| /dports/astro/libgal/libgal-0.5.0/sgp4/ |
| H A D | gal_sgp4gm.c | 78 double *j3oj2 in gal_sgp4gm() argument
98 *j3oj2 = *j3 / *j2 ; in gal_sgp4gm()
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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_sgp4init.c | 174 &sgp4->j3oj2 in gal_sgp4init()
284 cc3 = -2.0 * coef * tsi * sgp4->j3oj2 * sgp4->no * sinio / sgp4->ecco ; in gal_sgp4init()
320 sgp4->xlcof = -0.25 * sgp4->j3oj2 * sinio * ( 3.0 + 5.0 * cosio ) / ( 1.0 + cosio ) ; in gal_sgp4init()
323 sgp4->xlcof = -0.25 * sgp4->j3oj2 * sinio * ( 3.0 + 5.0 * cosio ) / temp4 ; in gal_sgp4init()
325 sgp4->aycof = -0.5 * sgp4->j3oj2 * sinio; in gal_sgp4init()
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| H A D | gal_sgp4gm.h | 88 double *j3oj2
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| H A D | gal_sgp4.c | 326 sgp4->aycof = -0.5 * sgp4->j3oj2 * sinip ; in gal_sgp4()
331 sgp4->xlcof = -0.25 * sgp4->j3oj2 * sinip * ( 3.0 + 5.0 * cosip ) / ( 1.0 + cosip ) ; in gal_sgp4()
334 sgp4->xlcof = -0.25 * sgp4->j3oj2 * sinip * ( 3.0 + 5.0 * cosip ) / temp4 ; in gal_sgp4()
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| H A D | gal_sgp4t.h | 98 double j3oj2 ; /* j3 divided by j2 */ 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/stellarium/stellarium-0.21.3/plugins/Satellites/src/gsatellite/ |
| H A D | sgp4unit.cpp | 687 tumin, mu, radiusearthkm, j2, j3, j4, j3oj2; in dsinit() local
1161 tumin, mu, radiusearthkm, j3, j4, j3oj2; in initl() local
1324 ss , j2 , j3oj2 , j4 , x2o3 , r[3] , v[3] , in sgp4init() local
1340 j2 = 0; j3oj2 = 0; j4 = 0; in sgp4init()
1482 satrec.aycof = -0.5 * j3oj2 * sinio; in sgp4init()
1666 twopi, x2o3 , j2 , j3 , tumin , j4 , xke , j3oj2, in sgp4() local
1675 j3oj2 = 0; in sgp4()
1818 satrec.aycof = -0.5*j3oj2*sinip; in sgp4()
2018 j3oj2 = j3 / j2; in getgravconst()
2029 j3oj2 = j3 / j2; 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 | 106 double& xke, double& j2, double& j3, double& j4, double& j3oj2);
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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/pykep/pykep-2.6/src/third_party/cspice/ |
| H A D | zzsgp4.c | 44 static doublereal j3oj2; in zzsgp4_0_() local
1112 j3oj2 = j3 / j2; in zzsgp4_0_()
1198 cc3 = coef * -2. * tsi * j3oj2 * no * sinio / ecco; in zzsgp4_0_()
1230 xlcof = j3oj2 * -.25 * sinio * (cosio * 5. + 3.) / (cosio + 1.); in zzsgp4_0_()
1232 xlcof = j3oj2 * -.25 * sinio * (cosio * 5. + 3.) / temp4; in zzsgp4_0_()
1234 aycof = j3oj2 * -.5 * sinio; in zzsgp4_0_()
1648 aycof = j3oj2 * -.5 * sinip; in zzsgp4_0_()
1653 xlcof = j3oj2 * -.25 * sinip * (cosip * 5. + 3.) / (cosip + 1.); in zzsgp4_0_()
1655 xlcof = j3oj2 * -.25 * sinip * (cosip * 5. + 3.) / temp4; in zzsgp4_0_()
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| /dports/astro/py-pykep/pykep-2.6/src/third_party/cspice/ |
| H A D | zzsgp4.c | 44 static doublereal j3oj2; in zzsgp4_0_() local
1112 j3oj2 = j3 / j2; in zzsgp4_0_()
1198 cc3 = coef * -2. * tsi * j3oj2 * no * sinio / ecco; in zzsgp4_0_()
1230 xlcof = j3oj2 * -.25 * sinio * (cosio * 5. + 3.) / (cosio + 1.); in zzsgp4_0_()
1232 xlcof = j3oj2 * -.25 * sinio * (cosio * 5. + 3.) / temp4; in zzsgp4_0_()
1234 aycof = j3oj2 * -.5 * sinio; in zzsgp4_0_()
1648 aycof = j3oj2 * -.5 * sinip; in zzsgp4_0_()
1653 xlcof = j3oj2 * -.25 * sinip * (cosip * 5. + 3.) / (cosip + 1.); in zzsgp4_0_()
1655 xlcof = j3oj2 * -.25 * sinip * (cosip * 5. + 3.) / temp4; in zzsgp4_0_()
