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卷48 志二十三 时宪四

Volume 48 Treatises 23: Calendar 4

Chapter 48 of 清史稿 · Draft History of Qing
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1
Treatise 23
2
Shixian Calendar 4
3
Kangxi jiazi calendrical system — middle section
4
Constants for solar motion
5
The calendrical epoch is the winter solstice of the first month in jiazi year, Kangxi 23. That is the winter solstice of the eleventh month in the guihai year.
6
A full circuit of heaven comprises 360 degrees. Half the circuit gives a semicircle, a quarter gives a quadrant, and a twelfth gives a mansion; each degree contains sixty minutes, and seconds and still finer units below are all broken down by successive factors of sixty. In calculation the full circuit is expressed as 1,296,000 seconds.
7
The day-circle is divided into 10,000 parts. There are 24 hours, 96 quarters, 1,440 fractional parts beneath a quarter, and 86,400 seconds.
8
The tropical year is 365.2421875 days.
9
The sexagenary cycle divisor is 60.
10
宿
The lunar-mansion divisor is 28.
11
The sun's mean daily motion is 3,548 seconds, fractional remainder 0.3305169.
12
The apogee advances 61 seconds per year, fractional remainder 0.16666.
13
The apogee's daily motion is 0.0001 second plus 0.67469.
14
The deferent radius is 10,000,000.
15
The deferent epicycle radius is 268,812.
16
The equating epicycle radius is 89,604.
17
宿
Lodge longitudes appear in the Treatise on Astronomy.
18
Annual precession is 51 seconds.
19
西
North polar altitudes and longitudinal offsets for each province and Mongolia are listed in the Treatise on Astronomy.
20
Obliquity of the ecliptic: 23°29′30″.
21
Apogee epoch: 7°10′11.10″.
22
Solar-term epoch offset: 7.656374926 days.
23
宿
Lodge epoch offset: 5.656374926 days.
24
The ten day-stems: jia, yi, bing, ding, wu, ji, geng, xin, ren, and gui.
25
The twelve branches: zi, chou, yin, mao, chen, si, wu, wei, shen, you, xu, and hai.
26
宿
The twenty-eight lodges: Jiao, Kang, Di, Fang, Xin, Wei, Ji, Dou, Niu, Nü, Xu, Wei, Shi, Bi, Kui, Lou, Wei, Mao, Bi, Shen, Zi, Jing, Gui, Liu, Xing, Zhang, Yi, and Zhen.
27
Hour names: each of the twelve branches is split into early and exact halves. They run from exact zi through early night zi.
28
滿 滿 宿滿宿宿宿
To find the winter solstice of the civil year: take the tropical year constant, multiply by the number of years elapsed since the epoch (minus one) to obtain the mean accumulated interval, then add the solar-term epoch offset for total accumulated parts; when projecting backward into antiquity, subtract the solar-term epoch instead. Remove full sexagenary cycles from the day count; the remainder is the day-fraction for the civil-year winter solstice. For backward projection, subtract the remainder from the cycle divisor instead; what is left is the winter-solstice day-fraction. Count the day-stems from jiazi on day one; convert the fractional remainder via sub-quarter parts and reduce to hours and quarters. Use the 10,000-part day-circle as the first ratio, the fractional remainder as the second, and sub-quarter parts as the third; the fourth ratio gives the hour-fraction. Combine every 60 parts into one hour and every 15 parts into one quarter. Hours start at exact zi; add the lodge epoch to the mean accumulated interval and remove full mansion cycles to obtain the lodge day-fraction for the winter solstice, counting mansions from Jiao on the first day.
29
For mean motion: use the day-circle as the first ratio, the sun's daily mean motion as the second, and the winter-solstice fractional remainder minus the day-circle as the third; the fourth ratio is the year's-root in seconds. Multiply the sun's daily mean motion by the number of days from the current date to the day after the winter solstice to obtain seconds. Add this to the year's root and reduce to mansion, degree, and minute to obtain the mean longitude.
30
宿宿宿宿 宿退宿
For true motion: multiply the apogee's annual rate by the accumulated years. Multiply the apogee's daily rate by the days elapsed since the day after the winter solstice. Sum the two results and add the apogee epoch (subtract it when projecting backward). Subtract this from the mean longitude to obtain the equation argument. By plane triangle: let two-thirds of the deferent epicycle radius be the side opposite the right angle, take the equation argument as one angle, and double the side opposite that angle. Find the side opposite the other angle and add or subtract it from the deferent radius. If the argument falls in mansions 3–8, add; if in mansions 9–2, subtract. Apply another plane triangle with the doubled value as the short side and the deferent radius after addition or subtraction as the long side; the right angle lies between them, and the angle opposite the short side is the equation of center. Add or subtract the equation from the mean longitude: add for mansions 1–5, subtract for mansions 6–11. This yields the true longitude. For lodge longitude: multiply years elapsed by annual precession, add to the jiazi-epoch ecliptic lodge position to obtain this year's lodge pivot, subtract from the true longitude; the remainder is the sun's lodge position. If the true longitude is less than the lodge pivot, step back one lodge before subtracting.
