133
increased and decreased by about 1 20'. Another perturbation
in the moon's motion is called variation. It depends solely on
the angular distance of the moon from the sun, and its maximum
is 37'. The annual equation depends on the variable distance
of the earth from the s'in, and amounts to 11'. The secular acce-
leration is an increase in the moon's motion which has been going
on for many centuries, at the rate of about 10" a century. This
perturbation is partly due to the diminution of the eccentricity
of the earth's orbit; and from what has been said on that subject
in Art. 98, it is evident that this inequality will at some distant
day become a secular retardation. [See Note, page 154.]
All of these perturbations are satisfactorily explained by the
investigation of what is known as the problem of the three bodies,
in which two bodies are supposed to revolve about their common
centre of gravity, according to the law of universal gravitation,
and the effects of the attraction exerted by a third body upon
the motions of these two bodies are made the object of mathe-
matical examination.
THE LUNAR CYCLE.
147. If we multiply the number of days, hours, &c., in a
synodical period of the moon (Art. 142) by 235, the product
will be 6939d. 16h. 27m. 50s. Now, in a period of nineteen civil
years there are either 6939 days, or 6940 days, according as there
are four or five leap years in that period. If, then, in any year,
new moon occurs on any particular day of the month, the first
of January, for instance, it will occur again on the first of Janu-
ary (or at all events within a few hours of its end or beginning),
after an interval of nineteen years ; and all the new moons and
the other phases will occur on very nearly the same days through-
out the second period of nineteen years on which they occurred
during the first period. This period is called the Lunar Cycle.
It is also called the Metonic Cycle, having been originally dis-
covered, B.C. 432, by Meton, an Athenian mathematician. The
present lunar cycle began in 1862.
This cycle is used in finding Easter: Easter being the first
Sunday after the full moon which occurs either upon or next
after the 21st day of March.
134 APPEARANCE OF THE MOON.
The golden number of any ye%r is the number which marks
the place of that year in the cycle. It may be found for any
year by adding 1 to the number of that year, and dividing the
sum by 19 ; the remainder (or 19, if there is no remainder) is
the golden number.
Four lunar cycles, or seventy-six civil years, constitute what
is called the Callippic cycle.
GENERAL DESCRIPTION OF THE MOON.
148. When viewed through powerful telescopes, the surface
of the moon is found to be made up of mountains, valleys, and
plains, similar in general appearance to those that exist on the
earth. As a whole, however, the surface of the moon is much
more uneven than that of the earth. The heights of over 1000
lunar mountains have been measured, and some of them have
been found to exceed 20,000 feet. Many of these mountains
bear the appearance of having been at one time volcanoes, far
surpassing in size and activity those on the earth. The common
belief among astronomers seems to be that these lunar volcanoes
are now extinct. Messrs. Beer and Madler, two Prussian astron-
omers who have made the moon their special study, have de-
tected no signs of activity in any of the volcanoes which they have
examined. A few years ago, certain phenomena were noticed
which seemed to show that one at least of these volcanoes,
named Linne", is not extinct : but later observations do not confirm
this suspicion.
There are no signs of the existence of water on the moon.
Certain large dark patches are seen, which were formerly con-
sidered to be oceans, gulfs, &c., and were so named ; but increased
telescopic power shows that they are dry plains.
It seems to be still an open question whether or not the moon
has an atmosphere. If there is an atmosphere, it must be of an
extremely minute height and density ; for we see no clouds and
no twilight, and there is nothing in the phenomena of the occul-
tations of stars by the moon which shows the existence of even
the rarest atmosphere. Some observers, however, and among
them Messrs. Beer and Madler, believe that they have detected
signs of the existence of a very slight atmosphere.
PLATE II
TOTAL ECLIPSE OF THE SUN, OF JULY 18, 1860,
showing the Corona and the Red Flames; as observed by Dr.
Feilitzsch, at Castellon de la Plana
LUNAR ECLIPSE. 135
CHAPTER X.
LUNAR AND SOLAR ECLIPSES. OCCULTATIONS.
149. Eclipses. The obscuration, either partial or total, of the
light of one celestial body by another is in astronomy termed an
eclipse. When the earth comes between the sun and the moon,
the light of the sun is shut off from the moon, and we have a
Mjnar eclipse. A lunar eclipse can occur only at the time when
the moon is in opposition to the sun, that is to say, at the time
:>f full moon. When the moon comes between the earth and the
sun, the light of the sun is shut off from the earth, and we have
a solar eclipse. A solar eclipse can occur only at the time of
new moon. An eclipse of a star or a planet by the moon is called
an occultation.
If the orbit of the moon lay in the plane of the ecliptic, a
lunar and a solar eclipse would occur in every month. Owing,
however, to the inclination of the plane of the moon's orbit to
the plane of the ecliptic, the latitude of the moon is usually too
great to allow either kind of eclipse to take place; and it is only
in special cases, when the moon is in or near the plane of the
ecliptic at the time of conjunction or opposition, that an eclipse
of the sun or the moon is possible.
LUNAR ECLIPSE.
150. In Fig. 57 let S be the centre of the sun, and E that of
Fig. 57.
136 LUNAR ECLIPSE.
the earth. Draw the lines BH. and GG, tangent to the two
spheres. These lines will meet at some point A, and AHEG
will be a section of the shadow cast by the earth.
The whole shadow is of a conical shape, the vertex of the cone
being at A ; and a lunar eclipse will occur whenever the moon is
within this shadow. Draw the tangent lines BG and CH.
KDL is a section of a second cone whose vertex is at Z>. The
earth's shadow is called the umbra, and that portion of the second
cone which lies outside of the umbra is called the penumbra.
Thus KHA and A GL are sections of the penumbra. It must
be noticed, in regard to the construction of this figure, that since
only one tangent can be drawn to the circumference of a circle
at any one point, the lines BG and CH do not touch the two
circumferences at precisely the same points at which BH and
CG touch ; and that, furthermore, in all these figures the relative
size of the sun should be immensely greater than it is.
Now let M'MM" represent a portion of the moon's orbit at the
time of a lunar eclipse. As soon as the moon passes within the
line DK, some of the rays of the sun will be cut off from it by
the earth, and its brightness will begin to decrease. The whole
disc, however, will still be visible. As soon as the moon begins
to pass within the line HA, the disc will begin to disappear, and
when the whole disc has passed within the cone, the eclipse will
be total.
151. Different Kinds of Eclipses. When the moon's orbit
is so situated that only a part of the moon enters the umbra,
we have a partial eclipse. When the moon does not enter the
umbra, but merely touches it, we have an appulse. When the
centre of the moon coincides with the line which connects the
centre of the earth and that of the sun, the eclipse is cen-
tral. A central eclipse occurs very rarely, if indeed it occurs
at all.
152. The Semi-Angle of the Umbral Cone. The semi-angle of
the umbral cone is the angle EA G, Fig. 58. Now we have, by
Geometry,
SEC= ECG + EAG.
But SEC is the sun's angular semi-diameter, and EGG is its
LUNAR ECLIPSE. 137
horizontal parallax. Putting S for SEC, and P for ECG, we
have,
EAG = S P.
Fig. 58.
153. The Angular Semi-Diameter of the Shadow at the Distance
of the Moon. The angular semi-diameter of the shadow at the
distance of the moon is the angle MEM'. We have, by Geometry,
EM' G = MEM' + EA G.
Now EM' G is the moon's horizontal parallax, which we will
represent by P', and the value of EA G has been obtained in
the preceding article. We therefore have,
MEM' = P'+P S.
Observation shows that the earth's atmosphere increases the
apparent breadth of the shadow by about its one-fiftieth part :
hence in practice the angular semi-diameter of the shadow is
taken equal to f J (P' -f- P S). If we substitute in this expres-
sion the least values of P f and P, and the greatest value of JS t
from the table given in Art. 155, we shall find that the least
value of the angular semi-diameter of the shadow is about 37' 25" :
so that the entire breadth of the shadow is always more than
double the greatest diameter of the moon.
154. Length of the Earth's Shadow. The length of the shadow,
or the line EA, can be computed from the right-angled triangle
EA G, in which we have,
EA=JEQco8ec(8 P).
The mean value of this length is 858,000 miles, or more than
three times the distance of the moon from the earth.
155. Lunar Ecliptic Limits. We see from Fig. 58 that a lunar
eclipse can occur only when the moon's geocentric latitude at
the time of opposition, (or at full moon,) is less than the sum
of the angular semi-diameter of the shadow and the semi-diameter
138
LUNAR ECLIPSE.
of the moon. If we represent the. moon's semi-diameter by
the expression for this sum is
If the moon's geocentric latitude at the time of opposition is
greater than the greatest value which this expression can attain,
no eclipse can possibly occur : if it is less than the least value of
the expression, an eclipse is inevitable. These two values of
this expression are called the lunar ecliptic limits. Now, we have
by observation the following values of P, P' } &c. :
MAXIMA.
MINIMA.
P'
61' 32"
52' 50"
p
9
9
S'
16 46
14 24
s
16 18
15 45
In order to find the greatest value of the expression, we sub-
stitute in it the greatest values of P, P and $', and the least value
of S. The result is 1 3' 37": and no eclipse will occur when the
moon's latitude exceeds this limit. The least value of the expres-
sion is 51' 49": and when the moon's latitude at opposition is less
than this, an eclipse cannot fail to occur. There are some con-
siderations, however, which have not been taken into account,
which may increase each of these limits by about 16".
When the moon's latitude at opposition is within these limits,
an eclipse is possible, but not necessarily certain. In order to
determine whether in such case it will or will not occur, the
actual values which P, P', S and S' will have at that time must
be substituted in the expression, and the result compared with
the corresponding latitude of the moon.
156. Since a lunar eclipse is caused by the moon's entering
the earth's shadow, it will be seen at the same instant of time by
every observer who has the moon above his horizon : and the
character of the eclipse, whether total or partial, will be every-
SOLAR ECLIPSE. 139
where the same, As the moon's motion towards the east is more
rapid than that of the earth (and consequently of the shadow),
the eclipse will begin at the eastern limb of the moon. A total
eclipse of the moon may last for nearly two hours. Even when
totally eclipsed, however, the moon does not, in general, disappear
from view, but shines with a dull reddish light. This phenomenon
is caused by the earth's atmosphere, which refracts the rays of
light from the sun which enter it near the points G and H, Fig.
57, and turns them into the cone. The rays which pass still
nearer to these points are probably absorbed by the atmosphere,
thus giving rise to the observed increase of the shadow mentioned
in Art. 153.
