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/dports/astro/gpstk/GPSTk-8.0.0/core/tests/GNSSEph/
H A DBrcKeplerOrbit_T.cpp72 fill(BrcKeplerOrbit& orbit) in fill() argument
142 BrcKeplerOrbit orbit; in equalityTest() local
143 fill(orbit); in equalityTest()
155 TUCATCH(orbitCopy = orbit); in equalityTest()
161 TUCATCH(orbitCopy = orbit); in equalityTest()
317 BrcKeplerOrbit orbit; in svXvtTest() local
339 zeroth_array[ii] = orbit.svXvt(orbit.getOrbitEpoch() + ii); in svXvtTest()
415 BrcKeplerOrbit orbit; in relativityTest() local
416 fill(orbit); in relativityTest()
427 BrcKeplerOrbit orbit; in fitIntTest() local
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/dports/astro/libnova/libnova-0.15.0/src/
H A Delliptic_motion.c215 orbit->n = ln_get_ell_mean_motion (orbit->a); in ln_get_ell_helio_rect_posn()
218 M = ln_get_ell_mean_anomaly (orbit->n, JD - orbit->JD); in ln_get_ell_helio_rect_posn()
227 r = ln_get_ell_radius_vector (orbit->a, orbit->e, E); in ln_get_ell_helio_rect_posn()
313 b = ln_get_ell_sminor_diam (orbit->e, orbit->a); in ln_get_ell_orbit_len()
317 H = (2.0 * orbit->a * b) / (orbit->a + b); in ln_get_ell_orbit_len()
351 V *= sqrt ((1.0 + orbit->e) / (1.0 - orbit->e)); in ln_get_ell_orbit_pvel()
366 V *= sqrt ((1.0 - orbit->e) / (1.0 + orbit->e)); in ln_get_ell_orbit_avel()
431 orbit->n = ln_get_ell_mean_motion (orbit->a); in ln_get_ell_body_phase_angle()
438 r = ln_get_ell_radius_vector (orbit->a, orbit->e, E); in ln_get_ell_body_phase_angle()
468 orbit->n = ln_get_ell_mean_motion (orbit->a); in ln_get_ell_body_elong()
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H A Dhyperbolic_motion.c146 t = JD - orbit->JD; in ln_get_hyp_helio_rect_posn()
155 sin_i = sin (ln_deg_to_rad (orbit->i)); in ln_get_hyp_helio_rect_posn()
156 cos_i = cos (ln_deg_to_rad (orbit->i)); in ln_get_hyp_helio_rect_posn()
173 v = ln_get_hyp_true_anomaly (orbit->q, orbit->e, t); in ln_get_hyp_helio_rect_posn()
176 r = ln_get_hyp_radius_vector (orbit->q, orbit->e, t); in ln_get_hyp_helio_rect_posn()
304 t = JD - orbit->JD; in ln_get_hyp_body_phase_angle()
307 r = ln_get_hyp_radius_vector (orbit->q, orbit->e, t); in ln_get_hyp_body_phase_angle()
311 d = ln_get_hyp_body_solar_dist (JD, orbit); in ln_get_hyp_body_phase_angle()
331 t = JD - orbit->JD; in ln_get_hyp_body_elong()
334 r = ln_get_hyp_radius_vector (orbit->q, orbit->e, t); in ln_get_hyp_body_elong()
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H A Dparabolic_motion.c106 t = JD - orbit->JD; in ln_get_par_helio_rect_posn()
115 sin_i = sin (ln_deg_to_rad (orbit->i)); in ln_get_par_helio_rect_posn()
116 cos_i = cos (ln_deg_to_rad (orbit->i)); in ln_get_par_helio_rect_posn()
133 v = ln_get_par_true_anomaly (orbit->q, t); in ln_get_par_helio_rect_posn()
136 r = ln_get_par_radius_vector (orbit->q, t); in ln_get_par_helio_rect_posn()
265 t = JD - orbit->JD; in ln_get_par_body_phase_angle()
268 r = ln_get_par_radius_vector (orbit->q, t); in ln_get_par_body_phase_angle()
272 d = ln_get_par_body_solar_dist (JD, orbit); in ln_get_par_body_phase_angle()
292 t = JD - orbit->JD; in ln_get_par_body_elong()
295 r = ln_get_par_radius_vector (orbit->q, t); in ln_get_par_body_elong()
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H A Dcomet.c34 double ln_get_ell_comet_mag (double JD, struct ln_ell_orbit * orbit, double g, double k) in ln_get_ell_comet_mag() argument
40 if (orbit->n == 0) in ln_get_ell_comet_mag()