31
宿滿 宿滿宿 宿宿
For the sexagenary day and its lodge: take days since the day after the winter solstice, add the solstice day-count, and remove full cycles of 60. Count day-stems from jiazi on day one, add the solstice lodge, and remove full cycles of 28 mansions. Starting mansions from Jiao on day one gives the cycle-day and its lodge.
32
滿 西
To find solar-term times: the sun's first mansion is Chou (Xingji). Degree 0 is the winter solstice; degree 15 is Lesser Cold. Mansion 1 is Zi (Yuanxiao). Degree 0 is Greater Cold; degree 15 is Beginning of Spring. Mansion 2 is Hai (Zouzi). Degree 0 is Rain Water; degree 15 is Awakening of Insects. Mansion 3 is Xu (Jianglou). Degree 0 is the spring equinox; degree 15 is Clear and Bright. Mansion 4 is You (Daliang). Degree 0 is Grain Rain; degree 15 is Beginning of Summer. Mansion 5 is Shen (Shichen). Degree 0 is Lesser Fullness; degree 15 is Grain in Ear. Mansion 6 is Wei (Chunshou). Degree 0 is the summer solstice; degree 15 is Lesser Heat. Mansion 7 is Wu (Chunhuo). Degree 0 is Greater Heat; degree 15 is Beginning of Autumn. Mansion 8 is Si (Chunwei). Degree 0 is End of Heat; degree 15 is White Dew. Mansion 9 is Chen (Shouxing). Degree 0 is the autumn equinox; degree 15 is Cold Dew. Mansion 10 is Mao (Dahu). Degree 0 is Frost's Descent; degree 15 is Beginning of Winter. Mansion 11 is Yin (Ximu). Degree 0 is Lesser Snow; degree 15 is Greater Snow. At exact zi, if the sun has not yet reached the term's mansion degree, that day is the term-entry day; if it has already passed that degree, term entry falls on the following day. Take the difference between today's and tomorrow's true longitudes as the first ratio, the daily sub-quarter parts as the second, and the gap between today's exact-zi true longitude and the term's mansion degree as the third; the fourth ratio is the interval after exact zi, which reduces to hours and quarters to give the term's early and exact times. If the true longitude exactly matches the term's mansion degree with no remainder, the term falls at exact zi in the first quarter. Provincial solar-term times are adjusted from the capital according to each place's longitudinal offset. Each degree of offset shifts the time by one quarter-hour. Add for places east of the capital, subtract for places west. For apparent solar-term time: convert the term-entry day's equation into a time correction and apply it with reversed sign. Next use the radius as the first ratio, the cosine of obliquity as the second, and the tangent of the term's ecliptic longitude as the third; the fourth ratio is the equatorial tangent. Look up the degree in the table, subtract from the ecliptic longitude, and convert the difference to the ascension time correction. Add after the equinoxes, subtract after the solstices. Apply both corrections to the mean term time to obtain apparent time. For ecliptic latitude: use the deferent radius as the first ratio, the sine of obliquity as the second, and the sine of the sun's distance from the equinoxes as the third; from mansion 1 degree 0 through the end of mansion 2, subtract mansion 3 — the remainder is before the spring equinox; From mansion 3 degree 0 through the end of mansion 5, subtract mansion 3 for the interval after the spring equinox. From mansion 6 degree 0 through the end of mansion 8, subtract mansion 9 for before the autumn equinox; From mansion 9 degree 0 through the end of mansion 11, subtract mansion 9 for after the autumn equinox. The fourth ratio is a sine; look it up in the table to obtain the latitude. For true motion in mansions 3–8, latitude is north of the equator; for mansions 9–2, latitude is south of the equator.
33
仿
For sunrise, sunset, and day-night length: use the deferent radius as the first ratio, the tangent of north polar altitude as the second, and the tangent of the day's ecliptic latitude as the third; the fourth ratio is a sine looked up in the table as the equatorial arc from Mao or You at rising and setting. Convert degrees to time at one quarter-hour per degree; all time conversions follow this rule. This gives the interval from Mao or You. Add or subtract from the Mao and You times to obtain sunrise and sunset. Before the spring equinox and after the autumn equinox, add to exact Mao for sunrise and subtract from exact You for sunset. After the spring equinox and before the autumn equinox, subtract from exact Mao for sunrise and add to exact You for sunset. Double the Mao-You interval and add or subtract it from the half-daylight value to obtain day and night lengths. After the spring equinox, add to get daylight quarters and subtract for night quarters; after the autumn equinox, reverse the operations.