SOLAR ECLIPSE.
157. In Fig. 59, let S represent the sun, E the earth, and M
the moon, at the time of a solar eclipse. HAK will be a section
of the moon's umbra, and GHA and AKD, sections of its pen-
umbra.
Fig. 59.
To an observer situated within the umbra, at any point of the
arc dby the eclipse will be total ; while to one situated within the
penumbra, as at L, for instance, the eclipse will be partial.
Beyond the penumbra no eclipse whatever will be seen. Hence
the geographical position of the observer determines the charac-
ter of the eclipse : a condition different from that in the case of
a lunar eclipse, which we have seen is the same to all observers.
158. Length of the Moon's Shadow. It is evident that, to an
observer at the apex of the shadow A, the angular semi-diametera
of the sun and the moon would be equal. Now, the mean angular
semi-diameters of these two bodies as seen from the earth's centre
140 SOLAR ECLIPSE.
are nearly equal ; hence the mean position of the apex does not fall
very far from the earth's centre E. An approximate value of the
length of the shadow may be thus obtained. We have in Fig. 59,
. _.,_ HM CS
8mHAM =AM=AS'
But we have just now seen that HAM is the sun's angular
genii-diameter, as seen from A ; and as AE is small compared
with AS, we may consider the angle HAM to be the sun's geo-
centric semi-diameter. Denoting this by S, we have,
sin = .
AM
Now, if S f represents the moon's geocentric semi-diameter, we
have,
HM
Combining these two equations, and finding the value of AM,
we have,
Knowing, then, the distance of the moon from the earth's centre,
and the semi-diameters of the sun and the moon, we may find
the length of AM. When the two semi-diameters are equal, we
have AM equal to EM, and the apex is at the earth's centre.
When the semi-diameter of the moon is greater than that of
the sun, the apex falls beyond the earth's centre : when it is
less, the apex does not reach the centre. Appropriate calcula-
tions will show that when both sun and moon are at their mean
distances from us, the apex falls short of the earth's surface :
and that when the moon is at its least distance from the earth,
and its shadow is the longest, the apex falls about 14,000 miles
beyond the earth's centre.
159. Different Kinds of Eclipses. When the shadow falls
beyond the earth's surface, the eclipse is total, as we have
already seen, within the umbra, and partial within the penumbra.
When the apex just touches the earth, the eclipse is total only
at the point where it touches. When the apex falls short of
the surface, there will be no total eclipse ; but at the point in
which the axis of the cone, prolonged, meets the earth, the
SOLAR ECLIPSE. 141
observer will see what is called an annular eclipse, the moon
being projected upon the disc of the sun, but not covering it.
160. Solar Ecliptic Limits. In Fig. 60 let S represent the
sun, E the earth, and M the moon. No eclipse of the sun can
occur unless some part of the moon passes within the lines BG
B
G
Fig. 60.
and GD, drawn tangent to the sun and the earth : that is, unless
the moon's geocentric latitude is less than the angle MES.
Now we have,
MES = MEA + AEB + BES,
and, also,
AEB= CAE CBE.
BES is the sun's semi-diameter, MEA that of the moon, CAE
the moon's horizontal parallax, and CBE the sun's : hence,
using the notation already employed in Art. 155, we have,
MES = 8 + 8 + P. P.
The greatest value of this expression is found by employing
the greatest values of S, $', and P', and the least value of P,
as given in Art. 155, and is 1 34' 27" : and there will be no
eclipse if the moon's latitude at conjunction is greater than
this amount. The least value is 1 22' 50" ; and if the latitude
at conjunction is less than this an eclipse is inevitable. These
two values, which, owing to certain considerations omitted in
this discussion, should both be increased by about 25", are called
the solar ecliptic limits. In order to determine whether an
eclipse will occur when the moon's latitude at conjunction falls
within these limits, we must substitute in the expression the
values which the different quantities will really have at that
time, and compare the result with the corresponding latitude
of the moon.
161. General Phenomena. Since the moon moves towards
142 CYCLE OF ECLIPSES.
the east more rapidly than the sun, a solar eclipse will begin
at the western side of the sun. For the same reason the moon's
shadow will cross the earth from west to east, and the eclipse
will begin earlier at the western portions of the earth's surface
than at the eastern. The moon's penumbra is tangent to the
earth's surface at the beginning and the end of the eclipse, so
that the sun will be rising at that place where the eclipse is
first seen, and setting at the place where it is last seen. A solar
eclipse may last at the equator about 4J hours, and in these
latitudes about 3.\ hours. That portion of the eclipse, however,
in which the sun is wholly concealed can only last about eight
minutes: and in these latitudes, only about six minutes.
The darkness during a total eclipse, though subject to some
variation, is scarcely so intense as might be expected. The sky
often assumes a dusky, livid color, and terrestrial objects are
similarly affected. The brighter planets and some of the stars
of the first magnitude generally become visible ; and sometimes
etars of the second magnitude are seen. The corona and the
rose-colored protuberances described in Art. 102 also make
their appearance. When the sun's disc has been reduced to a
narrow crescent, it sometimes appears as a succession of bright
points, separated by dark spaces. This phenomenon bears the
name of Baily's beads. The dark spaces are supposed to be
the lunar mountains, projected upon the sun's disc, and allowing
the disc to show between them.
Occasionally the moon's disc is faintly seen, shining with a
dusky light. This is caused by the rays of the sun, reflected
back to the moon by that portion of the earth's surface which
is still illuminated by the sun : just as at the time of new moon
its entire disc is rendered visible.
CYCLE AND NUMBER OF ECLIPSES.
162. Cycle of Eclipses. In order that either a solar or a
lunar eclipse shall occur, it is necessary, as we have seen, that
the moon shall be near the ecliptic (in other words, near the
line of nodes of its orbit), at either conjunction or opposition.
It is evident that when the moon is near the line of nodes at
such a time, the sun also must be near the same line. The
NUMBER OF ECLIPSES. 143
occurrence of eclipses, then, depends on the relative situations
of the sun, the moon, and the moon's nodes, and is only pos-
sible when they are all in, or nearly in, the same straight line.
AVe have already seen (Art. 128) that the line of nodes is con-
tinually revolving to the west, completing a revolution in about
18.6 years. The sun, then, in its apparent path in the ecliptic
will move from one of the moon's nodes to the same node again
in less than a year. This interval of time may be called the
synodical period of the node, and is found to be 346.62 days.
Now, we have,
19 X 346.62d. = 6585.8d:
and, the lunar month being 29.53 days, we have also,
223 X 29.53d. = 6585.2d.
If, then, the moon is full and at its node on any day, it will
again be full, and at the same node, or very nearly at it, after
an interval of 6585 days : and the eclipses which have occurred
in that interval will occur again in very nearly the same order.
This period of 6585 days, or 18 years and 10 days, is called the
cycle of eclipses. It was known to the Chaldsean astronomers
under the name of Saros. Care must be taken not to confound
this cycle with the lunar cycle described in Art. 147.
163. Number of Eclipses. Since the limit of the moon's lati-
tude is greater in the case of a solar eclipse than in the case
of a lunar eclipse, there are more solar eclipses than lunar
eclipses. Usually 70 eclipses occur in a cycle, of which 41
are solar and 29 are lunar. Since we know that a solar eclipse
is inevitable when the moon is so near the line of nodes at
conjunction that its latitude is less than 1 23' 15", we can com-
pute the corresponding angular distance of the sun at the same
time from this line ; and having computed this, we may also
determine the length of time required by the sun in passing
through double this angle, or, in other words, the time required
in passing from one of these limits to the corresponding limit on
the other side of the same node. If we do this, we shall find
that the sun cannot pass either node of the moon's orbit without
being eclipsed : and therefore there must be at least two solar
eclipses in a year. The greatest number that can occur is five.
The greatest number of lunar eclipses in the year is three, and
144 OCCULTATIONS.
there may be none at all. The greatest number of both kinds
of eclipses in a year is seven ; the usual number is four.
Although the annual number of solar eclipses throughout the
whole earth is the greater, yet at any one place more lunar eclipses
are-visible than solar. The reason of this is that a lunar eclipse,
when it does occur, is visible over an entire hemisphere, while
the area within which a solar eclipse is visible is very much
more limited.
OCCULTATIONS.
164. An occultation of a planet or a star will occur whenever
the planet or star is so situated in latitude as to allow the moon
to come in between it and the earth. In order to determine the
limit of a planet's latitude within which an occultation of the
planet is possible, let us refer to Fig. 61. In this figure, E is the.
A
Fig. 61.
centre of the earth, P that of a planet, and M that of the moon.
An occultajion will occur when the moon comes between the
tangent lines GB and AH. Let EC be the plane of the ecliptic.
PEC is then the geocentric latitude of the planet, and MEG
that of the moon.
We have,
PEC = PEG + GET) + DEM + MEC,
and also,
GET) = EDB EGD.
Now, PEG is the planet's semi-diameter, EGD its horizontal
parallax, DEM the moon's semi-diameter, EDB its horizontal
parallax, and MEC, as above stated, its latitude. The value
OCCULT ATIONS. ". 15
of PEC, therefore, can very readily be obtained. If P, instead
of representing a planet, represents a star, the distance PE
becomes so great that AH and BG are sensibly parallel, and
the star's parallax and semi-diameter reduce to zero. In this
case the greatest value of PEC, within which an occupation
can occur, will be the sum of 5 20' 6", 61' 32", and 16' 45",
which is 6 38' 23".
Since the moon moves from west to east, the occultation
always takes place at its eastern limb. From new moon to full,
the dark portion of the moon is to the east, as may be seen in
Fig. 54, and from full moon to new, the bright limb is to the
east. When an occultation occurs at the dark edge, particu-
larly if the moon is so far on towards its first quarter that the
dark portion is invisible, the disappearance is extremely strik-
ing, as the occulted body appears to be extinguished without
any visible interference.
As already stated in Art. 83, a solar eclipse, or an occultation
of a planet or star, although not visible at different places at
the same absolute instant of time, may still be made the means
of very accurately determining the longitude of a place, or the
difference of longitude of two places. For instance, in the case
of a solar eclipse, we may deduce, from the local times of the
beginning and the end of the eclipse, as observed at any place,
the time of true conjunction of the sun and the moon: the time
of conjunction, that is to say, as seen from the centre of the earth.
If, then, we compare the local time of true conjunction with the
Greenwich time of true conjunction, it amounts to comparing
the local and the Greenwich timje corresponding to the same
absolute instant: and the difference of these two times will evi-
dently be the longitude of the place of observation from Green-
wich.
