satkit 0.16.2

Satellite Toolkit
Documentation
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
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
353
354
355
356
357
358
359
360
361
362
363
364
365
366
367
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
445
446
447
448
449
450
451
452
453
454
455
456
use std::f64::consts::PI;

/*-----------------------------------------------------------------------------
*
*                           procedure dsinit
*
*  this procedure provides deep space contributions to mean motion dot due
*    to geopotential resonance with half day and one day orbits.
*
*  author        : david vallado                  719-573-2600   28 jun 2005
*
*  inputs        :
*    xke         - reciprocal of tumin
*    cosim, sinim-
*    emsq        - eccentricity squared
*    argpo       - argument of perigee
*    s1, s2, s3, s4, s5      -
*    ss1, ss2, ss3, ss4, ss5 -
*    sz1, sz3, sz11, sz13, sz21, sz23, sz31, sz33 -
*    t           - time
*    tc          -
*    gsto        - greenwich sidereal time                   rad
*    mo          - mean anomaly
*    mdot        - mean anomaly dot (rate)
*    no          - mean motion
*    nodeo       - right ascension of ascending node
*    nodedot     - right ascension of ascending node dot (rate)
*    xpidot      -
*    z1, z3, z11, z13, z21, z23, z31, z33 -
*    eccm        - eccentricity
*    argpm       - argument of perigee
*    inclm       - inclination
*    mm          - mean anomaly
*    xn          - mean motion
*    nodem       - right ascension of ascending node
*
*  outputs       :
*    em          - eccentricity
*    argpm       - argument of perigee
*    inclm       - inclination
*    mm          - mean anomaly
*    nm          - mean motion
*    nodem       - right ascension of ascending node
*    irez        - flag for resonance           0-none, 1-one day, 2-half day
*    atime       -
*    d2201, d2211, d3210, d3222, d4410, d4422, d5220, d5232, d5421, d5433    -
*    dedt        -
*    didt        -
*    dmdt        -
*    dndt        -
*    dnodt       -
*    domdt       -
*    del1, del2, del3        -
*    ses  , sghl , sghs , sgs  , shl  , shs  , sis  , sls
*    theta       -
*    xfact       -
*    xlamo       -
*    xli         -
*    xni
*
*  locals        :
*    ainv2       -
*    aonv        -
*    cosisq      -
*    eoc         -
*    f220, f221, f311, f321, f322, f330, f441, f442, f522, f523, f542, f543  -
*    g200, g201, g211, g300, g310, g322, g410, g422, g520, g521, g532, g533  -
*    sini2       -
*    temp        -
*    temp1       -
*    theta       -
*    xno2        -
*
*  coupling      :
*    getgravconst- no longer used
*
*  references    :
*    hoots, roehrich, norad spacetrack report #3 1980
*    hoots, norad spacetrack report #6 1986
*    hoots, schumacher and glover 2004
*    vallado, crawford, hujsak, kelso  2006
----------------------------------------------------------------------------*/

#[allow(clippy::too_many_arguments)]
pub fn dsinit(
    // sgp4fix just send in xke as a constant and eliminate getgravconst call
    // gravconsttype whichconst,
    xke: f64,
    cosim: f64,
    mut emsq: f64,
    argpo: f64,
    s1: f64,
    s2: f64,
    s3: f64,
    s4: f64,
    s5: f64,
    sinim: f64,
    ss1: f64,
    ss2: f64,
    ss3: f64,
    ss4: f64,
    ss5: f64,
    sz1: f64,
    sz3: f64,
    sz11: f64,
    sz13: f64,
    sz21: f64,
    sz23: f64,
    sz31: f64,
    sz33: f64,
    t: f64,
    tc: f64,
    gsto: f64,
    mo: f64,
    mdot: f64,
    no: f64,
    nodeo: f64,
    nodedot: f64,
    xpidot: f64,
    z1: f64,
    z3: f64,
    z11: f64,
    z13: f64,
    z21: f64,
    z23: f64,
    z31: f64,
    z33: f64,
    ecco: f64,
    eccsq: f64,
    em: &mut f64,
    argpm: &mut f64,
    inclm: &mut f64,
    mm: &mut f64,
    nm: &mut f64,
    nodem: &mut f64,
    irez: &mut i32,
    atime: &mut f64,
    d2201: &mut f64,
    d2211: &mut f64,
    d3210: &mut f64,
    d3222: &mut f64,
    d4410: &mut f64,
    d4422: &mut f64,
    d5220: &mut f64,
    d5232: &mut f64,
    d5421: &mut f64,
    d5433: &mut f64,
    dedt: &mut f64,
    didt: &mut f64,
    dmdt: &mut f64,
    dndt: &mut f64,
    dnodt: &mut f64,
    domdt: &mut f64,
    del1: &mut f64,
    del2: &mut f64,
    del3: &mut f64,
    xfact: &mut f64,
    xlamo: &mut f64,
    xli: &mut f64,
    xni: &mut f64,
) {
    /* --------------------- local variables ------------------------ */
    const TWOPI: f64 = 2.0 * PI;

