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/dports/misc/libpredict/libpredict-2.0.0/tests/
H A Dmaxelevation-t.cpp74 if (predict_is_geosynchronous(orbital_elements)) { in runtest()
81 if (test_max_elevation(start_time, observer, orbital_elements) != 0) { in runtest()
89 predict_orbit(orbital_elements, &orbit, start_time); in runtest()
101 double revolution_fraction = 1.0/orbital_elements->mean_motion/12.0; in runtest()
104 predict_orbit(orbital_elements, &orbit, start_time); in runtest()
135 if (test_max_elevation(start_time, observer, orbital_elements) != 0) { in runtest()
162 predict_orbit(orbital_elements, &orbit, start_time); in test_max_elevation()
166 double revolution_fraction = 1.0/orbital_elements->mean_motion/5.0; in test_max_elevation()
174 predict_orbit(orbital_elements, &orbit, start_time); in test_max_elevation()
194 predict_orbit(orbital_elements, &orbit, max_elevation_obs.time-EPSILON); in test_max_elevation()
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H A Daoslos-t.cpp61 predict_orbital_elements_t *orbital_elements = predict_parse_tle(tle[0], tle[1]); in runtest() local
74 if (aoslos_timepoint_consistency_test(orbital_elements, obs, start_time) != 0) { in runtest()
89 if (predict_is_geosynchronous(orbital_elements)) { in aoslos_timepoint_consistency_test()
94 aos = predict_next_aos(observer, orbital_elements, start_time); in aoslos_timepoint_consistency_test()
96 los = predict_next_los(observer, orbital_elements, aos_time); in aoslos_timepoint_consistency_test()
109 predict_orbit(orbital_elements, &orbit, aos_time); in aoslos_timepoint_consistency_test()
113 predict_orbit(orbital_elements, &orbit, los_time); in aoslos_timepoint_consistency_test()
123 predict_orbit(orbital_elements, &orbit, midpass); in aoslos_timepoint_consistency_test()
134 aos = predict_next_aos(observer, orbital_elements, los_time); in aoslos_timepoint_consistency_test()
136 los = predict_next_los(observer, orbital_elements, aos_time); in aoslos_timepoint_consistency_test()
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H A Dgeostationary-t.cpp56 std::vector<satellite_t> orbital_elements = orbital_elements_from_file(argv[1]); in main() local
68 for (size_t i=0; i < orbital_elements.size(); i++) { in main()
69 predict_orbital_elements_t *elements = orbital_elements[i].elements; in main()
70 std::string name = orbital_elements[i].name; in main()
H A Dorbit-t.cpp52 predict_orbital_elements_t *orbital_elements = predict_parse_tle(tle[0], tle[1]); in runtest() local
67 …bool check_squint_angle = testcase.containsValidAlonAlat() && (orbital_elements->ephemeris == EPHE… in runtest()
112 predict_orbit(orbital_elements, &orbit_lower, predict_to_julian(time)); in runtest()
116 predict_orbit(orbital_elements, &orbit_upper, predict_to_julian(time + DIFF)); in runtest()
/dports/misc/libpredict/libpredict-2.0.0/src/
H A Dobserver.c154 predict_orbit(orbital_elements, &orbit, curr_time); in predict_next_aos()
158 …if (predict_aos_happens(orbital_elements, observer->latitude) && !predict_is_geosynchronous(orbita… in predict_next_aos()
172 predict_orbit(orbital_elements, &orbit, curr_time); in predict_next_aos()
180 predict_orbit(orbital_elements, &orbit, curr_time); in predict_next_aos()
188 predict_orbit(orbital_elements, &orbit, curr_time); in predict_next_aos()
214 predict_orbit(orbital_elements, &orbit, curr_time); in step_pass()
235 predict_orbit(orbital_elements, &orbit, curr_time); in predict_next_los()