13
146
TIDES.
CHAPTER XL
THE TIDES.
165. THE surface of the ocean rises and falls twice in the
course of a lunar day, the length of which is, as we have already
seen (Art. 143), about 24h. 50m. of mean solar time. The rise
of the water is called flood tide, and the fall ebb tide. When the
water is at its greatest height it is said to be high water, and
when at its least height, low water.
166. Cause of the Tides. The tides are due to the inequality
of the attractions exerted by the moon upon the earth and the
waters of the ocean, and to a similar but smaller inequality in
the attractions exerted by the sun.
In order to examine the phenomena of the tides, we will con-
sider the earth to be a solid globe, surrounded by a shell of
water of uniform depth. The centrifugal force induced by the
rotation of the earth would tend to give a spheroidal form to
this shell of water; but as we wish simply to examine the effects
of the attractions exerted by the moon and the sun, we will dis-
regard the notation of the earth, and consider it to be at rest.
In Fig. 62, then. letABCD represent the earth, and the dotted
Fig. 62.
line GHIKihe surrounding shell of water. Let Mloe the moon.
The attraction of the moon on the solid mass of the earth is the
TIDES. 147
same that it would be if the whole mass were concentrated at
the point E. Now since, by the law of gravitation, the at-
traction of the moon on any two particles is inversely as the
square of the distances of the two particles from the moon, the
attraction exerted upon the particle of water at G will be greater
than that exerted upon the general mass of the earth, supposed
to be concentrated at E. The particle G will therefore tend to
recede from the earth : that is to say, its gravity towards the
earth's centre will be diminished, although, as is plain, it will not
move. The same result will follow at the opposite point /.
The moon will exert a greater attractive power upon the mass
of the earth than upon a particle at /, and will tend to draw the
earth away from the particle: so that the gravity of the particle
at I towards the earth's centre will also be diminished. Since
the ratio of the distances ME and MG is very nearly equal to
the ratio of the distances MI and ME, the amount of the decrease
of gravity at G and at I will be nearly the same.
Let us next examine the effect of the moon's attraction at
some point L, not situated vertically under the moon. The at-
traction of the moon at this point is less than that at the point
G, since the distance ML is greater than the distance MG; and
since the attraction exerted on the mass of the earth is, of course,
the same for both points, the difference of the attractions exerted
on the earth and the water is less at the point L than at the
point G. At the point L, however, this inequality of attraction
is not wholly counteracted by gravity : for if the force with which
the moon tends to draw a particle at L along the line ML be re-
solved into two forces, one in the direction of the radius EL,
and the other in the direction of the tangent LT, the latter force
will cause the particle to move towards the point G. The same
result will follow at any other point of the arc HGK: so that
all the water in that arc tends to flow towards the point G, and
to produce high water there.
In the same way it may be shown that the water in the arc
HIK tends to flow towards the point /, and to produce high
water at that point.
The result, then, of the attraction of the moon, exerted under
the suppositions which we made at the outset, is to give to the shell
148
TIUES.
N
of water a spheroidal form, as shown in the figure, the major
axis of the spheroid being directed towards the moon. Suitable
investigation shows that the difference of the major and the minor
semi-axis of this spheroid is about fifty-eight inches.
167. Daily Inequality of the Tides. The rotation of the earth,
and the inclination of the plane of the moon's orbit to the plane
of the equator, produce in general an inequality in the two daily
tides at any place. In order to show this, we will suppose that
the spheroidal form of the water is assumed instantaneously in
each new position of the earth as it rotates. In Fig. 63, let E
M be the centre of the
earth, surrounded,
as in Fig. 62, by
a spheroidal shell
of water, the trans-
verse axis of the
spheroid lying in
the direction of the
moon M. Let Pp
be the axis of rota-
tion of the earth,
and CD the equator.
The angle MED is
the moon's declination. The water is at its greatest height, as be-
fore, at the points A and B, and the height at other points dimi-
nishes as the angular distance of those points from the line GH
increases. Let / be a place having the same latitude that A has,
but situated 180 from it in longitude. The height of the tide
at /is represented by IK. In a little more than twelve hours
the rotation of the earth will have caused I and A to change
places with reference to the moon. I will then be where A is
in the figure, and will have a tide with the height A G, while
A will be where /is now, and will have a tide with the height
IK. It is not necessary to prove that IK is less than A G. We
see, then, that at both A and / the two daily tides are unequal,
the greater of the two occurring at each place at the time of the
moon's upper culmination at that place, or being, at all events,
the one which occurs next after that culmination. The same
Fig. 63.
TIDES. 149
daily inequality of tides may be shown to exist at any other
points on the earth's surface, as, for instance, at L and 0. At
the equator, however, and also at the poles, the two daily tides
are sensibly equal, as may readily be seen from the figure.
168. General Laws. As far as the influence of the moon is
concerned in causing tides, the following general laws may be
deduced from what has been shown in the preceding articles.
(1.) When the moon is in the plane of the celestial equator, or,
in Fig. 63, when EM coincides with ED, the tides are greatest
at the equator, and diminish at other places as the latitude in-
creases ; and the two daily tides at any place are sensibly equal.
(2.) When the moon is not in the plane of the celestial equa-
tor, the two daily tides at any place except the poles and the
equator are unequal. The greatest tides, and the greatest ine-
quality of tides, occur at those places whose latitude is numeri-
cally equal to the moon's declination. If the place is on the
same side of the equator as the moon, the greater of the two
daily tides occurs at or next after the upper culmination of the
moon; if the place is on the opposite side of the equator, the
greater tide occurs at or next after the lower culmination of the
moon.
(3.) Owing to the retardation of the moon (Art. 143), there is
a similar retardation in the occurrence of high water. The
length of the lunar day being on the average 24h. 50m., the aver-
age interval of time between two successive tides is 12h. 25m.
169. Influence of the Sun in Causing Tides. All that has been
said in the preceding articles with regard to the influence of the
moon in creating tides is equally true with regard to the influ-
ence of the sun. The mass of the sun being so immense in
comparison with that of the moon, it might be supposed that
the influence of the sun over the tides would be greater than
that of the moon, even although its distance from the earth is
much greater than that of the moon. But such is not the case
in fact. The height of the tide produced by either body is not
so much due to the absolute attraction which that body exerts,
as to the relative attractions which it exerts on the solid mass of
the earth and on the water : and the moon is so much nearer to
the earth than the sun, that the difference of its attractions on
150 PRIMING AND LAGGING.
the earth and the water is greatej than the corresponding dif-
ference in the case of the sun. It is computed that the effect
of the moon in creating tides is about 2i times that of the sun.
170. Combined Effects of both Sun and Moon. Since each
body, independently of the other, tends to raise the surface of the
water at certain points, and to depress it at certain other points,
the tides will evidently be higher when both bodies tend to raise
the surface of the water at the same time, than when one tends
to raise and the other to depress it. At new and full moon the
two bodies act together, while at the first and the last quarter
they act in opposition to each other. The tides at the former
periods will therefore be the greater, and are called spring tides ;
and the tides at the latter periods are called neap tides. The ratio
of the spring to the neap tide is that of (2i -f- 1) to (2 1),
or of 5 to 2.
The height of the tide is also affected by the change in the
distance of the attracting body. For instance, when the moon
is in perigee, the tides tend to run higher than when the moon is in
apogee; and when the moon is in perigee, and also either new or
full, unusually high tides will occur.
171. Priming and Lagging of the Tides. Each of these bodies
may be supposed to raise a tidal wave of its own, and the actual
high water at any place may be considered to be the result of
the combination of the two waves. When the moon is in its
first or its third quarter, the solar wave is to the west of the lunar
one, and the actual high water will be to the west of the place
at which it would have been had the moon acted alone. There
is therefore at these times an acceleration of the time of high water,
which is called the priming of the tides. In the second and the
fourth quarter, the solar wave is to the east of the lunar one,
and a retardation of the time of high water occurs, which is
called the lagging of the tides.
172. Although the theory of the tides, on the supposition that
the earth is wholly covered with water, admits of easy explana-
tion, the actual phenomena which they present are very much
more complicated, and must be obtained principally from obser-
vation. The lunar wave mentioned in the preceding article
being greater than the solar wave, we may consider the two to-
ESTABLISHMENT. 151
gether to constitute one great tidal wave, which at every moment
tends to accompany the moon in its apparent diurnal path to-
wards the west, raising the waters at successive meridians, but
giving them little or no progressive motion. This tidal wave
would naturally move westward with an angular velocity equal
to that of the moon, so that at the equator its motion would he
about 1000 miles an hour ; but the obstructions offered by the
continents, the irregularity of their outlines, the uneven surface
of the ocean bed, and the action of winds and currents and fric-
tion, all combine not only to diminish the velocity of the tidal
wave, but also to make it extremely variable.
173. Establishment of a Port. The interval of time between
the moon's transit over any meridian and high water at that
meridian varies at different places, and varies also on different
days at the same place. This interval of time is called the
luni-tidal interval. The mean of the values of this interval on
the days of new and full moon is called the common establish-
ment of a port. The mean of all the luni-tidal intervals in the
course of the month is called the corrected establishment. These
establishments are obtained by observation, and are given in
Bowditch's Navigator, and also in other works. Thus the estab-
lishment of Annapolis is 4h. 38m., and that of Boston llh. 12m.
The time of transit of the moon over any meridian on any day
can be obtained from the Nautical Almanac: and the sum of
this time of transit and of the establishment of any port will be
the approximate time of that flood tide which occurs next after
the transit. Suppose, for instance, the time of high water at
Annapolis, on January 11, 1867, is desired. We have from the
Almanac the time of the moon's transit, 4h. 33m. ; adding to this
the establishment, 4h. 38m., the sum is 9h. llm. This is, in this
case, the time of the evening tide. The time of the morning tide
may be obtained by subtracting 12h. 25m. from this time, which
will give us 8h. 46m. A.M. A more accurate result in this
last case might be obtained by taking from the Almanac the
time of the preceding lower transit, and adding the establish-
ment to it; but practically this would be a needless refinement,
for the two results would only vary by about two minutes.
The time of transit which the Almanac gives is in astronomical
152 COTIDAL LINES.
time: hence the resulting time of J^igh water will also be in astro-
nomical time, and it will frequently happen that the time which
we find, when turned into civil time, will fall on the civil day
subsequent to the day for which the time is desired. Take, for
instance, January 23, 1867, at Annapolis. The time of transit is
January 23, 15h. 34m. : hence the time of high water is Janu-
ary 23, 20h. 12m., or, in civil time, January 24, 8h. 12m. A.M.
