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Searched refs:x3thm1 (Results 1 – 20 of 20) sorted by relevance

/dports/astro/py-pykep/pykep-2.6/src/third_party/cspice/
H A Ddpspce.c49 qoms24, sinuk, templ, x1m5th, x1mth2, x3thm1, x7thm1, psisq, in dpspce_() local
527 x3thm1 = theta2 * 3. - 1.; in dpspce_()
534 del1 = ck2 * 1.5 * x3thm1 / (d__1 * d__1 * betao * betao2); in dpspce_()
539 delo = ck2 * 1.5 * x3thm1 / (d__1 * d__1 * betao * betao2); in dpspce_()
577 + ck2 * .75 * tsi / psisq * x3thm1 * (etasq * 3. * (etasq + in dpspce_()
587 x3thm1 * -3. * (1. - eeta * 2. + etasq * (1.5 - eeta * .5)) + in dpspce_()
593 xmdot = xnodp + temp1 * .5 * betao * x3thm1 + temp2 * .0625 * betao * in dpspce_()
731 rk = rk * (1. - temp2 * 1.5 * betal * x3thm1) + temp1 * .5 * x1mth2 * in dpspce_()
737 rfdotk = rfdot + xn * temp1 * (x1mth2 * cos2u + x3thm1 * 1.5); in dpspce_()
H A Dev2lin.c53 x3thm1, x7thm1, fmod2p, theta2, theta4, xinck, xlcof, xmcof, in ev2lin_() local
603 x3thm1 = prelim[(i__1 = n * 29 - 8) < 174 && 0 <= i__1 ? i__1 : in ev2lin_()
628 x3thm1 = theta2 * 3. - 1.; in ev2lin_()
644 del1 = ck2 * 1.5 * x3thm1 / (a1 * a1 * betao3); in ev2lin_()
647 delo = ck2 * 1.5 * x3thm1 / (ao * ao * betao3); in ev2lin_()
682 + ck2 * .75 * (tsi / psisq) * x3thm1 * (etasq * (etasq * 3. + in ev2lin_()
688 x3thm1 * -3. * (1. - eeta * 2. + etasq * (1.5 - eeta * .5)) + in ev2lin_()
696 xmdot = xnodp + temp1 * .5 * betao * x3thm1 + temp2 * .0625 * betao * in ev2lin_()
779 , i__1, "ev2lin_", (ftnlen)1013)] = x3thm1; in ev2lin_()
1258 rk = r__ * (1. - temp2 * 1.5 * betal * x3thm1) + temp1 * .5 * x1mth2 * in ev2lin_()
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/dports/astro/pykep/pykep-2.6/src/third_party/cspice/
H A Ddpspce.c49 qoms24, sinuk, templ, x1m5th, x1mth2, x3thm1, x7thm1, psisq, in dpspce_() local
527 x3thm1 = theta2 * 3. - 1.; in dpspce_()
534 del1 = ck2 * 1.5 * x3thm1 / (d__1 * d__1 * betao * betao2); in dpspce_()
539 delo = ck2 * 1.5 * x3thm1 / (d__1 * d__1 * betao * betao2); in dpspce_()
577 + ck2 * .75 * tsi / psisq * x3thm1 * (etasq * 3. * (etasq + in dpspce_()
587 x3thm1 * -3. * (1. - eeta * 2. + etasq * (1.5 - eeta * .5)) + in dpspce_()
593 xmdot = xnodp + temp1 * .5 * betao * x3thm1 + temp2 * .0625 * betao * in dpspce_()
731 rk = rk * (1. - temp2 * 1.5 * betal * x3thm1) + temp1 * .5 * x1mth2 * in dpspce_()
737 rfdotk = rfdot + xn * temp1 * (x1mth2 * cos2u + x3thm1 * 1.5); in dpspce_()
H A Dev2lin.c53 x3thm1, x7thm1, fmod2p, theta2, theta4, xinck, xlcof, xmcof, in ev2lin_() local
603 x3thm1 = prelim[(i__1 = n * 29 - 8) < 174 && 0 <= i__1 ? i__1 : in ev2lin_()