41 orbit->n = ln_get_ell_mean_motion (orbit->a); in ln_get_ell_comet_mag()
42 M = ln_get_ell_mean_anomaly (orbit->n, JD - orbit->JD); in ln_get_ell_comet_mag()
45 E = ln_solve_kepler (orbit->e, M); in ln_get_ell_comet_mag()
48 r = ln_get_ell_radius_vector (orbit->a, orbit->e, E); in ln_get_ell_comet_mag()
49 d = ln_get_ell_body_solar_dist (JD, orbit); in ln_get_ell_comet_mag()
64 double ln_get_par_comet_mag (double JD, struct ln_par_orbit * orbit, double g, double k) in ln_get_par_comet_mag() argument
69 t = JD - orbit->JD; in ln_get_par_comet_mag()
72 r = ln_get_par_radius_vector (orbit->q, t); in ln_get_par_comet_mag()
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H A Dasteroid.c34 double ln_get_asteroid_mag (double JD, struct ln_ell_orbit * orbit, double H, double G) in ln_get_asteroid_mag() argument
41 b = ln_get_ell_body_phase_angle (JD, orbit); in ln_get_asteroid_mag()
45 if (orbit->n == 0) in ln_get_asteroid_mag()
46 orbit->n = ln_get_ell_mean_motion (orbit->a); in ln_get_asteroid_mag()
47 M = ln_get_ell_mean_anomaly (orbit->n, JD - orbit->JD); in ln_get_asteroid_mag()
50 E = ln_solve_kepler (orbit->e, M); in ln_get_asteroid_mag()
53 r = ln_get_ell_radius_vector (orbit->a, orbit->e, E); in ln_get_asteroid_mag()
54 d = ln_get_ell_body_solar_dist (JD, orbit); in ln_get_asteroid_mag()
89 double ln_get_asteroid_sdiam_arc (double JD, struct ln_ell_orbit * orbit, double H, double A) in ln_get_asteroid_sdiam_arc() argument
94 dist = ln_get_ell_body_earth_dist (JD, orbit); in ln_get_asteroid_sdiam_arc()
/dports/databases/powa-web/powa-web-4.0.2/powa/static/bower_components/foundation/scss/foundation/components/
H A D_orbit.scss50 @include exports("orbit") {
130 .orbit-container {
199 .orbit-timer {
209 .orbit-progress {
259 .orbit-prev,
260 .orbit-next {
311 .orbit-bullets {
341 .orbit-container {
342 .orbit-prev,
354 .orbit-prev,
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/dports/math/gap/gap-4.11.0/pkg/fining/tst/
H A Dtst_finingorbits.tst8 93%..100%..[ <closed orbit, 1 points>, <closed orbit, 255 points>,
11 93%..100%..[ <closed orbit, 1 points>, <closed orbit, 255 points>,
14 6%..56%..100%..[ <closed orbit, 17 points>, <closed orbit, 136 points>,
17 6%..56%..100%..[ <closed orbit, 17 points>, <closed orbit, 136 points>,
24 90%..100%..[ <closed orbit, 738 points>, <closed orbit, 82 points> ]
26 90%..100%..[ <closed orbit, 738 points>, <closed orbit, 82 points> ]
34 10%..100%..[ <closed orbit, 82 points>, <closed orbit, 738 points> ]
36 10%..100%..[ <closed orbit, 82 points>, <closed orbit, 738 points> ]
42 85%..100%..[ <closed orbit, 2107 points>, <closed orbit, 344 points> ]
44 85%..100%..[ <closed orbit, 2107 points>, <closed orbit, 344 points> ]
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/dports/science/cdk/cdk-cdk-2.3/descriptor/signature/src/test/java/org/openscience/cdk/signature/
H A DOrbitTest.java41 private Orbit orbit; field in OrbitTest
52 orbit = new Orbit(orbitLabel, height); in setUp()
55 orbit.addAtom(atomIndex); in setUp()
73 for (Integer i : orbit) { in iteratorTest()
93 for (int index : orbit) { in isEmptyTest()
97 orbit.remove(index); in isEmptyTest()
102 private boolean isSorted(Orbit orbit) { in isSorted() argument
104 for (int index : orbit) { in isSorted()
134 orbit.addAtom(4); in addAtomTest()
151 orbit.remove(0); in removeTest()
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/dports/graphics/quat-gui/quat-1.20/kernel/
H A Diter.c62 orbit = is->orbit; in iterate_0()