34
Constants for lunar motion
35
The moon's mean daily motion is 47,435 seconds, fractional remainder 0.021177.
36
The moon advances four quarters per hour. Hourly mean motion is 1,976 seconds, fractional remainder 0.4592157.
37
The lunar apogee moves 401 seconds per day, fractional remainder 0.077477.
38
The ascending node moves 190 seconds per day, fractional remainder 0.64.
39
Deferent epicycle radius: 580,000.
40
Equating epicycle radius: 290,000.
41
Auxiliary circle radius: 797,000.
42
Secondary epicycle radius: 217,000.
43
Secondary equating epicycle radius: 117,500.
44
Ecliptic-lunar latitude at syzygy: 4°58′30″.
45
Ecliptic-lunar latitude at quadrature: 5°17′30″.
46
Mean ecliptic-lunar latitude: 5°08′.
47
Half-variation of ecliptic-lunar latitude: 9′30″.
48
Lunar mean-motion epoch: 1 mansion 8°40′57.16″.
49
Lunar apogee epoch: 3 mansions 4°49′54.09″.
50
Node epoch: 6 mansions 27°13′37.48″.
51
To find the civil-year winter solstice for lunar motion, use the same method as for solar motion.
52
滿 滿
For lunar mean motion: take the mean accumulated interval and add the solar-term epoch offset, as described under solar motion. Use only the fractional remainder, not the day count; the same applies below. Subtract the winter-solstice fractional remainder to obtain accumulated days. When projecting backward, subtract the solar-term fractional remainder and add the winter-solstice fractional remainder. Multiply by the moon's daily mean motion, remove full circuits of heaven in seconds, and reduce the remainder to mansions, degrees, and minutes. Add to the lunar mean-motion epoch to obtain the year's root. Subtract when projecting backward; multiply the moon's daily mean motion by days since the day after the winter solstice to obtain seconds. Reduce to mansions, degrees, and minutes, add to the year's root, and remove full cycles of twelve mansions. This is the lunar mean longitude.
53
滿 滿
For lunar apogee motion, use accumulated days as above; the same applies below. Multiply by the apogee's daily rate, remove full circuits in seconds, and reduce the remainder to mansions, degrees, and minutes. Add to the apogee epoch to obtain the apogee year's root. Subtract when projecting backward. Multiply the apogee's daily rate by days since the day after the winter solstice, reduce to mansions, degrees, and minutes, add to the year's root, and remove full twelve-mansion cycles. This is the lunar apogee longitude.
54
滿
For the node's mean motion: multiply accumulated days by the node's daily rate, reduce to mansions, degrees, and minutes, and subtract from the node epoch; if the epoch is too small, add twelve mansions before subtracting. This gives the node's year's root. Add when projecting backward. Multiply the node's daily rate by days since the day after the winter solstice, reduce to mansions, degrees, and minutes, and subtract from the year's root; if needed, add twelve mansions before subtracting. This is the node's mean longitude.
55
For the moon's mean longitude at apparent time: convert the sun's equation to a time correction, as under solar motion. This yields the equation time correction. If the equation is added, the time correction is subtracted; if the equation is subtracted, the time correction is added. Also obtain the sun's ecliptic and equatorial longitudes for the day, as under solar motion. Subtract them and convert the difference to the ascension time correction. Add after the equinoxes, subtract after the solstices. Combine the two time corrections to obtain the total time difference. If both corrections share the same sign, add them; addition stays addition and subtraction stays subtraction. If the signs differ, subtract the smaller from the larger and take the sign of the larger value. Convert the total to seconds, multiply by the moon's hourly mean motion, divide by the seconds in one degree, and reduce the result to degrees and minutes as the time-difference displacement. Apply it to lunar mean motion with reversed sign: subtract if the total correction adds, add if it subtracts. This is the lunar mean longitude at apparent time.
56
For the first true longitude: subtract the apogee longitude from the apparent-time mean longitude to obtain the equation argument. By plane triangle: use half the deferent epicycle radius as the side opposite the right angle, take the equation argument as one angle, and triple the opposite side. Find the side opposite the other angle and add or subtract it from the deferent radius. Add for argument mansions 9–2, subtract for mansions 3–8. Apply another plane triangle with the tripled value as the short side and the adjusted deferent radius as the long side; the angle opposite the short side is the first equation, and the side opposite the right angle is also found. This is the line from Earth's center to the secondary epicycle's nearest point. Add or subtract the first equation from the apparent-time mean longitude: subtract for mansions 1–5, add from mansion 6 onward. This is the first true longitude.
