/dports/astro/stellarium/stellarium-0.21.3/src/core/planetsephems/ |
H A D | sidereal_time.c | 54 double get_mean_sidereal_time (double JD, double JDE) in get_mean_sidereal_time() argument 69 t=(JDE-2451545.)/36525.; in get_mean_sidereal_time() 93 double get_apparent_sidereal_time (double JD, double JDE) in get_apparent_sidereal_time() argument 95 double meanSidereal = get_mean_sidereal_time (JD, JDE); in get_apparent_sidereal_time() 99 getNutationAngles(JDE, &deltaPsi, &deltaEps); in get_apparent_sidereal_time() 101 return meanSidereal+ (deltaPsi*cos(getPrecessionAngleVondrakEpsilon(JDE) + deltaEps))*180./M_PI; in get_apparent_sidereal_time()
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H A D | precession.c | 394 void getNutationAngles(const double JDE, double *deltaPsi, double *deltaEpsilon) in getNutationAngles() argument 405 if ((JDE<=NUT_BEGIN-NUT_TRANSITION ) || (JDE>=NUT_END + NUT_TRANSITION)) in getNutationAngles() 412 if (fabs(JDE-c_jdeLastNut)>NUTATION_EPOCH_THRESHOLD) in getNutationAngles() 414 c_jdeLastNut=JDE; in getNutationAngles() 415 double t=(JDE-2451545.0)/36525.0; in getNutationAngles() 447 if (JDE<NUT_BEGIN) in getNutationAngles() 449 limiter=1.-(NUT_BEGIN-JDE)/NUT_TRANSITION; in getNutationAngles() 451 if (JDE>NUT_END) in getNutationAngles() 453 limiter=1.-(JDE-NUT_END)/NUT_TRANSITION; in getNutationAngles()
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H A D | sidereal_time.h | 29 double get_mean_sidereal_time (double JD, double JDE); 32 double get_apparent_sidereal_time (double JD, double JDE);
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H A D | precession.h | 69 void getNutationAngles(const double JDE, double *deltaPsi, double *deltaEpsilon);
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/dports/astro/stellarium/stellarium-0.21.3/src/core/modules/ |
H A D | Orbit.hpp | 31 … virtual void positionAtTimevInVSOP87Coordinates(double JDE, double* v){Q_UNUSED(JDE) Q_UNUSED(v)} in positionAtTimevInVSOP87Coordinates() argument 102 virtual void positionAtTimevInVSOP87Coordinates(double JDE, double* v) Q_DECL_OVERRIDE; 117 …bool objectDateValid(const double JDE) const { return ((orbitGood==0.) || (fabs(epochJDE-JDE)<qMin… in objectDateValid() 122 …ool objectDateGoodEnoughForOrbits(const double JDE) const { return ((orbitGood==0.) || (fabs(epoch… in objectDateGoodEnoughForOrbits() 159 virtual void positionAtTimevInVSOP87Coordinates(double JDE, double* v) Q_DECL_OVERRIDE;
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H A D | Orbit.cpp | 199 void KeplerOrbit::positionAtTimevInVSOP87Coordinates(double JDE, double *v) in positionAtTimevInVSOP87Coordinates() argument 201 JDE -= t0; in positionAtTimevInVSOP87Coordinates() 203 if (e < 1.0) InitEll(JDE,rCosNu,rSinNu); // Laguerre-Conway seems stable enough to go for <1.0. in positionAtTimevInVSOP87Coordinates() 207 InitHyp(JDE,rCosNu,rSinNu); in positionAtTimevInVSOP87Coordinates() 209 else InitPar(JDE,rCosNu,rSinNu); in positionAtTimevInVSOP87Coordinates() 300 void GimbalOrbit::positionAtTimevInVSOP87Coordinates(double JDE, double* v) in positionAtTimevInVSOP87Coordinates() argument 302 Q_UNUSED(JDE) in positionAtTimevInVSOP87Coordinates()