175 orbit = is->orbit; in iterate_1()
299 orbit = is->orbit; in iterate_2()
302 re2 = orbit[0][0]*orbit[0][0]; in iterate_2()
303 pure2 = orbit[0][1]*orbit[0][1]; in iterate_2()
304 pure2 += orbit[0][2]*orbit[0][2]; in iterate_2()
305 pure2 += orbit[0][3]*orbit[0][3]; in iterate_2()
349 orbit = is->orbit; in iterate_3()
389 orbit = is->orbit; in iterate_4()
685 is.orbit = orbit; in obj_distance()
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/dports/graphics/quat/quat-1.20/kernel/
H A Diter.c62 orbit = is->orbit; in iterate_0()
175 orbit = is->orbit; in iterate_1()
299 orbit = is->orbit; in iterate_2()
302 re2 = orbit[0][0]*orbit[0][0]; in iterate_2()
303 pure2 = orbit[0][1]*orbit[0][1]; in iterate_2()
304 pure2 += orbit[0][2]*orbit[0][2]; in iterate_2()
305 pure2 += orbit[0][3]*orbit[0][3]; in iterate_2()
349 orbit = is->orbit; in iterate_3()
389 orbit = is->orbit; in iterate_4()
685 is.orbit = orbit; in obj_distance()
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/dports/math/polymake/polymake-4.5/apps/group/cpperl/
H A Dwrap-orbit.cpperl1 {"app": "group", "embed": "orbit.cc",
6 …nst Set<Int>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/Set.h", "polymake/gro…
7 …et<Set<Int>>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/Set.h", "polymake/gro…
10 …>>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/Set.h", "polymake/client.h", "p…
11 …nned<const Array<Int>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/group/orbit.…
12 …nned<const Array<Int>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/group/orbit.…
13 …Vector<Int>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/Vector.h", "polymake/g…
14 …Vector<Int>&>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/Vector.h", "polymake/g…
15 …, "func": "orbit", "include": ["polymake/Array.h", "polymake/IncidenceMatrix.h", "polymake/Matrix.…
20 …>"], "func": "orbit", "include": ["polymake/Array.h", "polymake/Rational.h", "polymake/Vector.h", …
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/dports/astro/libnova/libnova-0.15.0/examples/
H A Dasteroid.c48 struct ln_ell_orbit orbit; in main() local
71 orbit.a = 2.7730346; in main()
72 orbit.e = 0.2299839; in main()
73 orbit.i = 34.84989; in main()
74 orbit.omega = 173.16479; in main()
75 orbit.w = 310.45917; in main()
76 orbit.n =0.21343771; in main()
82 orbit.JD = ln_get_ell_last_perihelion (M_JD, 260.69458, orbit.n); in main()
108 l = ln_get_ell_orbit_len (&orbit); in main()
112 V = ln_get_ell_orbit_pvel (&orbit); in main()
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H A Dcomet.c51 struct ln_ell_orbit orbit; in main() local
74 orbit.JD = e_JD; in main()
75 orbit.a = 2.2091404; in main()
76 orbit.e = 0.8502196; in main()
77 orbit.i = 11.94525; in main()
78 orbit.omega = 334.75006; in main()
79 orbit.w = 186.23352; in main()
80 orbit.n = 0; in main()
112 l = ln_get_ell_orbit_len (&orbit); in main()
116 V = ln_get_ell_orbit_pvel (&orbit); in main()
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/dports/audio/orbit-lv2/orbit-0.1.431/
H A Dmanifest.ttl.in20 @prefix orbit: <http://open-music-kontrollers.ch/lv2/orbit#> .
23 orbit:looper
28 rdfs:seeAlso <orbit.ttl> .
31 orbit:cargoship
36 rdfs:seeAlso <orbit.ttl> .
39 orbit:timecapsule
47 orbit:click
55 orbit:pacemaker
63 orbit:beatbox
71 orbit:subspace
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H A Dorbit.ttl37 @prefix orbit: <http://open-music-kontrollers.ch/lv2/orbit#> .