If, then, we wish the time of high water on the morning of the
civil day January 23d, we must take from the Almanac the time
of transit for the astronomical day of January 22d.
There are other tables given in Bowditch's Navigator, and in
the United States Coast Survey Reports, by which the time of
high water can be obtained with greater accuracy than by the
method given above.
174. Cotidal Lines. If the tidal wave were everywhere uni-
form in its progress, it would come to all points on the same
meridian at the same time. But, owing to irregularities induced
by local causes, such is not the case, and places on different
meridians often have high water at the same instant of time.
Charts are therefore published on which are drawn lines con-
necting places where high tides occur at the same instant: and
these lines are called cotidal lines. These lines are usually ac-
companied by numerals, which indicate the hours of Greenwich
time at which high tides occur on the days of new and full moon
along the different lines.
175. Height of Tides. At small islands in mid-ocean the height
of the tides is not great, being sometimes less than one foot. When
the tidal wave approaches a continent, and the water begins to
shoal, the velocity of the wave is diminished, and the height of
the tide is increased. When the wave enters bays opening in
the direction in which the wave is moving, the height of the tide
is still further increased.
The eastern coast of the United States may be considered to
constitute three great bays : the first included between Cape Sable,
in Nova Scotia, and Nantucket, the second between Nantucket
and Cape Hatteras, and the third between Cape Hatteras and
Cape Sable, in Florida. In each of these bays the tides, in gene-
ral, increase in height from the entrance of the bay to its head.
HEIGHT OF TIDES. 153
For instance, in the most southern of these bays, the tides at
Cape Sable and Cape Hatteras are not more than two feet in
height; while at Port Royal, at the head of this bay, they are
about seven feet. The same thing is noticed, in general, in
smaller bays and sounds. For instance, in Long Island Sound,
the height of the tide is two feet at the eastern extremity, and
more than seven feet at the western. This increase of height is
particularly noticeable in the Bay of Fundy, in which the height
is eighteen feet at the entrance, and fifty and sometimes seventy
feet at the head.
There are in some cases, however, special causes which create
exceptions to this general rule of increase of the tides between
the entrance and the head of a bay. In Chesapeake Bay, for
instance, which is wider at some places than it is at the entrance,
and which lies about north and south, the tides in general dimin-
ish in height as we ascend the bay.
176. Tides in Rivers. The same general principle holds good
in the tides of rivers. When the channel contracts or shoals
rapidly, the height of the tide increases: when it widens or
deepens, the height decreases. In a long river, then, the tides
may alternately increase and decrease. For instance, at Tivoli,
on the Hudson, between West Point and Albany, the tide is
higher than it is at either of those two places.
177. Different Directions of the Tidal Wave. The tidal wave
naturally tends to move towards the west ; but the obstructions
offered by the continents and the promontories, and the irregular
conformation of the bottom of the ocean, materially change the
direction of its motion. Sometimes its direction is even towards
the east. From a point about one thousand miles southwest of
South America there appear to start two tidal waves, which travel
in nearly opposite directions, one towards the west and the other
towards the east.
178. Four Daily Tides. At some places the tides rise and
fall four times in each day. This is ascribed to the existence of
two different tidal waves, coming from opposite directions. This
phenomenon occurs on the eastern coast of Scotland, where one
wave comes into the North Sea through the English Channel,
while a second wave comes in around the northern extremity of
154 TIDES IN LAKES.
Scotland. At places where these two waves arrive at different
times, each wave will produce two daily tides.
179. Tides in Lakes and Inland Seas. If there is any tide in
lakes and inland seas, it is usually so slight as to be scarcely
measurable. A series of careful observations has demonstrated
the existence of a tide in Lake Michigan, which is at its height
about half an hour after the moon's transit. The average height
which it attains, however, is less than two inches.
180. Other Phenomena. Along the northern coast of the Gulf
of Mexico there is only one tide in the day, the second one being
probably obliterated by the interference of two waves. An ap-
proximation to this state of things is noticed on the Pacific coast,
where at times one of the daily tides has a height of several feet,
and the other a height of only a few inches. A very curious
statement is made by missionaries in reference to the tides at the
Society Islands. They say that the tides there are uniform, not
only in the height which they attain, but in the time of ebb and
flow, high tide occurring invariably at noon and at midnight : so
that the natives distinguish the hour of the day by terms de-
Bcriptive of the condition of the tide.
It is now generally admitted that one result of the friction of
the tides is a diminution of the velocity of the earth's rotation ; and it is
possible that the moon's secular acceleration (page 133) is partly due, not
to an increase in the moon's orbital velocity, but to this same diminution
of the earth's rotation. The amount of the diminution is, however, so very
small that all attempts to compute it have been thus far unsuccessful.
PLANETS. 15. r )
CHAPTER XII.
THE PLANETS AND THE PLANETOIDS. THE NEBULAR
HYPOTHESIS.
181. The Planets and their Apparent Motions. There are other
celestial bodies besides the sun and the moon, which, while they
share the common diurnal motion towards the west, appear to
change their relative positions among the stars. These bodies are
called planets, from a Greek word signifying wanderer. Some of
them are visible to the naked eye, and some only become visible
by the aid of a telescope. In some of them the change of position
among the stars becomes apparent from the observations of a
few nights : while in others even the annual change of position
is so small that they have for ages been considered to be fixed
stars.*
This change of position is determined, as it was determined in
the case of the sun and the moon, by observations of their right
ascensions and declinations. When such observations are made,
the apparent motions of the planets are found to be very irregular.
Sometimes they appear to move towards the east, and sometimes
towards the west, while at other times they appear to be station-
ary in the heavens. Such irregularity in the direction of their
motion is at once seen to be incompatible with the supposition
* The times of meridian passage of all the planets which ever become
conspicuously visible are given in the American Ephemeris. The altitude
which any planet has when on the meridian is obtained from the corre-
sponding zenith distance, and this is found at any pla^ce whose latitude
is known, from the formula
*=: d:
the declination being also given in the Ephemeris. It must be remembered
that (L d) becomes numerically (Zr + d) when L arid d have different
names ; that z in any case has the same name as (L d) ; and that when a
is north, the bearing of the body is south, a.nd conversely.
156 PLANETS.
that they are, like the moon, satellites of the earth, revolving
about it as a centre. The next supposition that will naturally
be made is that they may revolve about the sun.
182. Heliocentric Parallax. In order to test the correctness
of this second supposition, we must first, from the apparent
motions which are observed from the earth, deduce the corre-
sponding motions which would be seen by an observer stationed
at the sun. Fig. 64 will serve to show how, by means of a body's
heliocentric parallax (Art. 56), the position which that body
would have if seen from the sun's centre in other words, its helio-
centric position may be determined from its geocentric position.
In this figure let S represent the sun, AB CE the earth's orbit,
the plane of which intersects the celestial sphere in the circle
Fig. 64.
, and P the position of a planet when projected upon the
plane of the ecliptic. Let the vernal equinox be supposed to lie
in the direction EV or SV, which two lines must be supposed
sensibly to meet when prolonged to the celestial sphere. Draw
the lines EP and SP. Since the distances of the planet from the
sun and the earth are finite, these lines will not lie in the same
direction, and the angle EPS which they make with each other
will be the difference of the directions in which the planet is seen
from the earth and the sun : in other words, the planet's helio-
ORBITS OF THE PLANETS. 157
centric parallax in longitude. Through S draw SK parallel to
ED. The angle VEP, or its equal, VSK, is the planet's geo-
centric longitude, and is obtained by observation. The sum of
this angle and the angle EPS is the angle VSP, or the planet's
heliocentric longitude. Provided, then, we know the angle EPS,
we can readily obtain the angle VSP. Now, in the triangle PES
we know from Kepler's Third Law the ratio of the sides SP
and ES, which are the distances of the planet and the earth from
the sun; and the angle PES, the planet's angular distance from
the sun, or its elongation (Art. 56), can be obtained by observa-
tion. The angle EPS may then be readily computed.
By a similar method the planet's heliocentric latitude may be
determined from its geocentric latitude, and the heliocentric
place of a planet may thus be obtained at any time.
183. Orbits of the Planets. When the motions of the planets
as they would be seen from the centre of the sun are thus deduced
from their observed motions with reference to the earth, all the
apparent irregularities of motion disappear. The planets are
found to revolve from west to east in ellipses about the sun in
one of the foci, the eccentricity of the ellipses diminishing, as a
general rule, as the magnitude increases. The planes of the
orbits are found to be nearly coincident with the plane of the
ecliptic, and Kepler's and Newton's laws are exactly fulfilled in
the case of each planet. The line in which the plane of each
planet intersects the plane of the ecliptic is called the line of
nodes, and the terms perihelion and aphelion have the same
signification that they have in the case of the earth.
184. Inferior and Superior Planets. The planets are divided
into two classes : inferior and superior planets. The inferior
planets are those whose distances from the sun are less than the
distance of the earth from the sun, and whose orbits are therefore
included within the orbit of the earth. The inferior planets are
Mercury and Venus.* The superior planets are those whose
* There are some astronomers who are inclined to suspect the existence
of a third inferior planet, Vulcan, distant about 13,000,000 miles from the
sun. Two American observers are convinced that they saw such a planet
during the total solar eclipse of Julv 29, 1878.
14
158
INFERIOR PLANETS.
distances from the sun are greater than that of the earth, and
whose orbits therefore include the orbit of the earth. The
superior planets are Mars, Jupiter, Saturn, Uranus, and Neptune.
There is besides these a group of small planets, called minor
planets, planetoids, or asteroids, situated between Mars and
Jupiter. Up to October, 1878, 192 of these minor planets had
been discovered. The earth is also a planet, lying between
Venus and Mars. It is therefore a superior planet to Mercury
and Venus, and an inferior planet to the other planets. Its
sidereal period is greater than the periods of the inferior planets,
and less than those of the superior planets.
INFERIOR PLANETS.
185. In Fig. 65 let S represent the sun, pp'p"p"" the orbit
of an inferior planet, the plane of which is supposed to coincide
Fig. 65.
with the plane of the ecliptic, ABDEt\\Q orbit of the earth, and
the circle KGH the intersection of the plane of the ecliptic with
the celestial sphere. Suppose the earth to be at E. When the
planet is at P, between the earth and the sun, or at P"' 9 on the
opposite side of the sun to the earth, it has the same geocentric
DIRECT AND RETROGRADE MOTION. 159
longitude as the sun, and is in conjunction with it. The position
at P is called the inferior conjunction, and that at P'" the superior
conjunction.
