/dports/astro/stellarium/stellarium-0.21.3/plugins/Satellites/src/gsatellite/ |
H A D | sgp4io.cpp | 137 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 142 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 150 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 155 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 172 satrec.argpo = satrec.argpo * deg2rad; in twoline2rv() 204 satrec.ecco, satrec.argpo, satrec.inclo, satrec.mo, satrec.no, in twoline2rv()
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H A D | sgp4unit.cpp | 88 double cosim, double emsq, double argpo, double s1, double s2, 659 double cosim, double emsq, double argpo, double s1, double s2, in dsinit() argument 866 xlamo = std::fmod(mo + nodeo + argpo - theta, twopi); in dsinit() 1044 xomi = argpo + argpdot * atime; in dspace() 1381 satrec.argpo = xargpo; in sgp4init() 1454 (2.0 * etasq - eeta * (1.0 + etasq)) * std::cos(2.0 * satrec.argpo))); in sgp4init() 1471 satrec.omgcof = satrec.bstar * cc3 * std::cos(satrec.argpo); in sgp4init() 1495 dscom(epoch, satrec.ecco, satrec.argpo, tc, satrec.inclo, satrec.nodeo, in sgp4init() 1518 satrec.ecco, satrec.inclo, satrec.nodeo, satrec.argpo, satrec.mo, in sgp4init() 1695 argpdf = satrec.argpo + satrec.argpdot * satrec.t; in sgp4() [all …]
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H A D | sgp4unit.h | 89 bstar , /*rcse ,*/ inclo , nodeo , ecco , argpo , mo , member
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/dports/astro/marble/marble-21.12.3/src/3rdparty/sgp4/ |
H A D | sgp4io.cpp | 136 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 141 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 149 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 154 &satrec.nodeo,&satrec.ecco, &satrec.argpo, &satrec.mo, &satrec.no, in twoline2rv() 171 satrec.argpo = satrec.argpo * deg2rad; in twoline2rv() 257 satrec.ecco, satrec.argpo, satrec.inclo, satrec.mo, satrec.no, in twoline2rv()
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H A D | sgp4unit.cpp | 95 double cosim, double emsq, double argpo, double s1, double s2, 119 double dmdt, double dnodt, double domdt, double argpo, double argpdot, 687 double cosim, double emsq, double argpo, double s1, double s2, in dsinit() argument 894 xlamo = fmod(mo + nodeo + argpo - theta, twopi); in dsinit() 987 double dmdt, double dnodt, double domdt, double argpo, double argpdot, in dspace() argument 1072 xomi = argpo + argpdot * atime; in dspace() 1406 satrec.argpo = xargpo; in sgp4init() 1498 satrec.omgcof = satrec.bstar * cc3 * cos(satrec.argpo); in sgp4init() 1524 epoch, satrec.ecco, satrec.argpo, tc, satrec.inclo, satrec.nodeo, in sgp4init() 1732 argpdf = satrec.argpo + satrec.argpdot * satrec.t; in sgp4() [all …]
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H A D | sgp4unit.h | 89 bstar , rcse , inclo , nodeo , ecco , argpo , mo , member
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/dports/astro/py-sgp4/python-sgp4-2.20/sgp4/ |
H A D | exporter.py | 84 if not 0 <= satrec.argpo <= 2 * pi: 85 raise ValueError("Argument of Perigee must be between 0 and 2 pi, got %r", satrec.argpo) 86 append("{0:8.4f}".format(satrec.argpo / _deg2rad).rjust(8, " ") + " ") 131 "ARG_OF_PERICENTER": satrec.argpo / _deg2rad,
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H A D | io.py | 181 satrec.argpo = float(line[34:42]) 201 satrec.argpo = satrec.argpo * deg2rad; 237 satrec.ndot, satrec.nddot, satrec.ecco, satrec.argpo, satrec.inclo, satrec.mo,
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H A D | omm.py | 38 argpo = float(fields['ARG_OF_PERICENTER']) * _to_radians 50 argpo, inclo, mo, no_kozai, nodeo)
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H A D | model.py | 74 ndot, nddot, ecco, argpo, inclo, mo, no_kozai, nodeo): argument 94 ecco, argpo, inclo, mo, no_kozai, nodeo, self)
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H A D | propagation.py | 647 cosim, emsq, argpo, s1, s2, argument 842 xlamo = (mo + nodeo + argpo - theta) % twopi 943 dmdt, dnodt, domdt, argpo, argpdot, argument 1026 xomi = argpo + argpdot * atime; 1358 satrec.argpo = xargpo; 1469 satrec.omgcof = satrec.bstar * cc3 * cos(satrec.argpo); 1514 epoch, satrec.ecco, satrec.argpo, tc, satrec.inclo, satrec.nodeo, 1527 (satrec.ecco, satrec.inclo, satrec.nodeo, satrec.argpo, satrec.mo 1530 satrec.ecco, satrec.inclo, satrec.nodeo, satrec.argpo, satrec.mo, 1707 argpdf = satrec.argpo + satrec.argpdot * satrec.t; [all …]
