/dports/astro/gpstk/GPSTk-8.0.0/core/tests/GNSSEph/ |
H A D | BrcKeplerOrbit_T.cpp | 72 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 [all …]
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/dports/astro/libnova/libnova-0.15.0/src/ |
H A D | elliptic_motion.c | 215 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() [all …]
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H A D | hyperbolic_motion.c | 146 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() [all …]
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H A D | parabolic_motion.c | 106 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() [all …]
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H A D | comet.c | 34 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() [all …]
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H A D | asteroid.c | 34 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()
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/dports/databases/powa-web/powa-web-4.0.2/powa/static/bower_components/foundation/scss/foundation/components/ |
H A D | _orbit.scss | 50 @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, [all …]
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/dports/math/gap/gap-4.11.0/pkg/fining/tst/ |
H A D | tst_finingorbits.tst | 8 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> ] [all …]
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/dports/science/cdk/cdk-cdk-2.3/descriptor/signature/src/test/java/org/openscience/cdk/signature/ |
H A D | OrbitTest.java | 41 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() [all …]
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/dports/graphics/quat-gui/quat-1.20/kernel/ |
H A D | iter.c | 62 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() [all …]
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/dports/graphics/quat/quat-1.20/kernel/ |
H A D | iter.c | 62 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() [all …]
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/dports/math/polymake/polymake-4.5/apps/group/cpperl/ |
H A D | wrap-orbit.cpperl | 1 {"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", … [all …]
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/dports/astro/libnova/libnova-0.15.0/examples/ |
H A D | asteroid.c | 48 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() [all …]
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H A D | comet.c | 51 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() [all …]
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/dports/audio/orbit-lv2/orbit-0.1.431/ |
H A D | manifest.ttl.in | 20 @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 [all …]
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H A D | orbit.ttl | 37 @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 [all …]
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/dports/misc/libpredict/libpredict-2.0.0/src/ |
H A D | observer.c | 43 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 [all …]
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/dports/math/cmh/cmh-1.1.0/src/ |
H A D | io.h | 48 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, [all …]
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/dports/astro/libnova/libnova-0.15.0/src/libnova/ |
H A D | elliptic_motion.h | 81 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); [all …]
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/dports/math/nauty/nauty27r3/ |
H A D | nautest1c.ans | 57 …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 [all …]
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/dports/math/py-pynauty/pynauty-1.0.2/src/nauty27r1/ |
H A D | nautest1c.ans | 57 …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 [all …]
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/dports/math/gap/gap-4.11.0/pkg/polycyclic-2.15.1/gap/cover/const/ |
H A D | orb.gi | 7 # 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 [all …]
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/dports/audio/libbpm/libbpm-0.3/documentation/latex/ |
H A D | group__orbit.tex | 68 \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}} [all …]
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/dports/math/4ti2/4ti2-Release_1_6_9/src/util/ |
H A D | orbit.h | 24 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);
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/dports/science/dalton/dalton-66052b3af5ea7225e31178bf9a8b031913c72190/DALTON/test/trueresult/ |
H A D | benchmark_her_adz.ref | 1091 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%) [all …]
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