57
For true lunar latitude motion: subtract the sun's true longitude from the first true longitude to obtain the secondary argument. This is the elongation from the sun. By plane triangle: one side is the line to the secondary epicycle's nearest point; use double the secondary argument's versed sine with deferent radius as the first ratio, the sine of the secondary argument as the second, and the secondary epicycle radius as the third; double the fourth ratio to obtain the chord. As one side; Combine the first equation with the argument reduced by a semicircle: if the argument is less than 180°, subtract it from 180°; if greater, subtract 180°. Add these, then take the secondary argument's distance from a quadrant: if less than 90°, subtract from 90°; if beyond 90° or 270°, subtract 90° or 270° and use the remainder; if beyond 180°, subtract 180° and again subtract from 90° to obtain the secondary argument's quadrant distance. Combine them: if the first equation subtracts, add when the secondary argument exceeds 90° or 270°, subtract otherwise. Reverse the rule when the first equation adds. This is the included angle; if the sum exceeds 180°, subtract from 360°. If the sum is exactly 180° or subtraction leaves zero, there is no second equation. There is also no second equation if the secondary argument is at 0° or exactly 180°. The angle opposite the chord is the second equation; without a first equation, use the line to the secondary epicycle center and the secondary epicycle radius as the two sides; take double the secondary argument as the included angle, reducing by 360° if it exceeds 180°; use the interior angle at apogee and the exterior at perigee; the angle opposite the secondary epicycle radius is the second equation. Determine the sign of addition or subtraction accordingly. Add the first equation to the arc from the equating epicycle center to perigee to obtain the general comparison limit. If the general limit is exactly 90°, the second equation has the same sign as the first. If less than 90°, subtract from 90° and double the remainder for the fixed comparison limit. If the first equation subtracts, compare the doubled secondary argument; if the first equation adds, compare the remainder of double the secondary argument minus 360° against the fixed limit. If the general limit exceeds 90°, subtract 90° and double the remainder for the fixed limit. If the first equation adds, compare the doubled secondary argument; if the first equation subtracts, compare the remainder of double the secondary argument minus 360° against the fixed limit. If the value exceeds the fixed limit, the second equation matches the first in sign; if less, the sign is reversed. The side opposite the angle is the line from Earth's center to the secondary equating epicycle center. With this line and the secondary argument, form a plane triangle using the line to the secondary equating epicycle center and its radius as sides and double the secondary argument as the included angle, reducing by 360° if needed. The angle opposite the secondary equating epicycle radius is the third equation; determine its sign accordingly. Add if double the secondary argument is under 180°, subtract if over. Combine the second and third equations to obtain the combined second-third correction. If both equations share a sign, add them; if their signs differ, subtract. Apply the result to the first true longitude: if both equations add, add; if both subtract, subtract. If one equation adds and the other subtracts, take the sign of the larger term. This is the true lunar-path longitude.
58
For true ecliptic longitude, solve a spherical triangle with the mean lunar latitude, the latitude half-difference, and double the secondary argument as the included angle, reducing by 360° if needed. The side opposite the angle gives the lunar latitude; the angle opposite the half-difference is the node equation. Apply the node equation to the node's mean longitude: subtract if double the secondary argument is under 180°, add if over. This gives the true node longitude. Add or subtract six mansions for the middle-node longitude; subtract the node longitude from the lunar-path true longitude to obtain the arc from the node. Use the deferent radius as the first ratio, the cosine of lunar latitude as the second, and the tangent of the arc from the node as the third; the fourth ratio is the ecliptic tangent. Look up degrees and minutes in the table and subtract from the arc from the node to obtain the ascension difference, then apply it to the lunar-path longitude: subtract if the arc is within one or two quadrants of the node, add if within one or three. This is the true ecliptic longitude.
59
For ecliptic latitude, use the deferent radius as the first ratio, the sine of lunar latitude as the second, and the sine of the arc from the node as the third; the fourth ratio is the sine. Look up the ecliptic latitude in the table; the latitude is north from mansions 0–5 of the arc from the node and south from mansions 6–11.
60
宿宿宿 宿宿宿
For the four lodge longitudes, use the solar-motion lodge method to obtain this year's ecliptic lodge pivot. For each of the ecliptic, apogee, node, and middle-node longitudes, subtract the appropriate lodge from the pivot wherever possible; the remainders are the four lodge positions.
61
宿
For the lodge of the sexagenary day, use the same method as for solar motion.
62
For the time the moon crosses a node mansion, compare today's and tomorrow's true longitudes: if the crossing has not yet occurred, use today; if it has, use tomorrow. Take the remainder as the first ratio and the fractional minutes as the second; use today's true longitude without its mansion. Subtract from 30° for the third ratio; the fourth ratio is the time from midnight. Reduce by the standard method to obtain the node-crossing time.