239 …if (predict_aos_happens(orbital_elements, observer->latitude) && !predict_is_geosynchronous(orbita… in predict_next_los()
276 predict_orbit(orbital_elements, &orbit, time); in elevation_derivative()
325 if (predict_is_geosynchronous(orbital_elements)) { in predict_at_max_elevation()
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H A Dorbit.c11 bool predict_decayed(const predict_orbital_elements_t *orbital_elements, predict_julian_date_t time…
170 double epoch = 1000.0*orbital_elements->epoch_year + orbital_elements->epoch_day; in predict_orbit()
176 switch (orbital_elements->ephemeris) { in predict_orbit()
178 sdp4_predict((struct _sdp4*)orbital_elements->ephemeris_data, tsince, &output); in predict_orbit()
181 sgp4_predict((struct _sgp4*)orbital_elements->ephemeris_data, tsince, &output); in predict_orbit()
222 double xno = orbital_elements->mean_motion*temp*MINUTES_PER_DAY; in predict_orbit()
223 double xmo = orbital_elements->mean_anomaly * M_PI / 180.0; in predict_orbit()
224 …((xno*MINUTES_PER_DAY/(M_PI*2.0) + age*orbital_elements->bstar_drag_term)*age + xmo/(2.0*M_PI)) + … in predict_orbit()
227 m->decayed = predict_decayed(orbital_elements, utc); in predict_orbit()
235 satepoch=DayNum(1,0,orbital_elements->epoch_year)+orbital_elements->epoch_day; in predict_decayed()
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H A Dsgp4.c6 void sgp4_init(const predict_orbital_elements_t *orbital_elements, struct _sgp4 *m) in sgp4_init() argument
12 m->bstar = orbital_elements->bstar_drag_term / AE; in sgp4_init()
13 m->xincl = orbital_elements->inclination * M_PI / 180.0; in sgp4_init()
14 m->xnodeo = orbital_elements->right_ascension * M_PI / 180.0; in sgp4_init()
15 m->eo = orbital_elements->eccentricity; in sgp4_init()
16 m->omegao = orbital_elements->argument_of_perigee * M_PI / 180.0; in sgp4_init()
17 m->xmo = orbital_elements->mean_anomaly * M_PI / 180.0; in sgp4_init()
18 m->xno = orbital_elements->mean_motion*temp_tle*MINUTES_PER_DAY; in sgp4_init()
H A Dsgp4.h37 void sgp4_init(const predict_orbital_elements_t *orbital_elements, struct _sgp4 *m);
H A Dsdp4.h91 void sdp4_init(const predict_orbital_elements_t *orbital_elements, struct _sdp4 *m);
/dports/misc/libpredict/libpredict-2.0.0/examples/passplot/
H A Dgenerate_pass_data.c19 …predict_orbital_elements_t *orbital_elements = predict_parse_tle(oscar7_tle_line_1, oscar7_tle_lin… in main() local
40 aos = predict_next_aos(observer, orbital_elements, start_time); in main()
41 los = predict_next_los(observer, orbital_elements, start_time); in main()
54 predict_orbit(orbital_elements, &orbit, curr_time); in main()
68 predict_destroy_orbital_elements(orbital_elements); in main()
/dports/misc/libpredict/libpredict-2.0.0/examples/orbit-2d/
H A Dgenerate_orbit_data.cpp17 predict_orbital_elements_t *orbital_elements; member
59 …predict_julian_date_t end_time = start_time + 1.0/satellite.orbital_elements->mean_motion; //mean_… in main()
66 predict_orbit(satellite.orbital_elements, &orbit, curr_time); in main()
72 predict_destroy_orbital_elements(satellite.orbital_elements); in main()
101 satellite.orbital_elements = temp_elements; in orbital_elements_from_file()
/dports/math/gnuplot/gnuplot-5.4.1/demo/
H A Dstats.dem16 stats 'orbital_elements.dat' index 1 using 2 prefix "A"
23 plot 'orbital_elements.dat' index 1 using 0:2 title " Data" lw 2, \
32 stats 'orbital_elements.dat' index 1 using (f($0)):2 prefix "B"
39 plot 'orbital_elements.dat' index 1 using (f($0)):2 title " Data" lw 2, \