The greatest angular distance of the planet from the sun will
evidently occur when the line connecting the planet and the earth
is tangent to the orbit of the planet ; that is to say, when the planet
is at P" or P"". The position at P" is called the greatest western
elongation of the planet, that at P"" the greatest eastern elongation
of the planet. We have already seen in Art. 92 that the rela
tive distances of the planet and the earth from the sun are at
once obtained when we have measured the greatest elongation.
186. Direct and Retrograde Motion. The motion of the infe-
rior planets is always in reality from west to east, or direct, as it
is called; but when the planet is near its inferior conjunction,
its motion is apparently from east to west, or retrograde. This
apparent retrograde motion is explained in Fig. 65. Let the
planet be at its inferior conjunction at P, and let both the earth
and the planet move on about the sun in the direction EABD.
The angular and the linear velocity of the planet about the sun
being greater than they are in the case of the earth, when the
earth arrives at E', the planet will be at some point P', and will
lie in the direction E'G; the sun, on the other hand, will lie in
the direction E'S'. While, then, the earth is advancing from E
to E', the sun and the planet appear to move away in opposite
directions from the point (7, on which both were projected when the
earth was at E. But the apparent motion of the sun is invariably
towards the east ; hence the planet has apparently moved tow'ards
the west. It may also be shown that the same apparent retro-
grade motion occurs when the planet is approaching inferior
conjunction, and is within a short distance of it.
187. Stationary Points. When the planet is at P"", it is
moving directly towards the earth in the direction P""E, and
the motion of the earth in its orbit gives the planet an apparent
motion in advance. The same must also be the case when the
planet is at P". Since then the motion of the planet is direct
at the greatest elongations, and retrograde at inferior conjunction,
there -must be a point in the orbit between inferior conjunction
and each elongation at which the planet neither advances nor
160 ELEMENTS OF A PLANET'S ORBIT.
recedes, but appears stationary 4n the heavens. These points
are called the stationary points.
At all other parts of the orbit except those which have been
discussed, the apparent motion of the planet is direct ; but the
velocity with which it moves is subject to great variation. It
was on account of this irregularity, both in the direction and the
amount of their apparent motions, that these bodies were called
wandering stars by the ancient Greeks.
188. Evening and Morning Stars. Except at the times of
conjunction, an inferior planet is either to the east or to the west
of the sun. When it is to the east of the sun it will set after
the sun has set, and when it is to the west of the sun it will rise
before the sun has risen. In certain parts of its orbit the planet's
elongation from the sun is sufficiently great to carry the planet
beyond the limits of twilight, or 18 (Art. 101); it will then be
an evening star if to the east of the sun, and a morning star
if to the west. It is only to Venus, however, that these terms
are commonly applied, at least so far as the inferior planets are
concerned : since Mercury is so near to the sun that it is seldom
visible, and even when it is visible, it appears like a star of only
the third or the fourth magnitude.
189. Elements of a Planet's Orbit. In order to compute the
position in space at any time of either an inferior or a superior
planet, we must be able to determine:
1st. The relative position of the plane of the planet's orbit to
the plane of the ecliptic ;
2d. The position of the orbit itself in the plane in which it
lies;
3d. The magnitude and the form of the orbit; and
4th. The position of the planet in its orbit.
These four conditions require the knowledge of seven distinct
quantities. The first condition is satisfied if we know (1) the
position of the line in which the plane of the orbit intersects the
plane of the ecliptic, or, what amounts to the same thing, the
longitude of the planet's nodes, and (2) the inclination of the
two planes to each other. The second condition is satisfied if
we know (3) th longitude of the perihelion. The third condi-
tion is satisfied if we know (4) the semi-major axis, or the
LONGITUDE OF THE NODE.
161
]>lauet's mean distance from the sun, and (5) the eccentricity of
the orbit. Finally, the last condition is satisfied if we know
(6) the time in which it makes one complete revolution about
the sun, or its periodic time) and (7) the time when the planet
is at some known place in its orbit, as, for instance, the peri-
helion. These seven quantities are called the elements of the orbit.
190. Heliocentric Longitude of the Node. A planet is at its
nodes when its latitude is zero; and if the heliocentric longitude
of the planet at that time can be determined, it will also be the
heliocentric longitude of the node, since the line of nodes of
every planet passes through the sun. But the heliocentric longi-
tude of a planet when at its node differs from the geocentric
longitude (which may be obtained directly from observation),
excepting only in case the earth itself happens at that time to
be on the line of nodes. . We must therefore be able to deduce
the heliocentric longitude of the planet from the geocentric.
When the planet's distance from the sun is known, this can be
done by the method explained in Art. 182; and when this dis-
tance is not known, the following method can be used.
N
In Fig. 66, let 8 be the sun, POHK the orbit of a planet,
CDEE' the orbit of the earth, and NM the line of nodes of the
162 INCLINATION OF A PLANET'S ORBIT.
planet. Let the vernal equinox lie in the direction EV or SV.
Let E be the position of the earth when the planet is on the line
of nodes at P. The elongation of the planet, or the angle PES,
and the geocentric longitude of both planet and node, or the
angle VEP, can be obtained by observation. Suppose both
planet and earth to move on in their orbits, and the earth to be
at E' when the planet again reaches the same node, and let the
planet's elongation at this time, or the angle SE'P, be observed.
Now, since the earth's orbit, although represented in the figure
by a circle, is raally an ellipse, ES and E'S will not in general
be equal to each other. The value of each, however, can be
readily obtained from the solar tables. The same tables will
also give us the angle ESE', which is the angular advance of the
earth in its orbit in the interval. In the triangle ESE', then,
knowing two sides and the included angle, we can compute the
sid EE', and the angles SEE' and SE'E. The angles PES
and PE'S having been obtained by observation, we can find the
angles PEE' and PE'E. Then in the triangle PEE', knowing
two angles and the included side, we can compute the side EP.
Finally, in ths triangle PES, knowing an angle and the two in-
cluding sides, we can obtain PS, or the planet's distance from
the sun, and the angle EPS, thi planet's heliocentric parallax,
from which, and the planet's observed geocentric longitude, we
can obtain the planet's heliocentric longitude, as in Art. 182.
This is, as we have already seen, the heliocentric longitude of
the node.
The nodes of every planet are found to have a westward
movement, similar in character to the precession of the equi-
noxes. It is a very slight movement, however, being only 70' a
century in the case of Mercury, and being less than that in the
case of the other planets.
191. Inclination of the Planet's Orbit to the Ecliptic. The
line of nodes of any planet being, as we have just now seen, a
nearly stationary line in the plane of the ecliptic, the earth
must pass it once in very nearly six months in its revolution
about the sun. The inclination of the plane of any planet's
orbit to the plane of the ecliptic may be determined by obser-
vations made when the earth is on the line of nodes. In Fig.
PERIODIC TIME. 163
67 let E be the earth, and EN the line
of nodes of a planet. Let AEN be the
plane of the ecliptic, and P the position
of a planet projected on the surface of
the celestial sphere. With EP as a
radius, let the arc PA be described, per-
pendicular to the plane of the ecliptic, ri s- 67 -
and also the arcs PN and NA. In the spherical triangle PNA,
right-angled at A, the arc PA, which measures the angle PEA,
is the geocentric latitude of the planet; AN, or the angle AEN,
is the difference between the geocentric longitudes of the planet
and the node; and the angle PNA is the inclination of the plane
of the orbit to the plane of the ecliptic. In the triangle PNA,
we have,
tan PA
It may be noticed in this formula that, since the sine of a small
angle varies more rapidly than the sine of a large angle, an.
error in AN will affect the result the less, the greater AN itself
happens to be at the time of observation : that is to say, the
farther the planet is from the node.
192. The Periodic Time of an Inferior Planet The time in
which an inferior planet makes one complete revolution about
the sun, or its periodic time, may be found by taking the interval
of time between two successive passages of the planet through
the same node. The accuracy of this method is however dimin-
ished by the small inclination (less than 7) of the planes of the
orbits to the plane of the ecliptic, which renders it difficult to
determine the instant when the latitude of the planet is zero.
It is found to be better to determine the planet's synodical period,
or the interval between two successive conjunctions of the same
kind, and from it to compute the sidereal period. The condi-
tions of this problem, and the method by which it is solved, are
identical with those in the case of the synodical and the sidereal
period of the moon, Art. 141. The formula there given was,
ST
~8+ T'
In applying this to the case of an inferior planet, F and 3
164 MERCURY.
denote the sidereal and the synodical period of the planet, and
T denotes, as before, the sidereal*year.
Instead of using the interval between two conjunctions as
the synodical period, we may take the interval between two
greatest elongations of the same kind. A very accurate mean
synodical period is obtained by taking two elongations separated
by a long interval, and dividing this interval by the number
of synodical periods which it contains.
193. It is hardly necessary to describe the methods by which
the other elements given in Art. 189 are determined. It will
readily be understood that the distance of the planet from the
sun, obtained as in Art. 190, or by Kepler's Law, will enable
us to obtain the form and the magnitude of the ellipse in which
the planet moves. The method by which the longitude of the
perihelion is obtained, although not intrinsically difficult, is too
elaborate for this work. Finally, when the longitude of the
perihelion is obtained, the time of the planet's perihelion passage
may evidently at once be determined. The perihelion of Venus
has a very minute retrograde motion : the perihelia of .all the
other planets have an eastward motion, similar to that of the
earth's line of apsides.
MERCURY.
194. Mercury revolves about the sun at a mean distance of
about 36,000,000 miles, the eccentricity of its orbit being about
4th. Its synodical period is about 116 days, and its sidereal
period 88 days. Its real diameter is about 3000 miles.* Its
mass is a matter of considerable uncertainty, and quite different
values of it are given by different astronomers. It may be
assumed to be approximately equal to y^th of the mass of the
earth.
The greatest elongation of Mercury is only about 28 20' :
* The distances and the diameters of all the celestial bodies except the moon
depend for their accuracy upon the accuracy with which the solar parallax
is determined. An error of I" in this parallax would affect the sun's dis-
tance from us to the amount of several millions of miles, and propor-
tionally also the distances and the diameters of the other celestial bodies ;
the values given must therefore be considered to be only approximate.
VENUS. 165
anrl hence the planet is rarely visible to the naked eye, and is
never a conspicuous object in the heavens. It is not generally
believed that it has any atmosphere. It exhibits phases similar
to those of the moon, and due to the same causes. It is asserted
by some observers that it rotates on an axis in about 24 hours,
though the truth of the assertion is by no means unchallenged.