63
For moonrise and moonset, convert the sun's ecliptic longitude for the day to the corresponding equatorial longitude. Next solve a spherical triangle with the moon's distance from the ecliptic pole and the obliquity as sides. Take the moon's ecliptic longitude from the winter solstice as the exterior angle, reducing by 360° if it exceeds 180°. The opposite side gives the moon's polar distance. Subtract from 90° to obtain equatorial declination. If under 90°, subtract from 90°; the remainder is north declination. If over 90°, subtract 90°; the remainder is south declination. The angle at the north pole gives the moon's equatorial longitude from the winter solstice. Use the deferent radius as the first ratio, the tangent of the observer's latitude as the second, and the tangent of the moon's declination as the third; the fourth ratio is the sine. Look up the equatorial degrees before and after Mao and You for moonrise and moonset; north of the equator, the moon rises before Mao and sets after You; south of the equator, it rises after Mao and sets before You. Apply the correction: subtract before the cardinal point, add after. The moon's elongation in equatorial longitude is the moon's equatorial longitude minus the sun's. Convert the result to time. Measure from after Mao for rising and from after You for setting. Find the base time, then add the time for the moon's motion in the current hour — about 30′ of motion per hour, converted to two fractional hours. This gives moonrise and moonset.
64
For new moon and the quarters and full moon: conjunction is when the moon and sun share mansion and degree; limits fall three, six, and nine mansions apart for first quarter, full moon, and last quarter — use today if the moon has not reached the limit, tomorrow if it has. Subtract today's and tomorrow's true longitudes for moon and sun; take the ratio of the remainders as the first ratio and the fractional minutes as the second; add the limit to today's solar longitude — three mansions for first quarter, six for full moon, nine for last quarter. Subtract today's lunar longitude for the third ratio; the fourth ratio is the time from midnight. Reduce by the standard method to obtain the times of new moon and the quarters and full moon.
65
For direct, oblique, and horizontal ascension on new-moon day: direct from Zi 15° to You 15°, oblique from You 15° to Wei 0°, horizontal from Wei 0° to Yin 15°, oblique from Yin 15° back to Zi 15°.
66
For month length, compare the preceding and following new moons: if the day stem matches, the preceding month is long (30 days); if not, short (29 days).
67
For the intercalary month, use the months containing winter solstice in the surrounding years as the standard. When thirteen mean months accumulate, intercalate after the month without a mid-term qi, following the preceding month. If two months in one year lack mid-term qi, intercalate after the first such month.
68
Constants for Saturn
69
Mean motion 120 seconds per day, fractional remainder 0.6022551.
70
Apogee motion is 0.0002 second plus 0.195803 per day.
71
Node motion is 0.0001 second plus 0.146728 per day.
72
Deferent radius 865,587.
73
Equating epicycle radius 296,413.
74
Secondary epicycle radius 1,042,600.
75
Orbital inclination to the ecliptic: 2°31′.
76
Saturn mean-motion epoch: 7 mansions 23°19′44.55″.
77
Apogee epoch: 11 mansions 28°26′6.05″.
78
Node epoch: 6 mansions 21°20′57.24″.
79
Constants for Jupiter
80
Mean motion 299 seconds per day, fractional remainder 0.2852968.
81
Apogee motion is 0.0001 second plus 0.58433 per day.
82
Node motion is 0.0003 second plus 0.723557 per day.
83
Deferent radius 705,320.
84
Equating epicycle radius 247,980.
85
Secondary epicycle radius 1,929,480.
86
Orbital inclination to the ecliptic: 1°19′40″.
87
Jupiter mean-motion epoch: 8 mansions 9°13′13.11″.
88
Apogee epoch: 9 mansions 9°51′59.27″.
89
Node epoch: 6 mansions 7°21′49.35″.
90
Constants for Mars
91
Mean motion 1,886 seconds per day, fractional remainder 0.6700358.
92
Apogee motion is 0.0001 second plus 0.834399 per day.
93
Node motion is 0.0001 second plus 0.449723 per day.
94
Deferent radius 1,484,000.
95
Equating epicycle radius 371,000.
96
Minimum secondary epicycle radius 6,302,750.
97
Deferent eccentricity range: 258,500.
98
Solar eccentricity range: 235,000.
99
Orbital inclination to the ecliptic: 1°50′.
100
Mars mean-motion epoch: 2 mansions 13°39′52.15″.
101
Apogee epoch: 8 mansions 0°33′11.54″.
102
Node epoch: 4 mansions 17°51′54.07″; see solar motion for the remainder.
103
Methods for Saturn, Jupiter, and Mars
104
For the civil-year winter solstice, use the same method as for solar motion.
105
滿
For the three planets' mean longitudes, use accumulated days as in the lunar-motion section. Multiply by the planet's daily mean rate, reduce modulo a full circuit in seconds, and collect as mansions, degrees, and minutes to obtain the mean motion from accumulated days. Add to the planet's mean-motion epoch to obtain its year's root. Subtract when projecting backward. Multiply the planet's daily mean rate by days since the day after the winter solstice, add to the year's root, and obtain the planet's mean longitude.
