/dports/astro/stellarium/stellarium-0.21.3/plugins/Satellites/src/gsatellite/ |
H A D | sgp4unit.cpp | 1341 radiusearthkm = 0; in sgp4init() 1393 ss = 78.0 / radiusearthkm + 1.0; in sgp4init() 1421 perige = (rp - 1.0) * radiusearthkm; in sgp4init() 1667 radiusearthkm, mu, vkmpersec; in sgp4() local 1676 radiusearthkm = 0; in sgp4() 1910 r[0] = (mrt * ux)* radiusearthkm; in sgp4() 1911 r[1] = (mrt * uy)* radiusearthkm; in sgp4() 1912 r[2] = (mrt * uz)* radiusearthkm; in sgp4() 2012 radiusearthkm = 6378.135; // km in getgravconst() 2024 xke = 60.0 / std::sqrt(radiusearthkm*radiusearthkm*radiusearthkm/mu); in getgravconst() [all …]
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H A D | sgp4io.cpp | 86 double sec, mu, radiusearthkm, tumin, xke, j2, j3, j4, j3oj2; in twoline2rv() local 93 getgravconst( whichconst, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2 ); in twoline2rv()
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H A D | gSatTEME.hpp | 165 double tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2; member in gSatTEME
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H A D | sgp4unit.h | 105 void getgravconst(gravconsttype whichconst, double& tumin, double& mu, double& radiusearthkm,
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H A D | gSatTEME.cpp | 64 getgravconst(CONSTANTS_SET, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2); in gSatTEME()
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/dports/astro/marble/marble-21.12.3/src/3rdparty/sgp4/ |
H A D | sgp4unit.cpp | 1360 tumin, mu, radiusearthkm, xke, j3; in sgp4init() local 1418 ss = 78.0 / radiusearthkm + 1.0; in sgp4init() 1449 perige = (rp - 1.0) * radiusearthkm; in sgp4init() 1724 vkmpersec = radiusearthkm * xke/60.0; in sgp4() 1959 r[0] = (mrt * ux)* radiusearthkm; in sgp4() 1960 r[1] = (mrt * uy)* radiusearthkm; in sgp4() 1961 r[2] = (mrt * uz)* radiusearthkm; in sgp4() 2062 double& radiusearthkm, in getgravconst() argument 2076 radiusearthkm = 6378.135; // km in getgravconst() 2088 xke = 60.0 / sqrt(radiusearthkm*radiusearthkm*radiusearthkm/mu); in getgravconst() [all …]
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H A D | sgp4io.cpp | 82 double sec, mu, radiusearthkm, tumin, xke, j2, j3, j4, j3oj2; in twoline2rv() local 92 getgravconst( whichconst, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2 ); in twoline2rv()
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H A D | sgp4unit.h | 119 double& radiusearthkm,
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/dports/astro/libgal/libgal-0.5.0/sgp4/ |
H A D | gal_sgp4init.c | 169 &sgp4->radiusearthkm, in gal_sgp4init() 177 ss = 78.0 / sgp4->radiusearthkm + 1.0 ; in gal_sgp4init() 178 qzms2t = pow ( ( ( 120.0 - 78.0 ) / sgp4->radiusearthkm ), 4 ) ; in gal_sgp4init() 180 sgp4->vkmpersec = sgp4->radiusearthkm * sgp4->xke / 60.0 ; in gal_sgp4init() 251 if (rp < (220.0 / sgp4->radiusearthkm + 1.0)) { in gal_sgp4init() 256 perige = ( rp - 1.0 ) * sgp4->radiusearthkm ; in gal_sgp4init() 267 qzms24 = pow ( ( ( 120.0 - sfour ) / sgp4->radiusearthkm ), 4.0 ) ; in gal_sgp4init() 268 sfour = sfour / sgp4->radiusearthkm + 1.0 ; in gal_sgp4init()
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H A D | gal_initsgp4p.c | 105 tumin, mu, radiusearthkm, j3, j4, j3oj2 ; in gal_initsgp4p() local 119 gal_sgp4gm ( gm, &tumin, &mu, &radiusearthkm, &xke, &j2, &j3, &j4, &j3oj2 ) ; in gal_initsgp4p()