628 x3thm1 = theta2 * 3. - 1.; in ev2lin_()
644 del1 = ck2 * 1.5 * x3thm1 / (a1 * a1 * betao3); in ev2lin_()
647 delo = ck2 * 1.5 * x3thm1 / (ao * ao * betao3); in ev2lin_()
682 + ck2 * .75 * (tsi / psisq) * x3thm1 * (etasq * (etasq * 3. + in ev2lin_()
688 x3thm1 * -3. * (1. - eeta * 2. + etasq * (1.5 - eeta * .5)) + in ev2lin_()
696 xmdot = xnodp + temp1 * .5 * betao * x3thm1 + temp2 * .0625 * betao * in ev2lin_()
779 , i__1, "ev2lin_", (ftnlen)1013)] = x3thm1; in ev2lin_()
1258 rk = r__ * (1. - temp2 * 1.5 * betal * x3thm1) + temp1 * .5 * x1mth2 * in ev2lin_()
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/dports/misc/libpredict/libpredict-2.0.0/src/
H A Dsgp4.c32 m->x3thm1=3*theta2-1.0; in sgp4_init()
36 del1=1.5*CK2*m->x3thm1/(a1*a1*betao*betao2); in sgp4_init()
38 delo=1.5*CK2*m->x3thm1/(ao*ao*betao*betao2); in sgp4_init()
79 …c2=coef1*m->xnodp*(m->aodp*(1+1.5*etasq+eeta*(4+etasq))+0.75*CK2*tsi/psisq*m->x3thm1*(8+3*etasq*(8… in sgp4_init()
86 …->eta*(2+0.5*etasq)+m->eo*(0.5+2*etasq)-2*CK2*tsi/(m->aodp*psisq)*(-3*m->x3thm1*(1-2*eeta+etasq*(1… in sgp4_init()
93 m->xmdot=m->xnodp+0.5*temp1*betao*m->x3thm1+0.0625*temp2*betao*(13-78*theta2+137*theta4); in sgp4_init()
217 rk=r*(1-1.5*temp2*betal*m->x3thm1)+0.5*temp1*m->x1mth2*cos2u; in sgp4_predict()
222 rfdotk=rfdot+xn*temp1*(m->x1mth2*cos2u+1.5*m->x3thm1); in sgp4_predict()
H A Dsgp4.h18 t5cof, x1mth2, x3thm1, x7thm1, xmcof, xmdot, xnodcf, xnodot, xlcof; member
H A Dorbit.c118 double x3thm1=3*theta2-1.0; in predict_perigee() local
122 double del1=1.5*CK2*x3thm1/(a1*a1*betao*betao2); in predict_perigee()
124 double delo=1.5*CK2*x3thm1/(ao*ao*betao*betao2); in predict_perigee()
H A Dsdp4.c55 m->x3thm1=3*m->deep_arg.theta2-1; in sdp4_init()
59 del1=1.5*CK2*m->x3thm1/(a1*a1*m->deep_arg.betao*m->deep_arg.betao2); in sdp4_init()
61 delo=1.5*CK2*m->x3thm1/(ao*ao*m->deep_arg.betao*m->deep_arg.betao2); in sdp4_init()
93 …odp*(m->deep_arg.aodp*(1+1.5*etasq+eeta*(4+etasq))+0.75*CK2*tsi/psisq*m->x3thm1*(8+3*etasq*(8+etas… in sdp4_init()
98 …0.5*etasq)+m->eo*(0.5+2*etasq)-2*CK2*tsi/(m->deep_arg.aodp*psisq)*(-3*m->x3thm1*(1-2*eeta+etasq*(1… in sdp4_init()
103 …m->deep_arg.xmdot=m->deep_arg.xnodp+0.5*temp1*m->deep_arg.betao*m->x3thm1+0.0625*temp2*m->deep_arg… in sdp4_init()
222 rk=r*(1-1.5*temp2*betal*m->x3thm1)+0.5*temp1*m->x1mth2*cos2u; in sdp4_predict()
227 rfdotk=rfdot+deep_dyn.xn*temp1*(m->x1mth2*cos2u+1.5*m->x3thm1); in sdp4_predict()
H A Dsdp4.h61 double x3thm1, c1, x1mth2, c4, xnodcf, t2cof, xlcof, member
/dports/astro/pykep/pykep-2.6/src/third_party/libsgp4/
