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Searched refs:radiusearthkm (Results 1 – 19 of 19) sorted by relevance

/dports/astro/stellarium/stellarium-0.21.3/plugins/Satellites/src/gsatellite/
H A Dsgp4unit.cpp1341 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()
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H A Dsgp4io.cpp86 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()
H A DgSatTEME.hpp165 double tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2; member in gSatTEME
H A Dsgp4unit.h105 void getgravconst(gravconsttype whichconst, double& tumin, double& mu, double& radiusearthkm,
H A DgSatTEME.cpp64 getgravconst(CONSTANTS_SET, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2); in gSatTEME()
/dports/astro/marble/marble-21.12.3/src/3rdparty/sgp4/
H A Dsgp4unit.cpp1360 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()
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H A Dsgp4io.cpp82 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()
H A Dsgp4unit.h119 double& radiusearthkm,
/dports/astro/libgal/libgal-0.5.0/sgp4/
H A Dgal_sgp4init.c169 &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()
H A Dgal_initsgp4p.c105 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()
H A Dgal_sgp4.c438 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()
H A Dgal_sgp4t.h93 double radiusearthkm ; /* Radius of the earth in km */ member
H A Dgal_dsinit.c237 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()
/dports/astro/marble/marble-21.12.3/src/plugins/render/satellites/
H A DSatellitesTLEItem.cpp37 double radiusearthkm; in SatellitesTLEItem() local
38 getgravconst( wgs84, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2 ); in SatellitesTLEItem()
39 m_earthSemiMajorAxis = radiusearthkm; in SatellitesTLEItem()
/dports/astro/py-sgp4/python-sgp4-2.20/sgp4/
H A Dpropagation.py1376 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
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/dports/astro/py-sgp4/python-sgp4-2.20/extension/
H A DSGP4.h104 double tumin, mus, radiusearthkm, xke, j2, j3, j4, j3oj2; member
142 double& radiusearthkm,
H A DSGP4.cpp1462 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()
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H A Dwrapper.cpp376 {"radiusearthkm", T_DOUBLE, O(radiusearthkm), READONLY,
/dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/
H A DTLE.pm6445 $ss= 78/$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;
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