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H A D | RotationElements.cpp | 41 const double d=(JDE-J2000); in updatePlanetCorrections() 46 if (fabs(JDE-planetCorrections.JDE_E)>StelCore::JD_MINUTE) in updatePlanetCorrections() 48 planetCorrections.JDE_E=JDE; // keep record of when these values are valid. in updatePlanetCorrections() 65 if (fabs(JDE-planetCorrections.JDE_E)>5*StelCore::JD_MINUTE) in updatePlanetCorrections() 67 planetCorrections.JDE_M=JDE; // keep record of when these values are valid. in updatePlanetCorrections() 83 planetCorrections.JDE_J=JDE; // keep record of when these values are valid. in updatePlanetCorrections() 102 planetCorrections.JDE_S=JDE; // keep record of when these values are valid. in updatePlanetCorrections() 114 planetCorrections.JDE_U=JDE; // keep record of when these values are valid. in updatePlanetCorrections() 277 const double JDE=d+J2000; in corrWJupiter() 288 customGrsLongitude + customGrsDrift*(JDE - customGrsJD)/365.25 : in corrWJupiter() [all …]
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H A D | Planet.hpp | 240 bool hasValidPositionalData(const double JDE, const PositionQuality purpose) const; 313 double getSiderealTime(double JD, double JDE) const; 350 double getRotObliquity(double JDE) const; 362 void computeTransMatrix(double JD, double JDE);
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H A D | Planet.cpp | 1569 double Planet::getRotObliquity(double JDE) const in getRotObliquity() 1573 return getPrecessionAngleVondrakEpsilon(JDE); in getRotObliquity() 1655 void Planet::computeTransMatrix(double JD, double JDE) in computeTransMatrix() argument 1674 getPrecessionAnglesVondrak(JDE, &eps_A, &chi_A, &omega_A, &psi_A); in computeTransMatrix() 1685 getNutationAngles(JDE, &deltaPsi, &deltaEps); in computeTransMatrix() 1696 const double t=(JDE-J2000); in computeTransMatrix() 1821 double Planet::getSiderealTime(double JD, double JDE) const in getSiderealTime() 1826 return get_apparent_sidereal_time(JD, JDE); // degrees in getSiderealTime() 1828 return get_mean_sidereal_time(JD, JDE); // degrees in getSiderealTime() 1836 const double t=JDE-J2000; in getSiderealTime() [all …]
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H A D | RotationElements.hpp | 187 static void updatePlanetCorrections(const double JDE, const PlanetCorrection planet);
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/dports/astro/stellarium/stellarium-0.21.3/src/tests/ |
H A D | testSiderealTime.cpp | 75 double JD, JDE, s, est, ast, actualError, acceptableError = 2e-4; in testGreenwichMeanSiderealTime() local 81 JDE = JD + StelUtils::getDeltaTByEspenakMeeus(JD)/86400.; in testGreenwichMeanSiderealTime() 86 ast = get_mean_sidereal_time(JD, JDE)/15.; in testGreenwichMeanSiderealTime() 111 double JD, JDE, s, est, ast, actualError, acceptableError = 1e-4; in testGreenwichApparentSiderealTime() local 117 JDE = JD + StelUtils::getDeltaTByEspenakMeeus(JD)/86400.; in testGreenwichApparentSiderealTime() 122 ast = get_apparent_sidereal_time(JD, JDE)/15.; in testGreenwichApparentSiderealTime()
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/dports/astro/libnova/libnova-0.15.0/src/ |
H A D | dynamical_time.c | 217 double JDE; in ln_get_jde() local 220 JDE = JD + ln_get_dynamical_time_diff (JD) / secs_in_day; in ln_get_jde() 222 return JDE; in ln_get_jde()
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H A D | nutation.c | 192 long double D,M,MM,F,O,T,T2,T3,JDE; in ln_get_nutation() local 203 JDE = ln_get_jde (JD); in ln_get_nutation() 206 T = (JDE - 2451545.0)/36525; in ln_get_nutation()
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/dports/math/fricas/fricas-1.3.7/src/input/ |