    let mut f220: f64;
    let f221: f64;
    let f311: f64;
    let f321: f64;
    let f322: f64;
    let mut f330: f64;
    let f441: f64;
    let f442: f64;
    let f522: f64;
    let f523: f64;
    let f542: f64;
    let f543: f64;
    let g200: f64;
    let g201: f64;
    let g211: f64;
    let g300: f64;
    let mut g310: f64;
    let g322: f64;
    let g410: f64;
    let g422: f64;
    let g520: f64;
    let g521: f64;
    let g532: f64;
    let g533: f64;
    let cosisq: f64;
    let emo: f64;
    let emsqo: f64;

    /*
    double ainv2, aonv = 0.0, cosisq, eoc, f220, f221, f311,
        f321, f322, f330, f441, f442, f522, f523,
        f542, f543, g200, g201, g211, g300, g310,
        g322, g410, g422, g520, g521, g532, g533,
        ses, sgs, sghl, sghs, shs, shll, sis,
        sini2, sls, temp, temp1, theta, xno2, q22,
        q31, q33, root22, root44, root54, rptim, root32,
        root52, x2o3, znl, emo, zns, emsqo;
    */

    const Q22: f64 = 1.7891679e-6;
    const Q31: f64 = 2.1460748e-6;
    const Q33: f64 = 2.2123015e-7;
    const ROOT22: f64 = 1.7891679e-6;
    const ROOT44: f64 = 7.3636953e-9;
    const ROOT54: f64 = 2.1765803e-9;
    const RPTIM: f64 = 4.375_269_088_011_3e-3; // this equates to 7.29211514668855e-5 rad/sec
    const ROOT32: f64 = 3.7393792e-7;
    const ROOT52: f64 = 1.1428639e-7;
    const X2O3: f64 = 2.0 / 3.0;
    const ZNL: f64 = 1.5835218e-4;
    const ZNS: f64 = 1.19459e-5;

    // sgp4fix identify constants and allow alternate values
    // just xke is used here so pass it in rather than have multiple calls
    // getgravconst( whichconst, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2 );

    /* -------------------- deep space initialization ------------ */
    *irez = 0;
    if (*nm < 0.0052359877) && (*nm > 0.0034906585) {
        *irez = 1;
    }
    if (*nm >= 8.26e-3) && (*nm <= 9.24e-3) && (*em >= 0.5) {
        *irez = 2;
    }

    /* ------------------------ do solar terms ------------------- */
    let ses = ss1 * ZNS * ss5;
    let sis = ss2 * ZNS * (sz11 + sz13);
    let sls = -ZNS * ss3 * 6.0f64.mul_add(-emsq, sz1 + sz3 - 14.0);
    let sghs = ss4 * ZNS * (sz31 + sz33 - 6.0);
    let mut shs = -ZNS * ss2 * (sz21 + sz23);
    // sgp4fix for 180 deg incl
    if (*inclm < 5.2359877e-2) || (*inclm > PI - 5.2359877e-2) {
        shs = 0.0;
    }
    if sinim != 0.0 {
        shs /= sinim;
    }
    let sgs = cosim.mul_add(-shs, sghs);

    /* ------------------------- do lunar terms ------------------ */
    *dedt = (s1 * ZNL).mul_add(s5, ses);
    *didt = (s2 * ZNL).mul_add(z11 + z13, sis);
    *dmdt = (ZNL * s3).mul_add(-6.0f64.mul_add(-emsq, z1 + z3 - 14.0), sls);
    let sghl = s4 * ZNL * (z31 + z33 - 6.0);
    let mut shll = -ZNL * s2 * (z21 + z23);
    // sgp4fix for 180 deg incl
    if (*inclm < 5.2359877e-2) || (*inclm > PI - 5.2359877e-2) {
        shll = 0.0;
    }
    *domdt = sgs + sghl;
    *dnodt = shs;
    if sinim != 0.0 {
        *domdt -= cosim / sinim * shll;
        *dnodt += shll / sinim;
    }

