1 | ;
|
2 |
|
3 | Object.defineProperty(exports, "__esModule", {
|
4 | value: true
|
5 | });
|
6 |
|
7 | var _slicedToArray = function () { function sliceIterator(arr, i) { var _arr = []; var _n = true; var _d = false; var _e = undefined; try { for (var _i = arr[Symbol.iterator](), _s; !(_n = (_s = _i.next()).done); _n = true) { _arr.push(_s.value); if (i && _arr.length === i) break; } } catch (err) { _d = true; _e = err; } finally { try { if (!_n && _i["return"]) _i["return"](); } finally { if (_d) throw _e; } } return _arr; } return function (arr, i) { if (Array.isArray(arr)) { return arr; } else if (Symbol.iterator in Object(arr)) { return sliceIterator(arr, i); } else { throw new TypeError("Invalid attempt to destructure non-iterable instance"); } }; }(); /**
|
8 | * @copyright 2013 Sonia Keys
|
9 | * @copyright 2016 commenthol
|
10 | * @license MIT
|
11 | * @module node
|
12 | */
|
13 | /**
|
14 | * Node: Chapter 39, Passages through the Nodes.
|
15 | */
|
16 |
|
17 | exports.ellipticAscending = ellipticAscending;
|
18 | exports.ellipticDescending = ellipticDescending;
|
19 | exports.el = el;
|
20 | exports.parabolicAscending = parabolicAscending;
|
21 | exports.parabolicDescending = parabolicDescending;
|
22 | exports.pa = pa;
|
23 |
|
24 | var _base = require('./base');
|
25 |
|
26 | var _base2 = _interopRequireDefault(_base);
|
27 |
|
28 | function _interopRequireDefault(obj) { return obj && obj.__esModule ? obj : { default: obj }; }
|
29 |
|
30 | /**
|
31 | * EllipticAscending computes time and distance of passage through the ascending node of a body in an elliptical orbit.
|
32 | *
|
33 | * Argument axis is semimajor axis in AU, ecc is eccentricity, argP is argument
|
34 | * of perihelion in radians, timeP is time of perihelion as a jd.
|
35 | *
|
36 | * Result is jde of the event and distance from the sun in AU.
|
37 | */
|
38 | function ellipticAscending(axis, ecc, argP, timeP) {
|
39 | // (axis, ecc, argP, timeP float64) (jde, r float64)
|
40 | return el(-argP, axis, ecc, timeP);
|
41 | }
|
42 |
|
43 | /**
|
44 | * EllipticAscending computes time and distance of passage through the descending node of a body in an elliptical orbit.
|
45 | *
|
46 | * Argument axis is semimajor axis in AU, ecc is eccentricity, argP is argument
|
47 | * of perihelion in radians, timeP is time of perihelion as a jd.
|
48 | *
|
49 | * Result is jde of the event and distance from the sun in AU.
|
50 | */
|
51 | function ellipticDescending(axis, ecc, argP, timeP) {
|
52 | // (axis, ecc, argP, timeP float64) (jde, r float64)
|
53 | return el(Math.PI - argP, axis, ecc, timeP);
|
54 | }
|
55 |
|
56 | function el(ν, axis, ecc, timeP) {
|
57 | // (ν, axis, ecc, timeP float64) (jde, r float64)
|
58 | var E = 2 * Math.atan(Math.sqrt((1 - ecc) / (1 + ecc)) * Math.tan(ν * 0.5));
|
59 |
|
60 | var _base$sincos = _base2.default.sincos(E),
|
61 | _base$sincos2 = _slicedToArray(_base$sincos, 2),
|
62 | sE = _base$sincos2[0],
|
63 | cE = _base$sincos2[1];
|
64 |
|
65 | var M = E - ecc * sE;
|
66 | var n = _base2.default.K / axis / Math.sqrt(axis);
|
67 | var jde = timeP + M / n;
|
68 | var r = axis * (1 - ecc * cE);
|
69 | return [jde, r];
|
70 | }
|
71 |
|
72 | /**
|
73 | * ParabolicAscending computes time and distance of passage through the ascending node of a body in a parabolic orbit.
|
74 | *
|
75 | * Argument q is perihelion distance in AU, argP is argument of perihelion
|
76 | * in radians, timeP is time of perihelion as a jd.
|
77 | *
|
78 | * Result is jde of the event and distance from the sun in AU.
|
79 | */
|
80 | function parabolicAscending(q, argP, timeP) {
|
81 | // (q, argP, timeP float64) (jde, r float64)
|
82 | return pa(-argP, q, timeP);
|
83 | }
|
84 |
|
85 | /**
|
86 | * ParabolicDescending computes time and distance of passage through the descending node of a body in a parabolic orbit.
|
87 | *
|
88 | * Argument q is perihelion distance in AU, argP is argument of perihelion
|
89 | * in radians, timeP is time of perihelion as a jd.
|
90 | *
|
91 | * Result is jde of the event and distance from the sun in AU.
|
92 | */
|
93 | function parabolicDescending(q, argP, timeP) {
|
94 | // (q, argP, timeP float64) (jde, r float64)
|
95 | return pa(Math.PI - argP, q, timeP);
|
96 | }
|
97 |
|
98 | function pa(ν, q, timeP) {
|
99 | // (ν, q, timeP float64) (jde, r float64)
|
100 | var s = Math.tan(ν * 0.5);
|
101 | var jde = timeP + 27.403895 * s * (s * s + 3) * q * Math.sqrt(q);
|
102 | var r = q * (1 + s * s);
|
103 | return [jde, r];
|
104 | }
|
105 |
|
106 | exports.default = {
|
107 | ellipticAscending: ellipticAscending,
|
108 | ellipticDescending: ellipticDescending,
|
109 | el: el,
|
110 | parabolicAscending: parabolicAscending,
|
111 | parabolicDescending: parabolicDescending,
|
112 | pa: pa
|
113 | }; |
\ | No newline at end of file |