H A DOrbitalElements.cpp41 const double x3thm1 = 3.0 * theta2 - 1.0; in OrbitalElements() local
45 const double temp = (1.5 * kCK2) * x3thm1 / (betao * betao2); in OrbitalElements()
H A DSGP4.cpp63 common_consts_.x3thm1 = 3.0 * theta2 - 1.0; in Initialise()
113 … + 0.75 * kCK2 * tsi / psisq * common_consts_.x3thm1 * (8.0 + 3.0 * etasq * (8.0 + etasq))); in Initialise()
120 … * (-3.0 * common_consts_.x3thm1 * (1.0 - 2.0 * eeta + etasq * (1.5 - 0.5 * eeta)) in Initialise()
127 …ommon_consts_.xmdot = elements_.RecoveredMeanMotion() + 0.5 * temp1 * betao * common_consts_.x3thm1 in Initialise()
368 … common_consts_.aycof, common_consts_.x3thm1, common_consts_.x1mth2, in FindPositionSGP4()
391 … const double aycof, const double x3thm1, const double x1mth2, in CalculateFinalPositionVelocity() argument
501 const double rk = r * (1.0 - 1.5 * temp43 * betal * x3thm1) + 0.5 * temp42 * x1mth2 * cos2u; in CalculateFinalPositionVelocity()
506 const double rfdotk = rfdot + xn * temp42 * (x1mth2 * cos2u + 1.5 * x3thm1); in CalculateFinalPositionVelocity()
/dports/astro/py-pykep/pykep-2.6/src/third_party/libsgp4/
H A DOrbitalElements.cpp41 const double x3thm1 = 3.0 * theta2 - 1.0; in OrbitalElements() local
45 const double temp = (1.5 * kCK2) * x3thm1 / (betao * betao2); in OrbitalElements()
H A DSGP4.cpp63 common_consts_.x3thm1 = 3.0 * theta2 - 1.0; in Initialise()
113 … + 0.75 * kCK2 * tsi / psisq * common_consts_.x3thm1 * (8.0 + 3.0 * etasq * (8.0 + etasq))); in Initialise()
120 … * (-3.0 * common_consts_.x3thm1 * (1.0 - 2.0 * eeta + etasq * (1.5 - 0.5 * eeta)) in Initialise()
127 …ommon_consts_.xmdot = elements_.RecoveredMeanMotion() + 0.5 * temp1 * betao * common_consts_.x3thm1 in Initialise()
368 … common_consts_.aycof, common_consts_.x3thm1, common_consts_.x1mth2, in FindPositionSGP4()
391 … const double aycof, const double x3thm1, const double x1mth2, in CalculateFinalPositionVelocity() argument
501 const double rk = r * (1.0 - 1.5 * temp43 * betal * x3thm1) + 0.5 * temp42 * x1mth2 * cos2u; in CalculateFinalPositionVelocity()
506 const double rfdotk = rfdot + xn * temp42 * (x1mth2 * cos2u + 1.5 * x3thm1); in CalculateFinalPositionVelocity()
/dports/astro/xplanet/xplanet-1.3.1/src/libsgp4sdp4/
H A Dsgp4sdp4.c27 x1mth2,x3thm1,x7thm1,xmcof,xmdot,xnodcf,xnodot,xlcof; in SGP4() local
53 x3thm1 = 3*theta2-1.0; in SGP4()
57 del1 = 1.5*ck2*x3thm1/(a1*a1*betao*betao2); in SGP4()
59 delo = 1.5*ck2*x3thm1/(ao*ao*betao*betao2); in SGP4()
96 0.75*ck2*tsi/psisq*x3thm1*(8+3*etasq*(8+etasq))); in SGP4()
104 (-3*x3thm1*(1-2*eeta+etasq*(1.5-0.5*eeta))+0.75* in SGP4()
111 xmdot = xnodp+0.5*temp1*betao*x3thm1+ in SGP4()