If it has any compression, it is extremely small.
VENUS.
195. The mean distance of Venus from the sun is about
67,000,000 miles, its synodical period is 584 days, and its sidereal
period 225 days. The eccentricity of its orbit is small, being
only about T 7 oths. Venus is nearly as large as the earth, its
diameter being 7,600 miles. Its mass is about Jths of the mass
of the earth. It has no perceptible compression.
The greatest elongation of Venus from the sun amounts to
about 47 15', and hence it is often visible as an evening or a
morning star. At certain times its brightness is so great that
it can be seen in broad daylight with the naked eye, while at
night shadows are cast by the objects which it illuminates. It
exhibits phases similar to those of Mercury.
It seems to be generally admitted that Venus has an atmos-
phere the density of which is not very different from that of
the earth's atmosphere. Observations of spots upon the disc
go to show that the planet rotates upon an axis in a period of
about 23^ hours; but this conclusion is by no means certain.
The existence of a satellite of Venus was formerly suspected,
but no satellite was seen at the transit in December, 1874.
196. Transits of Venus. We have already seen (Art. 93)
how a transit of Venus across the sun's disc is employed in de-
termining the distance of the earth from the sun. If the plane
of the orbit of Venus coincided with the plane of the ecliptic,
a transit would occur whenever the planet came into inferior
conjunction, or once in every 584 days. Owing to the inclina-
tion of the planes to each other, however, it is evident that at
the time of inferior conjunction the planet m^y have too great a
latitude to touch any part of the sun's disc. Now the phenomenon
of a transit of Venus is analogous to a solar eclipse, and there-
166 TRANSITS OF VENUS.
fore if in Fig. 60 we suppose M to be Venus, the formula ob-
tained in Art. 160 will apply equally well to the limits of the
geocentric latitude of Venus within which a transit is possible.
These limits are the sum of the semi-diameters of the sun and
the planet and of the parallax of the planet, diminished by
the parallax of the sun. The greatest value of the limits will
be found to be about 17' 49". When, therefore, the latitude of
Venus is more than 17' 49" at the time of inferior conjunction,
no transit will occur : and as Venus in every sidereal revolution
attains a latitude of over 3 23', it is at once evident that a
transit is only a rare occurrence.
197. Intervals between Transits. Since the latitude of Venus
is so small when a transit occurs, it is plain that the planet must
be either at or very near one of its nodes. Now, let us suppose
that Venus is at its node at the time of inferior conjunction,
under which circumstances a transit will, of course, take place.
The sidereal period of Venus is 224.7 days. Now, we have,
224.7d. X 13 = 2921.11d.; and,
365.256d. X 8 = 2922.05d.
At the end of eight years, then, Venus will be very near the
same node at the time of inferior conjunction, and a transit will
probably occur. Again, we have,
224.7d. X 382 = 85835.4d.
365.256d. X 235 = 85835.16d. ;
so that transits at the same node also occur every 235 years. In
the same way transits may also occur at the other node: and the
intervals between transits at either node are found to be 8, 105<},
8, 12H, 8, &c. years.* The longitude of the ascending node of
Venus is 75 20', and a transit at that node must occur, when it
occurs at all, at the time when the earth is near that point, which
is about the 6th of June. For a similar reason transits at the
descending node occur about the 6th of December.
The last two transits occurred in June, 1769, and December,
1874. The next two will occur in December, 1882, and June,
2004. [See Table VIII., Appendix]
1
* Thus the years of transits at the ascending node are 1761, 1769, and
2004: at the descending noJe, 10^9, 1874, and 1882.
SUPERIOR PLANETS.
167
SUPERIOR PLANETS.
198. The superior planets are, as they have already been de-
fined to be, planets whose orbits include the orbit of the earth.
They have, like the inferior planets, superior conjunction, but
can evidently have no inferior conjunction. Their elongation
from the sun, eastern and western, can have all values between
and 180. When their elongation is 90, they are said to be in
quadrature, and when it is 180, in opposition. Much that has al-
ready been said in this chapter in reference to the inferior planets
is equally true in reference to the superior planets. The elements
of the orbits are in both instances the same, and so are the me-
thods by which the heliocentric longitudes of the nodes and the
inclinations of the orbits are determined. In some other points
there is a difference between the two classes of planets; and these
points we shall now proceed to examine.
199. Retrograde Motion. The superior planets, like the infe-
rior planets, have at times an apparent retrograde motion, which
N
Fig. 68.
occurs at or near the time of opposition. The explanation of
this retrogradation will be seen by a. reference to Fig. 68. S is
168 PERIODS OF A SUPERIOR PLANET.
the sun, EE'E"E" r the orbit of. the earth, and C GDP the orbit
of a superior planet, the plane of which is supposed to coincide
with the plane of the ecliptic, and to meet the celestial sphere in
the circle ANBM. Let the earth be at E, and the planet at P,
180 in geocentric longitude from the sun. The planet will ap-
pear to be projected upon the celestial sphere at the point M.
Let both earth and planet revolve in their orbits in the direction
indicated by the arrow. When the earth has reached the point
E r , the planet, whose angular velocity is less than that of the earth,
will have reached some point P', and will lie in the direction E'M':
in other words, it has apparently retrograded. If, on the other
hand, the earth is at E" and the planet at P, or in superior con-
junction, the apparent motion of the planet is at that point
direct, and its angular velocity appears to be greater than it
really is ; for when the earth is at E" r , and the planet at P', the
latter, having in reality moved through the arc MM" since con-
junction, appears to have moved through the arc MM'".
The apparent motion, then, of a superior planet is direct in
all cases except when it is at or near its opposition. The ap-
parent motion of an inferior planet has been shown to be retro-
grade at and near the time of inferior conjunction (Art. 186).
Now, since the earth is a superior planet to an inferior planet,
and an inferior planet to a superior planet, we see, by comparing
the two cases, that the retrograde motion occurs in each class
of planets at and near the time when the inferior planet conies
between the sun and the superior planet.
The stationary points in the orbit of a superior planet are
identical in character with those in the orbit of an inferior
planet, and occur when the retrograde motion is changing to the
direct motion, or the direct to the retrograde.
200. Synodical and Sidereal Periods. The synodical period
of a superior planet is the interval of time between two suc-
cessive conjunctions or two successive oppositions. When a planet
is in conjunction with the sun, it is above the horizon only in
the day time; but when it is in opposition, it is above the horizon
during the night, and can therefore be readily observed. Hence
in obtaining the synodical period it is better to employ the in-
terval of time between two oppositions: and by determining the
DISTANCE FROM THE SUN. 1H!)
times of two oppositions which are not consecutive, and div^ling
the interval between them by the number of synodical revo-
lutions which it contains, we may obtain a mean value of tK*?
synodical period. By using times of opposition which were ob-
served and recorded before the Christian era, a very accurate-
value of the mean synodical period may be obtained.
The method of deducing the periodic time from the synodica-'
period is the same that was used in the case of the inferio;
planets (Art. 192), with the important exception that in the
present case it is the earth that gains 360 upon the planet in the
course of a synodical revolution, and not the planet that gains it
upon the earth. If, therefore, we denote the periodic times of
the earth and the planet by Taud P, and the synodical period of
the planet by S, we shall have (Art. 141),
360 _ 360 _ 36i>, Sept. 23
1877
1873, JnlvlS
1871, Dec. 1
1835, Nov. 16
o t
334 31
113 31
101 46
245 57
148 27
209 40
268 54
55 10
1
13 05
10 48
29 45
12 34
13 56
11 22
54 32
17 45
0.847
0.755
0.802
0.756
0.660
0.558
0.830
0.967
2.22
3.14
3.14
3.50
3.44
3.81
6.03
17.99
1210
2020
2037
2415
2366
2715
4986
28000
Direct.
Direct.
Direct.
Direct.
Direct.
Direct.
Direct.
Ketro.
D' Arrest's....
leave's
Mechain's
Halley's
262
APPENDIX.
TABLE VIII.
TRANSITS OF THE INFERIOR PLANETS.
Mercury.
Venus.
1802.
November 8.
1639.
December 4.
1815.
November 11.
1761.
June 5.
1822.
November 4.
1769.
June 3.
1832.
May 5.
1874.
December 8.
1835.
November 7.
1882.
December 6.
1845.
May 8.
2004.
June 7.
1848.
November 9.
2012.
June 5.
1861.
November 11.
2117.
December 10.
1868.
November 4.
2125.
December 8.
1878.
May 6.
2247.
June 11.
1881.
November 7.
2255.
June 8.
1891.
May 9.
2360.
December 12.
1894.
November 10.
2368.
December 10.
TABLE IX.
LIST OF STARS WHOSE ANNUAL PARALLAX HAS BEEN
COMPUTED.
(All these are doubtful.)
Stars.
Parallax.
Distance in radii
of the Earth's
orbit.
Observer.
o. Centauri
0.92
224,000
Maclear. Henderson
61 Cygni
/ 0.35
589,000
Bessel.
21258 Lalande
17415 Oeltzen
(.0.56
0.27
025
368,000
764,000
825 000
Auvers.
Auvers.
Kriiger.
1830 Groombridge..
70 Ophiuchi
a Lyne
0.23
0.16
155
897,000
1,289,000
1 331 000
C. A. Peters.
Kr tiger.
W. & O. Struve.
Sirius
0150*
1 375,000
Henderson. Peters.
i Ursse Majoris..
A returns
Polaris
0.133
0.127
007
1,550,000
1,624,000
2 950,000
C. A. Peters.
C. A. Peters.
C. A. Peters.
Capella
005
4,130,000
C. A. Peters.
.
Another determination gives 0".23.
TABLES.
263
TABLE X.
THE PRINCIPAL CONSTELLATIONS.
Those found in Ptolemy's Catalogue (137 A.n.) are in Italics.
- THE NORTHERN CONSTELLATIONS.
No.
Name.
Coordinates of Centre.
R.A. D.
Name of
Principal Star of
1st or 2d magnitude.
Number
of stars of
1st mag.
Number 1
of stars
of first
ftve mag-
nitudes.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
29
h. m.