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H A D | gal_sgp4.c | 438 pv[0][0] = ( mrt * ux ) * sgp4->radiusearthkm * GAL_KM2M ; in gal_sgp4() 439 pv[0][1] = ( mrt * uy ) * sgp4->radiusearthkm * GAL_KM2M ; in gal_sgp4() 440 pv[0][2] = ( mrt * uz ) * sgp4->radiusearthkm * GAL_KM2M ; in gal_sgp4()
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H A D | gal_sgp4t.h | 93 double radiusearthkm ; /* Radius of the earth in km */ member
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H A D | gal_dsinit.c | 237 tumin , mu , radiusearthkm, j2 , j3 , j4 , j3oj2 ; in gal_dsinit() local 260 gal_sgp4gm ( gm, &tumin, &mu, &radiusearthkm, &xke, &j2, &j3, &j4, &j3oj2 ) ; in gal_dsinit()
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/dports/astro/marble/marble-21.12.3/src/plugins/render/satellites/ |
H A D | SatellitesTLEItem.cpp | 37 double radiusearthkm; in SatellitesTLEItem() local 38 getgravconst( wgs84, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2 ); in SatellitesTLEItem() 39 m_earthSemiMajorAxis = radiusearthkm; in SatellitesTLEItem()
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/dports/astro/py-sgp4/python-sgp4-2.20/sgp4/ |
H A D | propagation.py | 1376 ss = 78.0 / satrec.radiusearthkm + 1.0; 1378 qzms2ttemp = (120.0 - 78.0) / satrec.radiusearthkm; 1414 if rp < 220.0 / satrec.radiusearthkm + 1.0: 1418 perige = (rp - 1.0) * satrec.radiusearthkm; 1429 sfour = sfour / satrec.radiusearthkm + 1.0; 1935 _mr = mrt * satrec.radiusearthkm 2031 radiusearthkm = 6378.135; # km 2042 radiusearthkm = 6378.135; # km 2043 xke = 60.0 / sqrt(radiusearthkm*radiusearthkm*radiusearthkm/mu); 2053 radiusearthkm = 6378.137; # km [all …]
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/dports/astro/py-sgp4/python-sgp4-2.20/extension/ |
H A D | SGP4.h | 104 double tumin, mus, radiusearthkm, xke, j2, j3, j4, j3oj2; member 142 double& radiusearthkm,
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H A D | SGP4.cpp | 1462 ss = 78.0 / satrec.radiusearthkm + 1.0; in sgp4init() 1497 perige = (rp - 1.0) * satrec.radiusearthkm; in sgp4init() 2021 r[0] = (mrt * ux)* satrec.radiusearthkm; in sgp4() 2022 r[1] = (mrt * uy)* satrec.radiusearthkm; in sgp4() 2023 r[2] = (mrt * uz)* satrec.radiusearthkm; in sgp4() 2080 double& radiusearthkm, in getgravconst() argument 2094 radiusearthkm = 6378.135; // km in getgravconst() 2105 radiusearthkm = 6378.135; // km in getgravconst() 2106 xke = 60.0 / sqrt(radiusearthkm*radiusearthkm*radiusearthkm / mus); in getgravconst() 2116 radiusearthkm = 6378.137; // km in getgravconst() [all …]
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H A D | wrapper.cpp | 376 {"radiusearthkm", T_DOUBLE, O(radiusearthkm), READONLY,
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/dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/ |
H A D | TLE.pm | 6445 $ss= 78/$parm->{radiusearthkm}+ 1; 6446 $qzms2t= ((120-78)/$parm->{radiusearthkm}) ** 4; 6474 $perige= ($init->{rp}-1)*$parm->{radiusearthkm}; 6482 $sfour= $sfour/$parm->{radiusearthkm}+ 1; 6723 $vkmpersec= $parm->{radiusearthkm}* $parm->{xke}/60; 6929 $r[1] = $mr*$ux* $parm->{radiusearthkm}; 6930 $r[2] = $mr*$uy* $parm->{radiusearthkm}; 6931 $r[3] = $mr*$uz* $parm->{radiusearthkm}; 7047 $parm->{radiusearthkm}= 6378.135; 7059 $parm->{radiusearthkm}= 6378.135; [all …]
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