Searched defs:orbital_elements (Results 1 – 13 of 13) sorted by relevance
| /dports/astro/astrometry/astrometry.net-0.85/util/ |
| H A D | jpl.h | 10 struct orbital_elements { struct
19 typedef struct orbital_elements orbital_elements_t; argument
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| H A D | jpl.c | 10 struct orbital_elements { struct
14 typedef struct orbital_elements orbital_elements_t; argument
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| /dports/misc/libpredict/libpredict-2.0.0/src/ |
| H A D | observer.c | 147 …edict_next_aos(const predict_observer_t *observer, const predict_orbital_elements_t *orbital_eleme… in predict_next_aos()
210 …uble step_pass(const predict_observer_t *observer, const predict_orbital_elements_t *orbital_eleme… in step_pass()
228 …edict_next_los(const predict_observer_t *observer, const predict_orbital_elements_t *orbital_eleme… in predict_next_los()
272 …ion_derivative(const predict_observer_t *observer, const predict_orbital_elements_t *orbital_eleme… in elevation_derivative()
290 …_max_elevation(const predict_observer_t *observer, const predict_orbital_elements_t *orbital_eleme… in find_max_elevation()
321 …_max_elevation(const predict_observer_t *observer, const predict_orbital_elements_t *orbital_eleme… in predict_at_max_elevation()
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| H A D | orbit.c | 156 int predict_orbit(const predict_orbital_elements_t *orbital_elements, struct predict_position *m, d… in predict_orbit()
232 bool predict_decayed(const predict_orbital_elements_t *orbital_elements, predict_julian_date_t time) in predict_decayed()
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| H A D | sgp4.c | 6 void sgp4_init(const predict_orbital_elements_t *orbital_elements, struct _sgp4 *m) in sgp4_init()
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| /dports/misc/libpredict/libpredict-2.0.0/tests/ |
| H A D | aoslos-t.cpp | 61 predict_orbital_elements_t *orbital_elements = predict_parse_tle(tle[0], tle[1]); in runtest() local
87 int aoslos_timepoint_consistency_test(predict_orbital_elements_t *orbital_elements, predict_observe… in aoslos_timepoint_consistency_test()
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| H A D | maxelevation-t.cpp | 72 predict_orbital_elements_t *orbital_elements = predict_parse_tle(tle[0], tle[1]); in runtest() local
154 …tion(double start_time, predict_observer_t *observer, predict_orbital_elements_t *orbital_elements) in test_max_elevation()
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| H A D | geostationary-t.cpp | 56 std::vector<satellite_t> orbital_elements = orbital_elements_from_file(argv[1]); in main() local
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| H A D | orbit-t.cpp | 52 predict_orbital_elements_t *orbital_elements = predict_parse_tle(tle[0], tle[1]); in runtest() local
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| /dports/misc/libpredict/libpredict-2.0.0/examples/passplot/ |
| H A D | generate_pass_data.c | 19 …predict_orbital_elements_t *orbital_elements = predict_parse_tle(oscar7_tle_line_1, oscar7_tle_lin… in main() local
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| /dports/misc/libpredict/libpredict-2.0.0/examples/orbit-2d/ |
| H A D | generate_orbit_data.cpp | 17 predict_orbital_elements_t *orbital_elements; member
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| /dports/astro/py-pymeeus/PyMeeus-0.3.6/pymeeus/ |
| H A D | Coordinates.py | 2835 def orbital_elements(epoch, parameters1, parameters2): function
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| /dports/astro/swe/swisseph-2.10.1/ |
| H A D | swetest.c | 2730 static int32 orbital_elements(double tjd_et, int32 ipl, int32 iflag, char *serr) in orbital_elements() function
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