/dports/math/gnuplot-lite/gnuplot-5.4.1/demo/
H A Dstats.dem16 stats 'orbital_elements.dat' index 1 using 2 prefix "A"
23 plot 'orbital_elements.dat' index 1 using 0:2 title " Data" lw 2, \
32 stats 'orbital_elements.dat' index 1 using (f($0)):2 prefix "B"
39 plot 'orbital_elements.dat' index 1 using (f($0)):2 title " Data" lw 2, \
/dports/math/gnuplot-tex-extras/gnuplot-5.2.8/demo/
H A Dstats.dem16 stats 'orbital_elements.dat' index 1 using 2 prefix "A"
23 plot 'orbital_elements.dat' index 1 using 0:2 title " Data" lw 2, \
32 stats 'orbital_elements.dat' index 1 using (f($0)):2 prefix "B"
39 plot 'orbital_elements.dat' index 1 using (f($0)):2 title " Data" lw 2, \
/dports/astro/astrometry/astrometry.net-0.85/util/
H A Djpl.h10 struct orbital_elements { struct
19 typedef struct orbital_elements orbital_elements_t; argument
H A Djpl.c10 struct orbital_elements { struct
14 typedef struct orbital_elements orbital_elements_t; argument
/dports/misc/libpredict/libpredict-2.0.0/include/predict/
H A Dpredict.h.in136 * \param orbital_elements Orbit to free
138 void predict_destroy_orbital_elements(predict_orbital_elements_t *orbital_elements);
182 * \param orbital_elements Orbital elements
188 int predict_orbit(const predict_orbital_elements_t *orbital_elements, struct predict_position *x, p…
206 * \param orbital_elements Orbital elements
209 bool predict_is_geosynchronous(const predict_orbital_elements_t *orbital_elements);
385 * \param orbital_elements Orbital elements
390 …nst predict_observer_t *observer, const predict_orbital_elements_t *orbital_elements, predict_juli…
396 * \param orbital_elements Orbital elements
401 …nst predict_observer_t *observer, const predict_orbital_elements_t *orbital_elements, predict_juli…
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/dports/misc/libpredict/libpredict-2.0.0/
H A DREADME.md47 predict_orbital_elements_t *orbital_elements = orbital_elements = predict_parse_tle(tle_line_1, tle…
56 predict_orbit(orbital_elements, &orbit, prediction_time);
/dports/astro/py-pymeeus/PyMeeus-0.3.6/pymeeus/
H A DNeptune.py26 geometric_vsop_pos, apparent_vsop_pos, orbital_elements,
2149 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM)
2185 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM_J2000)
H A DUranus.py27 geometric_vsop_pos, apparent_vsop_pos, orbital_elements,
4211 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM)
4247 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM_J2000)
H A DJupiter.py27 geometric_vsop_pos, apparent_vsop_pos, orbital_elements,
3712 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM)
3748 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM_J2000)
H A DMars.py27 geometric_vsop_pos, apparent_vsop_pos, orbital_elements,
5711 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM)
5747 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM_J2000)
H A DEarth.py27 geometric_vsop_pos, apparent_vsop_pos, orbital_elements,
3293 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM)
3329 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM_J2000)
H A DMercury.py27 geometric_vsop_pos, apparent_vsop_pos, orbital_elements,
7056 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM)
7092 return orbital_elements(epoch, ORBITAL_ELEM, ORBITAL_ELEM_J2000)
/dports/astro/marble/marble-21.12.3/src/plugins/render/satellites/
H A Dsatellites.qrc9 <file alias="marble/satellites/elements.png">data/orbital_elements.png</file>

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