    /* ----------- calculate deep space resonance effects -------- */
    *dndt = 0.0;
    let theta = tc.mul_add(RPTIM, gsto) % TWOPI;
    *em += *dedt * t;
    *inclm += *didt * t;
    *argpm += *domdt * t;
    *nodem += *dnodt * t;
    *mm += *dmdt * t;
    //   sgp4fix for negative inclinations
    //   the following if statement should be commented out
    //if (inclm < 0.0)
    //  {
    //    inclm  = -inclm;
    //    argpm  = argpm - pi;
    //    nodem = nodem + pi;
    //  }

    /* -------------- initialize the resonance terms ------------- */
    if *irez != 0 {
        let aonv = f64::powf(*nm / xke, X2O3);

        /* ---------- geopotential resonance for 12 hour orbits ------ */
        if *irez == 2 {
            cosisq = cosim * cosim;
            emo = *em;
            *em = ecco;
            emsqo = emsq;
            emsq = eccsq;
            let eoc = *em * emsq;
            g201 = (*em - 0.64).mul_add(-0.440, -0.306);

            if *em <= 0.65 {
                g211 = 16.2900f64.mul_add(emsq, 13.2470f64.mul_add(-(*em), 3.616));
                g310 = 156.5910f64.mul_add(
                    eoc,
                    228.4190f64.mul_add(-emsq, 117.3900f64.mul_add(*em, -19.302)),
                );
                g322 = 146.5816f64.mul_add(
                    eoc,
                    214.6334f64.mul_add(-emsq, 109.7927f64.mul_add(*em, -18.9068)),
                );
                g410 = 313.9530f64.mul_add(
                    eoc,
                    471.0940f64.mul_add(-emsq, 242.6940f64.mul_add(*em, -41.122)),
                );
                g422 = 1083.4350f64.mul_add(
                    eoc,
                    1629.014f64.mul_add(-emsq, 841.8800f64.mul_add(*em, -146.407)),
                );
                g520 = 3708.2760f64.mul_add(
                    eoc,
                    5740.032f64.mul_add(-emsq, 3017.977f64.mul_add(*em, -532.114)),
                );
            } else {
                g211 = 266.724f64.mul_add(
                    eoc,
                    508.738f64.mul_add(-emsq, 331.819f64.mul_add(*em, -72.099)),
                );
                g310 = 1246.113f64.mul_add(
                    eoc,
                    2415.925f64.mul_add(-emsq, 1582.851f64.mul_add(*em, -346.844)),
                );
                g322 = 1215.972f64.mul_add(
                    eoc,
                    2366.899f64.mul_add(-emsq, 1554.908f64.mul_add(*em, -342.585)),
                );
                g410 = 3651.957f64.mul_add(
                    eoc,
                    7193.992f64.mul_add(-emsq, 4758.686f64.mul_add(*em, -1052.797)),
                );
                g422 = 12422.520f64.mul_add(
                    eoc,
                    24462.770f64.mul_add(-emsq, 16178.110f64.mul_add(*em, -3581.690)),
                );
                if *em > 0.715 {
                    g520 = 31324.56f64.mul_add(
                        eoc,
                        54087.36f64.mul_add(-emsq, 29936.92f64.mul_add(*em, -5149.66)),
                    );
                } else {
                    g520 = 3763.64f64.mul_add(emsq, 4664.75f64.mul_add(-(*em), 1464.74));
                }
            }
            if *em < 0.7 {
                g533 = 5542.21f64.mul_add(
                    eoc,
                    9064.7700f64.mul_add(-emsq, 4988.6100f64.mul_add(*em, -919.22770)),
                );
                g521 = 5337.524f64.mul_add(
                    eoc,
                    8491.4146f64.mul_add(-emsq, 4568.6173f64.mul_add(*em, -822.71072)),
                );
                g532 = 5341.4f64.mul_add(
                    eoc,
                    8624.7700f64.mul_add(-emsq, 4690.2500f64.mul_add(*em, -853.66600)),
                );
            } else {
                g533 = 109377.94f64.mul_add(
                    eoc,
                    229838.20f64.mul_add(-emsq, 161616.52f64.mul_add(*em, -37995.780)),
                );
                g521 = 146349.42f64.mul_add(
                    eoc,
                    309468.16f64.mul_add(-emsq, 218913.95f64.mul_add(*em, -51752.104)),
                );
                g532 = 115605.82f64.mul_add(
                    eoc,
                    242699.48f64.mul_add(-emsq, 170470.89f64.mul_add(*em, -40023.880)),
                );
            }