52 proj:orbit
58 orbit:looper_punch
74 orbit:looper_mute
110 orbit:looper
192 orbit:click
288 orbit:pacemaker
403 orbit:beatbox
480 orbit:subspace
549 orbit:cargoship
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/dports/misc/libpredict/libpredict-2.0.0/src/
H A Dobserver.c43 double julTime = orbit->time + JULIAN_TIME_DIFF; in predict_observe_orbit()
45 observer_calculate(observer, julTime, orbit->position, orbit->velocity, obs); in predict_observe_orbit()
54 obs->time = orbit->time; in predict_observe_orbit()
153 struct predict_position orbit; in predict_next_aos() local
155 predict_observe_orbit(observer, &orbit, &obs); in predict_next_aos()
211 struct predict_position orbit; in step_pass() local
234 struct predict_position orbit; in predict_next_los() local
274 struct predict_position orbit; in elevation_derivative() local
314 struct predict_position orbit; in find_max_elevation() local
329 struct predict_position orbit; in predict_at_max_elevation() local
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/dports/math/cmh/cmh-1.1.0/src/
H A Dio.h48 int get_iteration (const struct cm_data * K, const int orbit);
49 int get_level_producttrees (const struct cm_data * K, const int orbit,
52 int save_period (const struct cm_data * K, const int orbit, const int no,
55 const int orbit, const int no, const int iter);
59 const int orbit, const int iter);
60 int save_producttrees (const struct cm_data * K, const int orbit,
64 const struct cm_data * K, const int orbit,
66 int save_polynomial_real (const struct cm_data * K, const int orbit,
73 const struct cm_data * K, const int orbit,
75 int save_recognition_failed (const struct cm_data * K, const int orbit,
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/dports/astro/libnova/libnova-0.15.0/src/libnova/
H A Delliptic_motion.h81 void LIBNOVA_EXPORT ln_get_ell_geo_rect_posn (struct ln_ell_orbit* orbit, double JD, struct ln_rect…
87 void LIBNOVA_EXPORT ln_get_ell_helio_rect_posn (struct ln_ell_orbit* orbit, double JD, struct ln_re…
93 double LIBNOVA_EXPORT ln_get_ell_orbit_len (struct ln_ell_orbit * orbit);
99 double LIBNOVA_EXPORT ln_get_ell_orbit_vel (double JD, struct ln_ell_orbit * orbit);
105 double LIBNOVA_EXPORT ln_get_ell_orbit_pvel (struct ln_ell_orbit * orbit);
111 double LIBNOVA_EXPORT ln_get_ell_orbit_avel (struct ln_ell_orbit * orbit);
117 double LIBNOVA_EXPORT ln_get_ell_body_phase_angle (double JD, struct ln_ell_orbit * orbit);
123 double LIBNOVA_EXPORT ln_get_ell_body_elong (double JD, struct ln_ell_orbit * orbit);
130 double LIBNOVA_EXPORT ln_get_ell_body_solar_dist (double JD, struct ln_ell_orbit * orbit);
137 double LIBNOVA_EXPORT ln_get_ell_body_earth_dist (double JD, struct ln_ell_orbit * orbit);
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/dports/math/nauty/nauty27r3/
H A Dnautest1c.ans57 …Level 1: 3 cells; 1 singleton; target cell: 50; 1 orbit; 3 nodes (1 kept); 1 update; group_level:…
58 …Level 2: 7 cells; 3 singletons; target cell: 42; 1 orbit; 1 node (1 kept); 1 update; group_level:…
60 …Level 4: 50 cells; 50 singletons; target cell: 4; 1 orbit; 1 node (1 kept); 1 update; group_level…
61 1 orbit; grpsize=252000; 2 gens; 16 nodes (2 peak); maxlev=4
64 …Level 1: 3 cells; 1 singleton; target cell: 50; 1 orbit; 3 nodes (1 kept); 1 update; group_level:…
65 …Level 2: 7 cells; 3 singletons; target cell: 42; 1 orbit; 1 node (1 kept); 1 update; group_level:…
68 1 orbit; grpsize=252000; 2 gens; 16 nodes (2 peak); maxlev=4
71 …Level 1: 3 cells; 1 singleton; target cell: 50; 1 orbit; 3 nodes (1 kept); 1 update; group_level:…