227 rfdotk = rfdot+xn*temp1*(x1mth2*cos2u+1.5*x3thm1); in SGP4()
270 x3thm1,c1,x1mth2,c4,xnodcf,t2cof,xlcof,aycof,x7thm1; in SDP4() local
295 x3thm1 = 3*deep_arg.theta2-1; in SDP4()
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/dports/astro/pykep/pykep-2.6/include/keplerian_toolbox/third_party/libsgp4/
H A DSGP4.h60 double x3thm1; member
192 const double aycof, const double x3thm1, const double x1mth2,
/dports/astro/py-pykep/pykep-2.6/include/keplerian_toolbox/third_party/libsgp4/
H A DSGP4.h60 double x3thm1; member
192 const double aycof, const double x3thm1, const double x1mth2,
/dports/comms/gpredict/gpredict-2.2.1/src/sgpsdp/
H A Dsgp4sdp4.c53 sat->sgps.x3thm1 = 3 * theta2 - 1.0; in SGP4()
57 del1 = 1.5 * ck2 * sat->sgps.x3thm1 / (a1*a1*betao*betao2); in SGP4()
59 delo = 1.5 * ck2 * sat->sgps.x3thm1 / (ao*ao*betao*betao2); in SGP4()
96 0.75 * ck2 * tsi / psisq * sat->sgps.x3thm1 * in SGP4()
233 rk = r * (1.0 - 1.5 * temp2 * betal * sat->sgps.x3thm1) + in SGP4()
314 sat->sgps.x3thm1 = 3.0 * sat->deep_arg.theta2 - 1.0; in SDP4()
318 del1 = 1.5 * ck2 * sat->sgps.x3thm1 / in SDP4()
321 delo = 1.5 * ck2 * sat->sgps.x3thm1 / in SDP4()
353 sat->sgps.x3thm1 * (8.0 + 3.0 * etasq * in SDP4()
477 rk = r * (1.0 - 1.5 * temp2 * betal * sat->sgps.x3thm1) + in SDP4()
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H A Dsgp4sdp4.h137 double x1mth2,x3thm1,x7thm1,xmcof,xmdot,xnodcf,xnodot,xlcof; member
/dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/
H A DTLE.pm2994 my $x3thm1 = 3 * $theta2 - 1;
3039 (4 + $etasq)) + .75 * SGP_CK2 * $tsi / $psisq * $x3thm1
3059 my $xmdot = $xnodp + .5 * $temp1 * $beta0 * $x3thm1 + .0625 *
3113 X3THM1 = $x3thm1
3144 x3thm1 => $x3thm1,
3273 * $parm->{x3thm1});
3343 my $x3thm1 = 3 * $theta2 - 1;
3397 my $xmdot = $xnodp + .5 * $temp1 * $beta0 * $x3thm1 +
3431 X3THM1 = $x3thm1
3461 x3thm1 => $x3thm1,
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/dports/comms/predict/predict-2.2.7/
H A Dpredict.c794 x3thm1=3*theta2-1.0; in SGP4()
798 del1=1.5*ck2*x3thm1/(a1*a1*betao*betao2); in SGP4()
800 delo=1.5*ck2*x3thm1/(ao*ao*betao*betao2); in SGP4()
969 rk=r*(1-1.5*temp2*betal*x3thm1)+0.5*temp1*x1mth2*cos2u; in SGP4()
974 rfdotk=rfdot+xn*temp1*(x1mth2*cos2u+1.5*x3thm1); in SGP4()
1524 static double x3thm1, c1, x1mth2, c4, xnodcf, t2cof, xlcof, in SDP4() local
1550 x3thm1=3*deep_arg.theta2-1; in SDP4()
1554 del1=1.5*ck2*x3thm1/(a1*a1*deep_arg.betao*deep_arg.betao2); in SDP4()
1556 delo=1.5*ck2*x3thm1/(ao*ao*deep_arg.betao*deep_arg.betao2); in SDP4()
1699 rk=r*(1-1.5*temp2*betal*x3thm1)+0.5*temp1*x1mth2*cos2u; in SDP4()
[all …]