106
For apogee longitude: multiply accumulated days by the planet's apogee daily rate, add to the apogee epoch, and obtain the apogee year's root. Subtract when projecting backward. Multiply the planet's apogee daily rate by days since the day after the winter solstice, add to the year's root, and obtain the apogee longitude.
107
For node longitude: multiply accumulated days by the planet's node daily rate, add to the node epoch, and obtain the node's year's root. Subtract when projecting backward. Multiply the planet's node daily rate by days since the day after the winter solstice, add to the year's root, and obtain the node longitude.
108
For the first true longitude: subtract apogee longitude from mean longitude to obtain the equation argument. Form a plane triangle with the deferent minus equating epicycle radius as the side opposite the right angle and the equation argument as one angle; solve for the remaining sides. Next add the side opposite the equation-argument angle to the equating epicycle chord by the chord method, as in the lunar-motion section. This is the small side; add or subtract the other side and the deferent radius — subtract for argument mansions 3–8, add for mansions 9–2. This is the large side; with the right angle between them, the angle opposite the small side is the first equation. Also obtain the side opposite the right angle as the secondary epicycle center's geocentric distance; apply the first equation to the planet's mean longitude — subtract for argument mansions 0–5, add for mansions 6–11. This gives the planet's first true longitude.
109
For true longitude in the planet's own path: subtract the planet's first true longitude from the sun's true longitude that day to obtain the secondary argument. This is the elongation from the sun. Form a plane triangle with the secondary epicycle center's geocentric distance as one side and the secondary epicycle radius as the other — Mars's secondary epicycle radius alone varies; see below. Take the secondary argument as the exterior angle; if it exceeds a semicircle, subtract from a full circuit and use the remainder. The angle opposite the secondary epicycle radius is the second equation; the side opposite the secondary-argument angle is the star's geocentric distance. Apply the second equation to the first true longitude with the sign opposite to the first equation. This gives the planet's true longitude in its own path. For Mars's true secondary epicycle semidiameter: use Mars's primary epicycle diameter (20,000,000) as the first ratio, the primary-heaven great high-low difference as the second, the versed sine of the equating epicycle center's perigee distance as the third, and the equation argument subtracted from a semicircle as the perigee distance in degrees. The fourth ratio is the primary-heaven high-low correction. Next use the sun's primary epicycle diameter (20,000,000) as the first ratio, the solar great high-low difference as the second, and the versed sine of that day's solar equation argument as the third; if the argument exceeds a semicircle, subtract from a full circuit and use the remainder. The fourth ratio is the solar high-low correction. Add both high-low corrections to Mars's minimum secondary epicycle semidiameter to obtain its true secondary epicycle semidiameter.
110
For ecliptic true longitude: subtract the planet's node longitude from its first true longitude to obtain the arc from the node. This is the secondary epicycle center's arc from the node. Use primary heaven radius as the first ratio, the cosine of the planet-path/ecliptic angle as the second, and the tangent of the arc from the node as the third; the fourth ratio is the tangent. Look up ecliptic degrees from the table, subtract from the arc from the node to get the ascension difference, and apply it to true longitude in the planet's path — subtract when the node arc is within a quadrant or passes two quadrants; add when it passes one or three quadrants. This gives the planet's ecliptic true longitude.
111
For apparent latitude: use primary heaven radius as the first ratio, the sine of the planet-path/ecliptic angle as the second, and the sine of the arc from the node as the third; look up the resulting sine for the preliminary latitude. Next use primary heaven radius as the first ratio, the sine of the preliminary latitude as the second, and the secondary epicycle center's geocentric distance as the third; the fourth ratio is the star's distance from the ecliptic. Then use the star's geocentric distance as the first ratio, its distance from the ecliptic as the second, and primary heaven radius as the third; the fourth ratio is the sine. Look up the planet's apparent latitude and assign north or south accordingly. Node arcs in mansions 0–5 place the planet north of the ecliptic; mansions 6–11, south.
112
宿
For ecliptic lodge degree and sexagenary day assignment, use the solar-motion method.
113
For the moment of node mansion crossing, use the lunar-motion method.