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/dports/astro/libgal/libgal-0.5.0/sgp4/ |
H A D | gal_sgp4init.c | 193 sgp4->argpo = tle->argpo * GAL_D2R ; in gal_sgp4init() 292 … ( 2.0 * etasq - eeta * ( 1.0 + etasq ) ) * cos ( 2.0 * sgp4->argpo ) ) ) ; in gal_sgp4init() 307 sgp4->omgcof = sgp4->bstar * cc3 * cos ( sgp4->argpo ) ; in gal_sgp4init() 345 sgp4->argpo, in gal_sgp4init() 472 &sgp4->argpo, in gal_sgp4init() 485 sgp4->argpo, in gal_sgp4init()
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H A D | gal_tle.h | 144 double argpo ; /* Argument of Perigee (deg) */ member
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H A D | gal_dspace.c | 129 double argpo, in gal_dspace() argument 286 xomi = argpo + argpdot * (*atime) ; in gal_dspace()
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H A D | gal_dspace.h | 140 double argpo,
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H A D | gal_tledec_test.c | 72 gal_vdv ( tle.argpo, 65.4476, 0.0, "gal_tledec", "argpo 0" ) ; in gal_tledec_test()
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H A D | gal_dsinit.h | 167 double argpo,
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H A D | gal_sgp4t.h | 74 double argpo ; /* Argument of Perigee (rad) */ member
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H A D | gal_dsinit.c | 155 double argpo, in gal_dsinit() argument 461 *xlamo = fmod ( mo + nodeo + argpo - theta, GAL_2PI ) ; in gal_dsinit()
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/dports/astro/py-sgp4/python-sgp4-2.20/extension/ |
H A D | SGP4.cpp | 110 double cosim, double emsq, double argpo, double s1, double s2, 134 double dmdt, double dnodt, double domdt, double argpo, double argpdot, 706 double cosim, double emsq, double argpo, double s1, double s2, in dsinit() argument 913 xlamo = fmod(mo + nodeo + argpo - theta, twopi); in dsinit() 1092 xomi = argpo + argpdot * atime; in dspace() 1449 satrec.argpo = xargpo; in sgp4init() 1532 (2.0 * etasq - eeta * (1.0 + etasq)) * cos(2.0 * satrec.argpo))); in sgp4init() 1548 satrec.omgcof = satrec.bstar * cc3 * cos(satrec.argpo); in sgp4init() 1783 argpdf = satrec.argpo + satrec.argpdot * satrec.t; in sgp4() 1829 satrec.argpo, satrec.argpdot, satrec.t, tc, in sgp4() [all …]
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H A D | wrapper.cpp | 184 double ecco, argpo, inclo, mo, no_kozai, nodeo; in Satrec_sgp4init() local 188 &ecco, &argpo, &inclo, &mo, &no_kozai, &nodeo)) in Satrec_sgp4init() 205 bstar, ndot, nddot, ecco, argpo, inclo, mo, no_kozai, in Satrec_sgp4init() 325 {"argpo", T_DOUBLE, O(argpo), READONLY,
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/dports/astro/pykep/pykep-2.6/src/third_party/cspice/ |
H A D | zzsgp4.c | 64 static doublereal argpo, xlcof, xmcof; in zzsgp4_0_() local 1075 argpo = elems[6]; in zzsgp4_0_() 1204 (etasq * 2. - eeta * (etasq + 1.)) * cos(argpo * 2.))); in zzsgp4_0_() 1219 omgcof = bstar * cc3 * cos(argpo); in zzsgp4_0_() 1251 zzdscm_(&epoch, &ecco, &argpo, &tc, &inclo, &nodeo, &no, &snodm, & in zzsgp4_0_() 1268 ecco, &inclo, &nodeo, &argpo, &mo); in zzsgp4_0_() 1275 zzdsin_(geophs, &cosim, &emsq, &argpo, &s1, &s2, &s3, &s4, &s5, & in zzsgp4_0_() 1512 omgadf = argpo + argpdot * *t; in zzsgp4_0_() 1542 dmdt, &dnodt, &domdt, &argpo, &argpdot, t, &tc, &gsto, &xfact, in zzsgp4_0_()
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H A D | zzdspc.c | 14 dmdt, doublereal *dnodt, doublereal *domdt, doublereal *argpo, in zzdspc_() argument 366 xomi = *argpo + *argpdot * *atime; in zzdspc_()
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/dports/astro/py-pykep/pykep-2.6/src/third_party/cspice/ |
H A D | zzsgp4.c | 64 static doublereal argpo, xlcof, xmcof; in zzsgp4_0_() local 1075 argpo = elems[6]; in zzsgp4_0_() 1204 (etasq * 2. - eeta * (etasq + 1.)) * cos(argpo * 2.))); in zzsgp4_0_() 1219 omgcof = bstar * cc3 * cos(argpo); in zzsgp4_0_() 1251 zzdscm_(&epoch, &ecco, &argpo, &tc, &inclo, &nodeo, &no, &snodm, & in zzsgp4_0_() 1268 ecco, &inclo, &nodeo, &argpo, &mo); in zzsgp4_0_() 1275 zzdsin_(geophs, &cosim, &emsq, &argpo, &s1, &s2, &s3, &s4, &s5, & in zzsgp4_0_() 1512 omgadf = argpo + argpdot * *t; in zzsgp4_0_() 1542 dmdt, &dnodt, &domdt, &argpo, &argpdot, t, &tc, &gsto, &xfact, in zzsgp4_0_()
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H A D | zzdspc.c | 14 dmdt, doublereal *dnodt, doublereal *domdt, doublereal *argpo, in zzdspc_() argument 366 xomi = *argpo + *argpdot * *atime; in zzdspc_()
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