1
1 10
2
3 30
5 45
6
7 55
10 05
10 40
12 40
13
14 35
15
15 40
15 40
16 45
17 20
17 50
18 10
18 40
19 30
19 40
20
20 20
20 20
20 40
21
21 40
22 25
35
60
32
47
68
42
50
36
58
26
40
30
78
30
10
27
66
5
15 S.
35
10
18
25
42
44
15
6
65
15
Alpheratz (a)
Mirfak (a)
Capella (a)
Dubhe (a)
Cor Caroli (a)
Arcturus (a)
Polaris (a)
Unnkalhay (a)
Rasalgeti (a)
Thuban (a)
Vega (a)
Altair (a)
Deneb (a)
Markab (a)
1
1
1
1
1
1
18
46
5
40
36
35
28
15
53
20
15
35
23
19
23
65
80
6
4
18
33
5
23
67
13
10
5
44
43
Camelopa.rd.us
Aurioci
UTSCL J\fctjor
Coma Berenicis
Bootes
Corona Borealis
Draco
TaurusPoniatowskii
Clypeus Sobieskii...
Vulpecula et Anser.
Total
6
827
264
APPENDIX.
TABLE X. Continued.
THE ZODIACAL CONSTELLATIONS.
No.
1
2
3
4
5
6
7
8
9
10
11
12
12
Name.
Coordinates oi Centre.
K.A. P.
Name of
Principal Star of
1st or 2d magnitude.
Number
of stars of
1st laag.
Number
of stars
of first
five mag-
nitudes.
Aries
h. m.
2 30
4
7
8 40
10 20
13 20
15
16 15
18 55
21
22
20
18 N.
18
25
20
15
3N.
15 S.
26
32
20
9S.
ION.
Hamal (a)
Aldebaran (a)
f Castor (a)
\ Pollux (0)
Regulus (a)
Spica (a)
Zubenelg (a)
An tares (a)
SecundaGiedi(a)
Sadalmelik (a)
1
1
1
1
1
17
58
28
15
47
39
23
34
38
22
25
18
Taurus
Cancer
Libra
Scorpio
Sagittarius
JPisces
Total
5
364
THE SOUTHERN CONSTELLATIONS.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
n
18
19
20
21
Apparatus Sculptoris.
20
1
2
2 20
2 40
3 15
3 40
4
4 40
4 40
5 20
5 25
5 25
5 25
5 30
6 45
7
7 25
7 40
7 40
10
32
50
12
30
70
57
30
62
62
42
75
35
55
20
24
2
5
50
68
Menkar (a)
Achernar (a)
Phact (a)
Arneb (a)
Rigel (ft)
Sirius (a)
Procyon (a)
Canopus (a)
1
2
1
1
2
13
32
32
6
25
11
64
11
17
6
9
15
17
18
37
27
12
6
133
9
3
Qetus
Fornax Chemica . ...
Hvdrus
Horologiuni
Reticulus Rhomboidalis ..
Csjla Sculptoris
J^fons Mensae
Columba Noachi . ...
Equuleus Pictoris...
Lspus
Orion
Monoceros . ...
Canis Minor
Piscis Volaiis
Sextans
TABLES.
265
TABLE X. Continued.
THE SOUTHERN CONSTELLATIONS.
No
Name.
Coordinates of Centre.
R.A. D.
Name of
Principal Star of
1st or 2d magnitude.
Number
ofsta.rsof
1st mag.
Number
of stars
of first
five mag-
nitudes.
22
23
24
J25
26
27
28
29
30
31
32
33
34
35
36
37
33
39
40
41
42
43
44
45
h. m.
10
10
10 50
11 20
12 15
12 20
12 25
13
15
15 20
15 25
15 40
16
17
17
18 30
18 40
19 20
20 40
21
21
21 40
22 20
23 45
10
35
78
15
60
18
68
48
64
76
45
65
45
54
40
53
68
37
55
80
32
47
66
Alphard (a)
Algorab (a)
Rasalague (a)
Fomalhaut (a)
1
2
1
49
7
17
9
10
8
7
54
2
7
34
11
12
15
40
7
8
27
5
15
16
16
11
21
Antlia Pneumatica..
Cliamselcon
Crater
Crux
Corvus
Musca Australia
Circinus -
A pus
TriangulumAustrale
Norma
Ara
Corona Australls
Tel6scopium
Pavo
Indus ... ...
Octans
Piscis Australia
Toucan
45
86
1
Total
11
911
22
2102
23
266
APPENDIX.
TABLE XL
VARIABLE STARS.
Name.
Coordinates, 1870.
R.A. D.
Period in
Days.
Change of
Magnitude.
1
Authontj.
h. m. s.
o t
a Cassiopeise.
33 09
55 49.4 N
79.1
2 to 2.5
Birt, 1831
o Ceti ... .
2 12 47
3 34.1 S
331.34
2 " 12
D. Fabricius 1596
/?Persei
2 59 43
40 27.2 N
2.87
2.5" 4
Montanari, 1669
A Tauri
3 53 29
12 07.3 N
3.95
4" 4.5
Baxendell, 1848
e Aurigae
4 52 38
43 37.7 N
250.
3.5" 4.5
Heis, 1846
fj- Doradus....
5 05 47
61 58.4 S
Long.
5 " 9
Moesta, 1865
a Orionis
5 48 08
7 22.8 N
196.
1 " 1.5
J. Herscliel, 1836
C Gerainorum
6 56.24
20 45.5 N
10.16
3.8" 4.5
Schmidt, 1847
a Hydrse.
9 21 12
8 05.9 S
55.
2.5" 3
J. Herschel, 1837
R Leonis
9 40 34
12 01. 8 N
331.
5 "11.5
Koch, 1782
77 Argus
10 40 02
59 0.1 S
46yrs.
1 " 4
Burchell, 1827
R Hydra?
13 22 37
22 36.4 S
447.8
4 "10
Maraldi, 1704
Z Virginia....
13 27 45
1232.7 8
?
5 " 8
Schmidt, 1866
T Coronae
15 54 04
26 17.5 N
?
2.5" 9.8
Bermingham, 1866
30 Herculis...
16 24 22
42 10.1 N
106.
5 " 6
Baxendell, 1857
Nov. Ophiu...
16 52 13
12 41.4 S
?
4.5 " 13.5
Hind, 1848
a Herculis....
17 08 43
14 32.4 N
?
3.1" 3.9
W. Herschel, 1795
R Clyp. Sob.
18 40 33
5 50.5 S
89.
5 " 9
Pigotl, 1795
(3 Lyra?
18 45 17
33 12.7 N
12.91
3.5" 4.5
Goodricke, 1784
13 Lyra
18 51 23
43 46.6 N
46.
4.2" 4.6
Baxendell, 1855
^ 2 Cygni
19 45 34
32 35.2 N
409.2
5 "13
Kirch, 1686
T? Aquilse
19 45 51
040!4N
7.18
3.6" 4.4
Pigott, 1784
34 Cygni
20 13
37 37.8 N
18yrs.
3 " 6
Jansen, 1600
RCephei
20 23 41
8844. N
73 yrs.
5 "11
Pogson, 1851.
fj- Cephei
21 39 31
58 11.1 N
5 or 6yrs.
4 " 6
W. Herschel, 178S
6 Cephei
22 24 21
5745. N
5.37
3.7" 4.8
Goodricke, 1784
j3 Pegasi
22 57 28
27 22.', N
?
2 " 2.5
Schmidt, 184. 1
1
TABLES.
267
TABLE XII.
BINARY STARS.
Name.
Co-ordinates, 1870.
K.A. D.
Magnitude
of Com-
ponents.
Semi-
major
Axis.
Eccen-
tricity.
Period
in
Years.
Calculator.
Herculis. ...
h. m. a.
16 36
O f
3151 N
3 6
n
1.25
0.45
36.3
Villarceau.
rj CoronaeBor.
15 18
3047 N
6 6J
0.95
0.28
43.6
Winnecke.
f Cancri
8 04 45
18 02.4 N
6-7-7
1.29
0.23
58.9
Madler.
f UrsaeMaj...
11 11 15
3216 N
4 -6J
2.45
0.39
63.1
J. Breen.
a Centauri....
14 30 48
60 17.9 S
1 2
15.50
0.95
80.0
E.B.Powell.
w Leonis ......
9 21
939 N
6-7
0.85
0.64
82.5
Madler.
r Ophiuchi...
17 56
811 S
5 6
0.82
0.037
87.
Madler.
70 Ophiuchi..
17 58 52
2 22.5 N
4 7
4.19
0.44
92.8
Madler.
A Ophiuchi...
16 24
217 N
4 6
0.84
0.477
95.
Hind.
7 Coronas Aus.
I Bootis
18 57 38
14 45 22
19 41
37 14.7 S
19 38.5 N
4448 N
6 6
3i 9
2.54
12.56
1.81
0.60
0.59
0.60
100.8
117.1
178.7
Jacob.
J.Herschel.
Hind.
6 Cygni
ri Cassiopeiae .
41 09
57 07.8 N
4 -7*
10.33
0.77
181.
E.B.Powell.
7 Virginia... .
12 35 05
044.2S
4 4
3.58
0.87
182.1
J.Herschel.
o CoronseBor.
16 10
7 26 18
21 01 04
3412 N
32 10.4 N
38 05.1 N
6 6J
3 3J
5 6
2.71
8.08
15.4
0.30
0.75
195.1
252.6
452.
Jacob.
J.Herschel.
61 Cygni
fi Bootis
15 19 35
3750 N
4 8
3.21
0.84
649.7
Hind.
y Leonis
10 12 47
20 30.1 N
2 4
1200.
INDEX.
[The references are to the pages.]
Aberration of light, 116; diurnal and
annual, 117; separated from par-
allax, 221.
Acceleration, secular of the moon, 133.
Aerolites, 209.
Algol, 224.
Altazimuth, 39.
Altitude, 19.
Altitude and azimuth instrument, 38;
use of, 40.
Altitudes, method of equal, 39.
Amplitude, 19.
Andromeda, nebula in, 231.
Annular eclipse, 141.
Anomaly, 90.
Aphelion, 90.
Apogee, 122.
Appulse, 136.
Apsides, of earth, 116; of moon, 122;
of planets, 164.
Arc of meridian measured, 59.
Argo, nebula in, 234.
Aries, first point of, 20, 84.
Ascension, right, 20 ; related to sidereal
time, 22.
Asteroids, 171; table of, 260.
Astronomy, 11; chronology of, 248.
Atmosphere, height of, 52.
Attraction, law of, 108.
Axis, of the heavens, 15; of the earth,
17; of rotation and collimation, 32.
Azimuth, 19.
Base-line, 60.
Bode's law, 171.
Branches of meridian, 18.
Calendar, 105.
Centauri, alpha, distance of, 222; a
binary star, 227.
