Apparent(EphemerisFile::Handle &H) | pcl::Position | |
Apparent(const StarPosition &S) | pcl::Position | |
ApparentVisualMagnitude(EphemerisFile::Handle &H) | pcl::Position | |
Astrometric(EphemerisFile::Handle &H) | pcl::Position | |
Astrometric(const StarPosition &S) | pcl::Position | |
BarycentricPositionOfEarth() const | pcl::Position | inline |
BarycentricPositionOfSun() const | pcl::Position | inline |
BarycentricVelocityOfEarth() const | pcl::Position | inline |
CanComputeApparentVisualMagnitude(const EphemerisFile::Handle &H) const | pcl::Position | |
CanComputeCometApparentVisualNuclearMagnitude(const EphemerisFile::Handle &H) const | pcl::Position | |
CanComputeCometApparentVisualTotalMagnitude(const EphemerisFile::Handle &H) const | pcl::Position | |
CIO() | pcl::Position | inline |
CIOBiasPrecessionNutationInverseMatrix() | pcl::Position | inline |
CIOBiasPrecessionNutationMatrix() | pcl::Position | inline |
CIP() | pcl::Position | inline |
CIP_ITRS() const | pcl::Position | |
CometApparentVisualNuclearMagnitude(EphemerisFile::Handle &H) | pcl::Position | |
CometApparentVisualTotalMagnitude(EphemerisFile::Handle &H) | pcl::Position | |
DisablePolarMotion(bool disable=true) | pcl::Position | inline |
EclipticToEquatorial(const Vector &q, double se, double ce) | pcl::Position | inlinestatic |
EclipticToEquatorial(const Vector &q, double eps) | pcl::Position | inlinestatic |
EclipticToEquatorial(const DPoint &q, double se, double ce) | pcl::Position | inlinestatic |
EclipticToEquatorial(const DPoint &q, double eps) | pcl::Position | inlinestatic |
EnablePolarMotion(bool enable=true) | pcl::Position | inline |
EO() | pcl::Position | inline |
EpsA() const | pcl::Position | inline |
EquatorialToEcliptic(const Vector &q, double se, double ce) | pcl::Position | inlinestatic |
EquatorialToEcliptic(const Vector &q, double eps) | pcl::Position | inlinestatic |
EquatorialToEcliptic(const DPoint &q, double se, double ce) | pcl::Position | inlinestatic |
EquatorialToEcliptic(const DPoint &q, double eps) | pcl::Position | inlinestatic |
EquatorialToHorizontal(const DPoint &q) | pcl::Position | inline |
EquatorialToHorizontal(double ra, double dec) | pcl::Position | inline |
EquinoxBiasPrecessionNutationInverseMatrix() | pcl::Position | inline |
EquinoxBiasPrecessionNutationMatrix() | pcl::Position | inline |
ERA() | pcl::Position | inline |
GalacticToICRSEquatorial(const Vector &g) | pcl::Position | inlinestatic |
GalacticToICRSEquatorial(const DPoint &g) | pcl::Position | inlinestatic |
GAST() | pcl::Position | inline |
Geometric(EphemerisFile::Handle &H) | pcl::Position | |
Geometric(const StarPosition &S) | pcl::Position | |
HeliocentricPositionOfEarth() const | pcl::Position | inline |
ICRSEquatorialToGalactic(const Vector &q) | pcl::Position | inlinestatic |
ICRSEquatorialToGalactic(const DPoint &q) | pcl::Position | inlinestatic |
InitCIOBasedParameters() | pcl::Position | |
InitEquinoxBasedParameters() | pcl::Position | |
Intermediate(EphemerisFile::Handle &H) | pcl::Position | |
Intermediate(const StarPosition &S) | pcl::Position | |
IsPolarMotionEnabled() const | pcl::Position | inline |
IsTopocentric() const | pcl::Position | inline |
LightTravelTime(EphemerisFile::Handle &H) | pcl::Position | inline |
NutationAngles() | pcl::Position | inline |
Observer() const | pcl::Position | inline |
operator=(const Position &)=default | pcl::Position | |
operator=(Position &&)=default | pcl::Position | |
PhaseAngle(EphemerisFile::Handle &H) | pcl::Position | |
PhaseAngle(const StarPosition &S) | pcl::Position | |
Position(TimePoint t, const IsoString ×cale="TT") | pcl::Position | |
Position(const Position &)=default | pcl::Position | |
Position(Position &&)=default | pcl::Position | |
Proper(EphemerisFile::Handle &H) | pcl::Position | |
Proper(const StarPosition &S) | pcl::Position | |
SetGeocentric() | pcl::Position | |
SetObserver(const ObserverPosition &observer) | pcl::Position | |
TDB() const | pcl::Position | inline |
Teph() const | pcl::Position | inline |
True(EphemerisFile::Handle &H) | pcl::Position | inline |
True(const StarPosition &S) | pcl::Position | inline |
TrueDistance(EphemerisFile::Handle &H) | pcl::Position | inline |
TrueDistance(const StarPosition &S) | pcl::Position | inline |
TT() const | pcl::Position | inline |
UT1() const | pcl::Position | inline |
UTC() const | pcl::Position | inline |