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| /dports/astro/marble/marble-21.12.3/src/3rdparty/sgp4/ |
| H A D | sgp4unit.cpp | 716 tumin, mu, radiusearthkm, j2, j3, j4, j3oj2; in dsinit() local
1193 tumin, mu, radiusearthkm, j3, j4, j3oj2; in initl() local
1359 qzms2t, ss, j2, j3oj2, j4, x2o3, r[3], v[3], in sgp4init() local
1475 cc3 = -2.0 * coef * tsi * j3oj2 * satrec.no * sinio / satrec.ecco; in sgp4init()
1508 satrec.xlcof = -0.25 * j3oj2 * sinio * (3.0 + 5.0 * cosio) / temp4; in sgp4init()
1509 satrec.aycof = -0.5 * j3oj2 * sinio; in sgp4init()
1866 satrec.aycof = -0.5*j3oj2*sinip; in sgp4()
2067 double& j3oj2 in getgravconst() argument
2082 j3oj2 = j3 / j2; in getgravconst()
2093 j3oj2 = j3 / j2; 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 | 124 double& j3oj2
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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
147 double& j3oj2
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| H A D | SGP4.cpp | 1427 satrec.j2, satrec.j3, satrec.j4, satrec.j3oj2); in sgp4init()
1525 cc3 = -2.0 * coef * tsi * satrec.j3oj2 * satrec.no_unkozai * sinio / satrec.ecco; in sgp4init()
1556 satrec.xlcof = -0.25 * satrec.j3oj2 * sinio * (3.0 + 5.0 * cosio) / (1.0 + cosio); in sgp4init()
1558 satrec.xlcof = -0.25 * satrec.j3oj2 * sinio * (3.0 + 5.0 * cosio) / temp4; in sgp4init()
1559 satrec.aycof = -0.5 * satrec.j3oj2 * sinio; in sgp4init()
1928 satrec.aycof = -0.5*satrec.j3oj2*sinip; in sgp4()
1933 satrec.xlcof = -0.25 * satrec.j3oj2 * sinip * (3.0 + 5.0 * cosip) / temp4; in sgp4()
2085 double& j3oj2 in getgravconst() argument
2100 j3oj2 = j3 / j2; in getgravconst()
2111 j3oj2 = j3 / j2; in getgravconst()
[all …]
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| H A D | wrapper.cpp | 386 {"j3oj2", T_DOUBLE, O(j3oj2), READONLY,
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| /dports/astro/marble/marble-21.12.3/src/plugins/render/satellites/ |
| H A D | SatellitesTLEItem.cpp | 36 double tumin, mu, xke, j2, j3, j4, j3oj2; in SatellitesTLEItem() local
38 getgravconst( wgs84, tumin, mu, radiusearthkm, xke, j2, j3, j4, j3oj2 ); in SatellitesTLEItem()
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| /dports/astro/py-sgp4/python-sgp4-2.20/sgp4/ |
| H A D | propagation.py | 1339 satrec.j2, satrec.j3, satrec.j4, satrec.j3oj2) = whichconst;
1446 cc3 = -2.0 * coef * tsi * satrec.j3oj2 * satrec.no_unkozai * sinio / satrec.ecco;
1477 satrec.xlcof = -0.25 * satrec.j3oj2 * sinio * (3.0 + 5.0 * cosio) / (1.0 + cosio);
1479 satrec.xlcof = -0.25 * satrec.j3oj2 * sinio * (3.0 + 5.0 * cosio) / temp4;
1480 satrec.aycof = -0.5 * satrec.j3oj2 * sinio;
1842 satrec.aycof = -0.5*satrec.j3oj2*sinip;
1847 satrec.xlcof = -0.25 * satrec.j3oj2 * sinip * (3.0 + 5.0 * cosip) / temp4;
2037 j3oj2 = j3 / j2;
2048 j3oj2 = j3 / j2;
2059 j3oj2 = j3 / j2;
[all …]
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| /dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/ |
| H A D | TLE.pm | 6500 -2*$coef*$tsi*$parm->{j3oj2}*$parm->{meanmotion}*
6538 $parm->{xlcof}= -0.25*$parm->{j3oj2}*$init->{sinio}*
6541 $parm->{xlcof}= -0.25*$parm->{j3oj2}*$init->{sinio}*
6544 $parm->{aycof}= -0.5*$parm->{j3oj2}*$init->{sinio};
6837 $parm->{aycof}= -0.5*$parm->{j3oj2}*$sinip;
6840 $parm->{xlcof}= -0.25*$parm->{j3oj2}*$sinip*
6843 $parm->{xlcof}= -0.25*$parm->{j3oj2}*$sinip*
7054 $parm->{j3oj2}= $parm->{j3}/ $parm->{j2};
7065 $parm->{j3oj2}= $parm->{j3}/ $parm->{j2};
7076 $parm->{j3oj2}= $parm->{j3}/ $parm->{j2};
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