Centrifugal force, 65, 247.
Ceres, discovery of, 172.
Chronograph, 29.
Chronometer, Greenwich time given
by, 77.
Circle, vertical, 19 ; hour, 20 ; of per-
petual apparition, 20; diurnal, 24;
of latitude, 84.
Circle, meridian, 34; mural, 38; re-
flecting, 48.
Clock, astronomical, 28; driving, 41.
Clusters of stars, 229.
Coal sack, 234.
Collimation, axis of, 32.
Colures, 84.
Comets, 187; diversity of appearance,
188; tail, 1 89 ; orbits, 191 ; periods and
motion, 192 ; mass and density, 193 ;
light, 194; periodic, 195; Encke's,
195 ; Winnecke's or Pons's,197 ; Bror-
sen's, 197; Biela's, 197; D'Arrest's,
198; Faye's, 198; Mechain's, 199;
Halley 's, 199 ; Great, of 1 811 , 200 ; of
1843, 200 ; Donati's, 201 ; of 1861, 202 ;
connection with meteors, 211; ele-
ments of periodic, 261.
Compression, 63.
Conjunction, 126; inferior and supe-
rior, 159.
Constellations, 215; list of, 263.
Co-ordinates, spherical, 25.
Corona, 96.
Count, least, 47.
Crescent, 127.
Cross-wires, 32.
Culmination, 20.
Cycle, lunar, 133; of eclipses, 142.
Cygni, 61, its distance, 222.
Day, solar and sidereal, 21 ; inequality
of solar, 91; astronomical and civil,
105; intercalary, 106.
Declination, 20.
Degree of meridian, 62.
270
INDEX.
departure, 18.
Dip of the horizon, 57.
Dipper, 215.
Disc, spurious, of stars, 223.
Distance, zenith, 19,' polar, 20.
Earth, general form of, 12; spheroidal
form, 62; dimensions, 63; density,
Gibbous, 127.
Golden -number, 1 34.
Gravitation, universal, 107.
Heliocentric, parallax, 56, 156; motion
of planets, 157.
Hemisphere, 17.
Horizon, 13 ; points of, 19 ; artificial, 45.
Horizontal point, 36.
63; linear velocity of rotation, 70; Hour angle, 20; relation to sidereal
revolution about the sun, 88 ; orbital I time, 22.
velocity, 89; orbit, 89; motion at Hyades, 230.
perihelion and aphelion, 110; revo- Hyperbola, 245.
lution proved by aberration, 119;
phases, 127 ; elements, 257.
Eccentricity of an ellipse, 90.
Eclipses, 135; lunar, 135; solar, 139;
total, 142; cycle of, 142; number of,
143; of Jupiter's satellites, 174.
Ecliptic, 83.
Ecliptic limits, lunar, 137; solar, 141.
Elements, of planetary orbit, 160; of
^ometary, 190.
Ellipse, 244.
Elongation, 56 ; greatest eastern and
western, 159.
Equation, of centre, 102; of time, 104;
annual, 133.
Equator, 17; celestial, 19.
Equatorial, 40.
Equilibrium of centrifugal and centri-
petal forces, 107.
Equinoctial, 19.
Equinox, vernal, 20, 83.
Error of clock, 28.
Errors of observation, 49.
Establishment of port, 151.
Evection, 132.
Evening star, 160, 170.
Faculae, 96.
Finder, 34.
Flames, red, 97.
Forces, centrifugal and centripetal,247.
Foucault's experiment, 68.
Galaxy, 234.
Gemini, 216.
Geocentric, parallax, 55; motion of
planets, 155, 158, 167.
Incidence, angle of, 51.
Index correction, 44.
Jupiter, 173; mass of, 175.
Kepler 's laws, 111.
Kirkwood's law, 247.
Latitude, 18; equal to altitude of pole,
23 ; methods of determining, 72 ; at
sea, 75; reduction of, 75; celestial,
84.
Level, hanging, 34.
Librations, 131.
Light, analysis of, 48 ; of sun, 97; velo-
city of, 118 ; of planets, 183 ; of stars,
218; of nebulse, 230.
Line of sight, 32.
Longitude, 18; how determined, 76; by
telegraph, 78; by star signals, 79;
at sea, 80; celestial, 84; by eclipses
and occupations, 145.
Luculi, 96.
Lunar distance, 78.
Lunation, 128.
Magellanic clouds, 233.
Magnitudes, 214.
Mars, 170.
Mercury, 164; transits of, 262.
Meridian, 18; prime and celestial, 18;
line, 19.
Meteors, 202 ; showers, 203; height and
velocity, 205 ; orbits, 206 ; detonating,
208.
Microscope, reading, 35.
INDEX.
271
Milky way, 234.
Minor planets, 171 ; list of, 260.
Mira, or o Ceti, 223.
Moon, orbit of, 120 ; nodes, 120 ; obli-
quity of orbit, 121 ; form of orbit, 122;
line of apsides, 122; meridian zenith
distance, 122; distance, 123; magni-
tude and mass, 125; augmentation
of diameter, 125; phases, 126; side-
real and synodic periods, 128; retar-
dation, 129 ; harvest, 130 ; rotation,
130; librations, 131; other pertur-
bations, 132; general description,
134; elements, 257.
Morning star, 160, 170.
Motion, diurnal, 13; upward and
downward, 18; west to east, 88
(note); direct and retrograde, 159,
167.
Mural circle, 38.
Nadir, 18; point, 37.
Navigation, sketch of, 255.
Nebulae, resolvable and irresolvable,
230; annular and elliptic, 231 ; spiral
and planetary, 232 ; nebulous stars,
232; double, 232; variation of bright-
ness, 233.
Nebular hypothesis, 183.
Neptune, 182; immense distance of,
183.
Nodes, of moon's orbit, 120; heliocentric
longitude of planet's, 161.
Noon, 105.
Nubeculce, 233.
Nutation, 115.
Obliquity of ecliptic, 84, 115.
Occultation, 135, 144; of Jupiter's sa-
tellites, 174.
Octant, 48.
Gibers' s theory, 172.
Opposition, 126.
Qrion, 21 6.
Pendulum experiment, 68.
Penumbra, of solar spots, 95 ; of eolipsa
136.
Perigee, 122.
Perihelion, 90.
Perturbations, in earth's orbit, 112; in
moon's, 130.
Phases, of moon, 126 ; of earth, 127; of
Mercury and Venus, 165; of Mars,
171.
Photosphere, 95.
Planetoids, 171; list of, 260.
Planets, 155 ; orbits of, 157 ; inferior, 158j
stationary points, 159,168; elements
of orbit, 160; heliocentric longitude
of node, 161 ; inclination of orbit,
102; periods, 163,168; superior, 167 j
distance, 169 ; elements, 256.
Plateau's experiment, 185.
Pleiades, 230.
Points, fixed, 36.
Pointers, 216.
Poles, of the heavens, 15, 17; of the
earth, 17.
Pole-star, 14.
Position angle, 24.
Prcesepe, 230.
Precession, 112.
Problem of three bodies, 133.
Projections, spherical, 27.
Proper motions, 213.
Quadrant, 48.
Quadrature, 126.
Radiant points, 206.
Rate of clock, 28.
Refraction, 51; astronomical, 52; ge-
neral laws, 53; effects of, 54.
Resisting medium, 196.
Reticule, 32.
Reirogradation, 159, 167,
Rings of Saturn, 177; disappearance
of, 178.
Parabola, 246.
Parallax, geocentric and horizontal. 55:
heliocentric. 5G, 156; annual, 21<).
Pcqaxus, 216
os, 143.
Satellites, elements of, 258.
Saturn, 170; rings of, 177.
\SeaftonSf yo.
272
INDEX.
Sextant, 42 ; prismatic, 48.
Shadow, of earth, 136; of moon, 139.
Signs of zodiac, 84.
Sirius, light of, 223 j orbit of, 240.
Solar system, 11; orbit of, 238.
Solstices, 84.
Spectroscope, 48; use of, 97.
Sphere, celestial, 11; parallel, 16; right
and oblique, 17.
Spheroid, oblate, 63, 245.
Spots, solar, 95; observations of, 261.
Star signals, 79.
Stars, circumpolar, 14; fixed, 213;
number of, 214,234 ; magnitudes,214 ;
of first magnitude, 217 ; constitution,
218; distance, 218; differential ob-
servations, 220; real magnitudes,
222; variable and temporary, 223;
double and binary, 225 ; colored, 228;
examples of variable, 266; of binary,
267.
Stationary points, 159, 168.
Style, old and new, 106.
Sun, distance of, 84; magnitude, 87;
rotation, 95; constitution, 98; irreg-
ular advance, 102; first mean, 102;
second mean, 103; mass and density,
109; size compared with stars, 223;
motion in space, 235; elements, 256.
Synodical revolution, of moon, 128; of
planets, 163, 168.
Talcotfs method of finding latitude, 74.
Telegraph, used in determining longi-
tude, 78.
Telescopic comets, 188.
Tempel's comet, leads November
shower, 212.
Theodolite, 48.
Tides, 146; daily inequality, 148; ge-
neral laws, 149; influence of sun,
149; spring and neap, 150; priming
and lagging, 150; tidal wave, 151 j
establishment, 151; cotidal lines,
152; height, 152; four daily, 153,-
in lakes, 154.
Time, solar and sidereal, 21 ; sidereal
and right ascension, 22 ; Greenwich,
77 ; local time at different meridians,
81; astronomical and civil, 105.
Torsion balance, 63.
Trade-winds, 67.
Transit instrument, 31.
Transit, 20; of inferior planets, 262.
Triangle, astronomical, 23.
Triangulation, 60.
Twilight, 94.
Umbra, of solar spots, 95 ; of eclipses,
136.
Universal instrument, 48.
Uranus, 180.
Ursa, major, 215; minor, 216.
Vanishing points and circles, 26.
Variation, 133.
Venus, relative distances from sun and
earth, 84; transit of, 86, 165, 262; de-
scription of, 165.
Vernier, 46.
Vertical, lines, 18; prime, 19.
Vulcan, 157 (note).
Weight, in different latitudes, 64; on
the sun, 110.
rear, sidereal, 83; tropical, 105,114;
anomalistic, 116.
Zenith, 18; geographical and geocen-
tric, 76.
Zenith telescope, 48; use of, 74.
Zodiac, 84.
Zodiacal light, 99.
THE END.
14 DAY USE
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9 1962
LD 21A-50m-12,'60
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THE UNIVERSITY OF CALIFORNIA LIBRARY