H A D | jet.input | 5 de := JDE(jb, jb1) 20 de := JDE(jb, jb1) 35 de := JDE(jb, jb1) 50 de := JDE(jb, jbe) 68 de := JDE(jb, jb1)
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/dports/astro/py-pymeeus/PyMeeus-0.3.6/docs/source/ |
H A D | ex-Epoch.rst | 14 print_me("JDE for 1987/6/19.5", e) 16 # JDE for 1987/6/19.5: 2446966.00064 22 print_me("JDE for 333/1/27.5", e) 24 # JDE for 333/1/27.5: 1842713.0 32 print_me("JDE for 837/4/10.3", f) 34 # JDE for 837/4/10.3: 2026871.8 91 We can convert the internal JDE value back to a date:: 99 print_me("Date from JDE 2436116.31", s) 101 # Date from JDE 2436116.31: 1957/10/4.81
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/dports/math/fricas/fricas-1.3.7/pre-generated/src/algebra/ |
H A D | JDE.lsp | 2 (SDEFUN |JDE;setSimpMode;2Nni;1| 7 (SDEFUN |JDE;adapt| 164 (SDEFUN |JDE;jacobiMatrix;$L;6| 280 (SDEFUN |JDE;makeSystem2| 518 (SDEFUN |JDE;dimension;$2Nni;14| 595 (SDEFUN |JDE;simplify;$R;15| 908 (SDEFUN |JDE;prolong;$R;17| 1147 (SDEFUN |JDE;prolong;$NniR;18| 1590 (SDEFUN |JDE;prolongMV;2R;22| 1618 (SDEFUN |JDE;power| [all …]
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/dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/ |
H A D | Sun.pm | 623 my $JDE = 0.00001 * $S / $delta_lambda + $JDE0; 625 and print "Debug - JDE = $JDE\n"; 626 my $time = ( $JDE - JD_OF_EPOCH ) * SECSPERDAY;
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/dports/astro/stellarium/stellarium-0.21.3/src/core/ |
H A D | StelObserver.hpp | 65 Mat4d getRotAltAzToEquatorial(double JD, double JDE) const;
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H A D | StelObserver.cpp | 223 Mat4d StelObserver::getRotAltAzToEquatorial(double JD, double JDE) const in getRotAltAzToEquatorial() 229 …return Mat4d::zrotation((getHomePlanet()->getSiderealTime(JD, JDE)+static_cast<double>(currentLoca… in getRotAltAzToEquatorial()
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/dports/science/py-pygmo2/pygmo2-2.18.0/doc/tutorials/ |
H A D | cec2013_comp.rst | 55 :alt: CEC2013-JDE-2D 121 :alt: CEC2013-JDE-10D
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/dports/astro/py-ephem/ephem-4.1.3/libastro/ |
H A D | satmoon.c | 210 double JDE,LPE,LPP,LEE,LEP; in bruton_saturn() local 258 JDE = 2444238.5; /* Epoch Jan 0.0 1980 = December 31,1979 0:0:0 UT */ in bruton_saturn() 280 NN = JD - JDE; /* NN = Number of days since epoch */ in bruton_saturn()
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/dports/editors/emacs-devel/emacs-4d1968b/lisp/calendar/ |
H A D | lunar.el | 295 (JDE (+ 2451550.09765 388 (newJDE (+ JDE correction additional)))
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/dports/editors/emacs/emacs-27.2/lisp/calendar/ |
H A D | lunar.el | 273 (JDE (+ 2451550.09765 366 (newJDE (+ JDE correction additional)))
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/dports/arabic/libitl/ITL-f8f41cc/prayertime/ |
H A D | astro.c | 717 double JDE = JD; in computeAstroDay() local 719 double T = (JDE - 2451545)/36525.0; in computeAstroDay()
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/dports/astro/stellarium/stellarium-0.21.3/guide/ |
H A D | app_ssystem_ini.tex | 349 \item[orbit\_Epoch] JDE when these elements are valid. Defaults to 413 \item[orbit\_Epoch], JDE when these elements are valid. Defaults to J2000.0, i.e., 2451545.0. 449 \item[orbit\_TimeAtPericenter] $T$ JDE of closest approach to the Sun 450 \item[orbit\_Epoch] JDE when these elements are valid (optional).
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