            let sini2 = sinim * sinim;
            f220 = 0.75 * (2.0f64.mul_add(cosim, 1.0) + cosisq);
            f221 = 1.5 * sini2;
            f321 = 1.875 * sinim * 3.0f64.mul_add(-cosisq, 2.0f64.mul_add(-cosim, 1.0));
            f322 = -1.875 * sinim * 3.0f64.mul_add(-cosisq, 2.0f64.mul_add(cosim, 1.0));
            f441 = 35.0 * sini2 * f220;
            f442 = 39.3750 * sini2 * sini2;
            f522 = 9.84375
                * sinim
                * sini2.mul_add(
                    5.0f64.mul_add(-cosisq, 2.0f64.mul_add(-cosim, 1.0)),
                    0.33333333 * 6.0f64.mul_add(cosisq, 4.0f64.mul_add(cosim, -2.0)),
                );
            f523 = sinim
                * (4.92187512 * sini2).mul_add(
                    10.0f64.mul_add(cosisq, 4.0f64.mul_add(-cosim, -2.0)),
                    6.56250012 * 3.0f64.mul_add(-cosisq, 2.0f64.mul_add(cosim, 1.0)),
                );
            f542 = 29.53125
                * sinim
                * cosisq.mul_add(
                    10.0f64.mul_add(cosisq, 8.0f64.mul_add(cosim, -12.0)),
                    8.0f64.mul_add(-cosim, 2.0),
                );
            f543 = 29.53125
                * sinim
                * cosisq.mul_add(
                    10.0f64.mul_add(-cosisq, 8.0f64.mul_add(cosim, 12.0)),
                    8.0f64.mul_add(-cosim, -2.0),
                );
            let xno2 = *nm * *nm;
            let ainv2 = aonv * aonv;
            let mut temp1 = 3.0 * xno2 * ainv2;
            let mut temp = temp1 * ROOT22;
            *d2201 = temp * f220 * g201;
            *d2211 = temp * f221 * g211;
            temp1 *= aonv;
            temp = temp1 * ROOT32;
            *d3210 = temp * f321 * g310;
            *d3222 = temp * f322 * g322;
            temp1 *= aonv;
            temp = 2.0 * temp1 * ROOT44;
            *d4410 = temp * f441 * g410;
            *d4422 = temp * f442 * g422;
            temp1 *= aonv;
            temp = temp1 * ROOT52;
            *d5220 = temp * f522 * g520;
            *d5232 = temp * f523 * g532;
            temp = 2.0 * temp1 * ROOT54;
            *d5421 = temp * f542 * g521;
            *d5433 = temp * f543 * g533;
            *xlamo = (mo + nodeo + nodeo - theta - theta) % TWOPI;
            *xfact = 2.0f64.mul_add(nodedot + *dnodt - RPTIM, mdot + *dmdt) - no;
            *em = emo;
            emsq = emsqo;
        }

        /* ---------------- synchronous resonance terms -------------- */
        if *irez == 1 {
            g200 = emsq.mul_add(0.8125f64.mul_add(emsq, -2.5), 1.0);
            g310 = 2.0f64.mul_add(emsq, 1.0);
            g300 = emsq.mul_add(6.60937f64.mul_add(emsq, -6.0), 1.0);
            f220 = 0.75 * (1.0 + cosim) * (1.0 + cosim);
            f311 = (0.9375 * sinim * sinim)
                .mul_add(3.0f64.mul_add(cosim, 1.0), -(0.75 * (1.0 + cosim)));
            f330 = 1.0 + cosim;
            f330 = 1.875 * f330 * f330 * f330;
            *del1 = 3.0 * *nm * *nm * aonv * aonv;
            *del2 = 2.0 * *del1 * f220 * g200 * Q22;
            *del3 = 3.0 * *del1 * f330 * g300 * Q33 * aonv;
            *del1 = *del1 * f311 * g310 * Q31 * aonv;
            *xlamo = (mo + nodeo + argpo - theta) % TWOPI;
            *xfact = mdot + xpidot - RPTIM + *dmdt + *domdt + *dnodt - no;
        }

        /* ------------ for sgp4, initialize the integrator ---------- */
        *xli = *xlamo;
        *xni = no;
        *atime = 0.0;
        *nm = no + *dndt;
    }

    //#include "debug3.cpp"
} // dsinit