72 …Level 2: 7 cells; 3 singletons; target cell: 42; 1 orbit; 1 node (1 kept); 1 update; group_level:…
75 1 orbit; grpsize=252000; 2 gens; 16 nodes (2 peak); maxlev=4
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/dports/math/py-pynauty/pynauty-1.0.2/src/nauty27r1/
H A Dnautest1c.ans57 …Level 1: 3 cells; 1 singleton; target cell: 50; 1 orbit; 3 nodes (1 kept); 1 update; group_level:…
58 …Level 2: 7 cells; 3 singletons; target cell: 42; 1 orbit; 1 node (1 kept); 1 update; group_level:…
60 …Level 4: 50 cells; 50 singletons; target cell: 4; 1 orbit; 1 node (1 kept); 1 update; group_level…
61 1 orbit; grpsize=252000; 2 gens; 16 nodes (2 peak); maxlev=4
64 …Level 1: 3 cells; 1 singleton; target cell: 50; 1 orbit; 3 nodes (1 kept); 1 update; group_level:…
65 …Level 2: 7 cells; 3 singletons; target cell: 42; 1 orbit; 1 node (1 kept); 1 update; group_level:…
68 1 orbit; grpsize=252000; 2 gens; 16 nodes (2 peak); maxlev=4
71 …Level 1: 3 cells; 1 singleton; target cell: 50; 1 orbit; 3 nodes (1 kept); 1 update; group_level:…
72 …Level 2: 7 cells; 3 singletons; target cell: 42; 1 orbit; 1 node (1 kept); 1 update; group_level:…
75 1 orbit; grpsize=252000; 2 gens; 16 nodes (2 peak); maxlev=4
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/dports/math/gap/gap-4.11.0/pkg/polycyclic-2.15.1/gap/cover/const/
H A Dorb.gi7 # initialise orbit
8 orbit := [pt];
12 # Start constructing orbit.
19 l := Length( orbit );
20 orbit[p*l] := true;
25 orbit[h+t] := act( orbit[h+s], pcgs[i] );
34 return orbit;
44 # set up orbit
45 orbit := [block];
84 # set up orbit reps
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/dports/audio/libbpm/libbpm-0.3/documentation/latex/
H A Dgroup__orbit.tex68 \index{orbit@{orbit}!get\_\-rbend@{get\_\-rbend}}
69 \index{get\_\-rbend@{get\_\-rbend}!orbit@{orbit}}
127 \index{v\_\-copy@{v\_\-copy}!orbit@{orbit}}
138 \index{v\_\-mag@{v\_\-mag}!orbit@{orbit}}
149 \index{v\_\-scale@{v\_\-scale}!orbit@{orbit}}
160 \index{v\_\-norm@{v\_\-norm}!orbit@{orbit}}
180 \index{v\_\-add@{v\_\-add}!orbit@{orbit}}
191 \index{v\_\-sub@{v\_\-sub}!orbit@{orbit}}
202 \index{v\_\-dot@{v\_\-dot}!orbit@{orbit}}
213 \index{v\_\-cross@{v\_\-cross}!orbit@{orbit}}
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/dports/math/4ti2/4ti2-Release_1_6_9/src/util/
H A Dorbit.h24 orbit* createOrbit(vector, listVector*, listVector*);
26 orbit* softCopyOrbit(orbit*);
28 void printOrbit(orbit*, int);
31 listCriticalPair* createListCriticalPair(orbit*, orbit*);
32 int isOrbitEqualToFullGroup(orbit*, listVector*, int);
33 orbit* computeOrbitPermutationsGraver(orbit*, listVector*, int);
34 orbit* computeOrbitPermutationsGroebner(orbit*, listVector*, int);
/dports/science/dalton/dalton-66052b3af5ea7225e31178bf9a8b031913c72190/DALTON/test/trueresult/
H A Dbenchmark_her_adz.ref1091 Number of two-electron spin-orbit integrals written: 16127847 (21.7%)
1094 Number of two-electron spin-orbit integrals written: 36040607 (21.5%)
1097 Number of two-electron spin-orbit integrals written: 39989710 (21.5%)
1100 Number of two-electron spin-orbit integrals written: 8123114 (21.8%)
1103 Number of two-electron spin-orbit integrals written: 18063940 (21.6%)
1106 Number of two-electron spin-orbit integrals written: 20024491 (21.5%)
1109 Number of two-electron spin-orbit integrals written: 13858830 (24.8%)
1112 Number of two-electron spin-orbit integrals written: 27687321 (24.8%)
1115 Number of two-electron spin-orbit integrals written: 6976019 (25.0%)
1118 Number of two-electron spin-orbit integrals written: 13874384 (24.9%)
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