114
退退 退退退 退
For the fixed morning/evening visibility limits of the three planets: conjunction and invisibility occur when the planet's and sun's ecliptic true longitudes share the same mansion and degree. After conjunction/invisibility, increasing solar separation brings morning visibility in the east under direct motion. Direct motion slows until it stations and turns retrograde. Early retrograde at semicircular solar separation is opposition in retrograde; evening visibility begins the next day. Retrograde motion slows until it stations and turns direct again. Direct motion accelerates as the planet again approaches the sun until conjunction/invisibility — evening invisibility. Visibility limits: Saturn 11°, Jupiter 10°, Mars 11°30′. When solar and planetary true longitudes on some day near conjunction/invisibility approach this limit, take the planet's ecliptic true longitude that day and solve a spherical triangle with the equator-horizon angle known — for evening visibility after the spring equinox use the interior angle, after the autumn equinox the exterior angle; For morning visibility, reverse the rule. Take the true longitude's distance from the equinoxes as one opposite side and the great yellow-red distance as a known angle; solve for the other opposite side. With two known sides opposite two known angles, solve for the remaining angle — for evening, use the interior angle after the autumn equinox and the exterior angle after the spring equinox; For morning visibility, reverse the rule. This gives the limit height above the horizon. Next form a spherical right triangle with the ecliptic-horizon angle equal to the limit height above the horizon. With the planet's visibility limit as the arc opposite the crossing angle, the arc opposite the right angle is the ecliptic elongation from the sun. If the star lies on the ecliptic with no latitude offset, that value is the fixed limit. Again use a spherical right triangle with the ecliptic-horizon angle; take the planet's ecliptic latitude as the arc opposite the crossing angle; the arc between the angles is the correction. Apply this correction to the ecliptic elongation from the sun — add for south latitude, subtract for north. This yields the fixed visibility limit. When the planet's solar separation nears the fixed limit: if this occurs before conjunction/invisibility on a given day, that day is evening invisibility; if after conjunction/invisibility on a given day, that day is morning visibility.
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For the moment of conjunction/invisibility: if the sun's true longitude is about to reach the planet's, the event falls on that day; if it has already passed the planet's true longitude, the next day. For the time fraction, use the sun's daily true motion — the difference between this day's and the next day's true longitudes. Use the planet's daily true motion as the divisor for the first ratio; proceed as in the lunar-motion section for new and full moon.
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For opposition in retrograde: when ecliptic separation of planet and sun approaches a semicircle, the event falls on that day; if a semicircle has already been exceeded, the next day. For the time fraction, add the sun's and planet's daily true motions as the first ratio; proceed as before for the remainder.
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For the moment of equal longitude: combine the two bodies' daily true motions — subtract when both move in the same direction. Add when one is direct and the other retrograde. That sum is the first ratio, fractional parts under a quarter the second, the bodies' separation the third; the fourth ratio is the fraction from midnight — convert to hours and quarters. The same method applies to all five planets.
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Constants for Venus
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Mean motion 3,548 seconds per day, fractional remainder 0.3305169.
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Apogee daily rate: two parts in ten thousand of a second plus 0.271095.
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Visibility mean motion 2,219 seconds per day, fractional remainder 0.4311886.
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Primary epicycle radius: 231,962.
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Equating epicycle radius: 88,852.
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Secondary epicycle radius: 7,224,850.
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Secondary epicycle plane/ecliptic angle: 3°29′.
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Venus mean-motion epoch: 0 mansions 0°20′19.18″.
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Apogee epoch: 6 mansions 1°33′31.04″.
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Visibility epoch: 0 mansions 18°38′13.06″.
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Constants for Mercury
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Daily mean motion matches Venus.
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Apogee daily rate: two parts in ten thousand of a second plus 0.881193.
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Visibility mean motion 11,184 seconds per day, fractional remainder 0.1165248.
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Primary epicycle radius: 567,523.
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Equating epicycle radius: 114,632.
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Secondary epicycle radius: 3,850,000.
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At greatest elongation the secondary epicycle center/ecliptic angle is 5°40′.
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仿
At the node the ecliptic angle is 5°05′10″ north; the crossing-angle differential is 34′50″. Compare with the greatest-elongation angle; follow this pattern below. South 6°31′02″; crossing-angle differential 51′02″.
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At the middle node the ecliptic angle is 6°16′50″ north; crossing-angle differential 36′50″. South 4°55′32″; crossing-angle differential 44′28″.
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Mercury mean-motion epoch matches Venus.
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Apogee epoch: 11 mansions 3°03′54.54″.
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Visibility epoch: 10 mansions 1°13′11.17″; see solar motion for the remainder.
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Methods for Venus and Mercury
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For the civil-year winter solstice, use the same method as for solar motion.
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For Venus and Mercury mean longitudes, use the Saturn, Jupiter, and Mars method.
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For Venus and Mercury apogee longitudes, use the Saturn, Jupiter, and Mars method.
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For Venus and Mercury visibility mean motion, use each planet's mean-longitude method.
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For node longitude: from the planet's apogee mean longitude, subtract 16° for Venus or add/subtract six mansions for Mercury.
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For Venus's first true longitude: derive the first equation from the equation argument and apply it to mean longitude. Finding the secondary epicycle center's geocentric distance follows the Saturn, Jupiter, and Mars method.
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For Mercury's first true longitude: form a plane triangle with primary and equating epicycle radii as sides and triple the equation argument as the exterior angle; if it exceeds a semicircle, subtract from a full circuit and use the remainder. Solve for the side opposite the angle and the angle opposite the equating epicycle radius. Next form a plane triangle with primary heaven radius as the large side and the opposite side as the small side; combine the angle opposite the equating epicycle radius with the equating epicycle center's perigee distance — if the argument is less than a semicircle, subtract from a semicircle; if it exceeds a semicircle, subtract a semicircle to obtain the perigee distance in degrees. Add when triple the equation argument is less than a semicircle; subtract when it exceeds one. With that as the contained angle, the angle opposite the small side is the first equation and the side opposite the angle is the secondary epicycle center's geocentric distance. Apply the first equation to Mercury's mean longitude — subtract for argument mansions 0–5, add for mansions 6–11. This yields Mercury's first true longitude.
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For Venus and Mercury visibility true longitude: take visibility mean motion and apply the first equation, adding for mansions 1–5 and subtracting for mansions 6–11. This gives the result.
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For ecliptic true longitude of Venus and Mercury: form a plane triangle with the line to the secondary epicycle center and its radius as sides and visibility true longitude as the exterior angle, reducing by 360° if over 180°. The angle opposite the secondary epicycle radius is the second equation, and the opposite side is the planet's geocentric distance. Apply the second equation to the first true longitude, adding for visibility mansions 1–5 and subtracting for 6–11. This yields the planet's ecliptic true longitude.
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For distance from the node: subtract the node's longitude from the first true longitude. Add visibility true longitude to obtain distance from the secondary node.
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For apparent latitude: use deferent radius as the first ratio and the sine of the secondary epicycle–ecliptic crossing angle as the second; Venus uses a fixed angle, but Mercury needs the true crossing angle computed below. Use the sine of distance from the secondary node as the third ratio, look up the fourth ratio in the table for secondary latitude. Next use deferent radius, sine of secondary latitude, and secondary epicycle radius to obtain the planet's distance from the ecliptic. Then use geocentric distance, ecliptic distance, and deferent radius to look up apparent latitude and assign north or south. Mansions 1–5 are north of the ecliptic, mansions 6–11 are south.
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For Mercury's true orbital inclination: use radius 10,000,000 and the crossing-angle difference in seconds; apply the ascending-node difference for mansions 9–2 and the mid-node difference for 3–8, according to hemisphere. The sine of distance from the node gives the crossing-angle correction. Take the nominal crossing angle; apply the correction by the same procedure as the crossing-angle difference. Apply the correction: for mansions 9–2, add if north of the ecliptic and subtract if south; reverse for mansions 3–8. This yields the true crossing angle.
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宿
For ecliptic lodge longitude and sexagenary day, use the solar-motion method.
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For node-crossing time, use the lunar-motion method.
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For Venus and Mercury visibility limits: conjunction-invisibility occurs when planet and sun share the same longitude; afterward the planet moves away from the sun; it appears in the west at dusk, moving direct but ever slower until it stations and turns retrograde. Retrograde motion brings it back toward the sun until evening visibility ends at conjunction-retrograde-invisibility. It then separates from the sun again and appears in the east at dawn. Still retrograde, it slows until it stations and resumes direct motion. Direct motion accelerates as it nears the sun again to conjunction-invisibility, ending morning visibility. Visibility limits are 5° for Venus and 10° for Mercury. Find the fixed limit as for the outer planets by comparing solar elongation to the limit. The day before conjunction-invisibility when the limit is reached is morning invisibility; the day after conjunction-invisibility when the limit is reached is evening visibility; before conjunction-retrograde-invisibility is evening invisibility; after conjunction-retrograde-invisibility is morning visibility.
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For conjunction-invisibility time: if the planet is about to catch the sun, the event is today; if it has passed, tomorrow. Compute the moment by the same method used for new and full moons.
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For conjunction-retrograde-invisibility: if the sun is about to catch the planet, the event is today; if it has passed, tomorrow. Compute the moment by the outer-planet retrograde-opposition method.
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Constants for fixed stars
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See under solar motion.
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For fixed-star ecliptic longitude: multiply years since Kangxi renzi (minus one) by annual precession. Reduce to degrees and minutes and add to the Kangxi renzi star-table longitudes for each star's current ecliptic longitude. For equatorial coordinates: use a spherical triangle with polar distance, obliquity, and the star's distance from the summer solstice as the included angle. Before the summer solstice use the value directly; after, subtract from 360°. Count equatorial longitude from the start of the Xingji mansion. The side opposite the original angle minus 90° gives equatorial latitude. If the star is inside the quadrant the latitude is north; if outside, south.
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For the culminating star: proportion from sub-quarter parts, the sun's daily motion, and the given time to obtain the sun's ecliptic longitude at that moment. Derive solar equatorial longitude by spherical triangle, converting time to arc at 15° per hour, 15′ per minute, and 15″ per second. Adjust by 180°: add if under 180°, subtract if over. This gives the sun's hour-angle from noon. Add to solar equatorial longitude to obtain the meridian's equatorial longitude at that moment. The fixed star whose equatorial longitude matches is the star on the meridian.
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