GeoDynamics

Classes
class	AtmosphericDrag
	This class computes the acceleration due to drag on a satellite using an Earth atmosphere model that conforms to the computeDensity abstract method. More...
class	CiraExponentialDrag
	This class computes the acceleration due to drag on a satellite using an exponential Earth atmosphere model. More...
class	EarthBody
	Class to handle earth planet, it'll be taken as the central body of the spacecraft. More...
class	EarthOceanTide
	Solid Earth Ocean Tide reference: IERS Conventions 2003. More...
class	EarthPoleTide
	Solid Earth Pole Tide reference: IERS Conventions 2003. More...
class	EarthSolidTide
	Class to do Earth Solid Tide correction reference: IERS Conventions 2003. More...
class	EGM96GravityModel
	EGM96 gravity model. More...
class	EquationOfMotion
	The EquationsOfMotion provides the mechanism for passing a method that computes the derivatives to an integrator. More...
class	ForceModel
	Force Model is a simple interface which allows uniformity among the various force models. More...
class	ForceModelList
	ForceModelList is a countainer for force models. More...
class	HarrisPriesterDrag
	The HarrisPriester class computes the Harris-Priester atmosphere model. More...
class	Integrator
	This is an abstract base class for objects solving a ODE system with integrator. More...
class	JGM3GravityModel
	JGM3 gravity model. More...
class	KeplerOrbit
	This class do some useful Keplerian orbit computation. More...
class	LEOSatOrbit
	This class handle equation of motion for low earth orbit satellites. More...
class	MoonForce
	This class calculate the gravitational effect of the moon. More...
class	Msise00Drag
	This class computes the NRLMSISE atmosphere model. More...
class	NavSatOrbit
	This class handle equation of motion for navigation satellites. More...
class	ReferenceFrames
	Class to do Reference frame transformation. More...
class	RelativityEffect
	This class calculate Relativity Effect to earth satellite. More...
struct	RungeKuttaFehlberg
	This class do integrations with Runge Kutta Fehlberg algorithm. More...
class	SatOrbit
	This Class handle general orbit for different satellite orbit type. More...
class	SatOrbitPropagator
	Satellite Orbit Progagator. More...
class	SolarRadiationPressure
	This class provides a generic model for the influence of solar radiation pressure on a satellite. More...
class	Spacecraft
	The Spacecraft class encapsulates physical parameters. More...
class	SphericalHarmonicGravity
	This class computes the body fixed acceleration due to the harmonic gravity field of the central body. More...
class	SunForce
	This class calculate the gravitational effect of the Sun. More...
class	UTCTime
	Class to convert UTC Time to all other different time systems. More...
class	IERS
	Class to easy handle IERS Earth Orientation Data globally. More...
Functions
std::ostream &	gpstk::operator<< (std::ostream &s, const gpstk::ForceModel &fm)
	Stream output for DayTime objects.
ostream &	gpstk::operator<< (ostream &s, SatOrbitPropagator &op)
	Stream output for OrbitPropagator objects.
std::ostream &	gpstk::operator<< (std::ostream &s, const gpstk::Spacecraft &sc)
	Stream output for DayTime objects.
void	gpstk::GPST2UTC (const DayTime &gpst, DayTime &utc)
	GPS time to UTC time.
void	gpstk::UTC2GPST (const DayTime &utc, DayTime &gpst)
	UTC time to GPS time.
void	gpstk::UT12UTC (const DayTime &ut1, DayTime &utc)
	UT1 time to UTC time.
void	gpstk::UTC2UT1 (const DayTime &utc, DayTime &ut1)
	UTC time to UT1 time.
void	gpstk::TT2UTC (const DayTime &tt, DayTime &utc)
	TT time to UTC time.
void	gpstk::UTC2TT (const DayTime &utc, DayTime &tt)
	UTC time to TT time.
void	gpstk::TAI2UTC (const DayTime &tai, DayTime &utc)
	TAI time to UTC time.
void	gpstk::UTC2TAI (const DayTime &utc, DayTime &tai)
	UTC time to TAI time.
void	gpstk::BDT2UTC (const DayTime &bdt, DayTime &utc)
	BDT time to UTC time.
void	gpstk::UTC2BDT (const DayTime &utc, DayTime &bdt)
	UTC time to BDT time.

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Function Documentation

void BDT2UTC (  const DayTime &  bdt, DayTime &  utc )

BDT time to UTC time. Parameters: bdt  BDT as input utc  UTC as output Definition at line 481 of file UTCTime.cpp. References gpstk::GPST2UTC(). Referenced by IERS::BDT2UTC().

void GPST2UTC (  const DayTime &  gpst, DayTime &  utc )

GPS time to UTC time. Parameters: gpst  GPST as input utc  UTC as output Definition at line 359 of file UTCTime.cpp. References DayTime::MJD(), and gpstk::TAImUTC(). Referenced by gpstk::BDT2UTC(), SatOrbitStore::getPvt(), and IERS::GPST2UTC().

std::ostream& operator<< (  std::ostream &  s, const gpstk::Spacecraft &  sc )

Stream output for DayTime objects. Typically used for debugging. Parameters: s  stream to append formatted DayTime to. t  DayTime to append to stream s. Returns: reference to s.

ostream & operator<< (  ostream &  s, SatOrbitPropagator &  op )

Stream output for OrbitPropagator objects. Typically used for debugging. Parameters: s  stream to append formatted DayTime to. t  DayTime to append to stream s. Returns: reference to s. Definition at line 342 of file SatOrbitPropagator.cpp.

std::ostream& operator<< (  std::ostream &  s, const gpstk::ForceModel &  fm )  [inline]

Stream output for DayTime objects. Typically used for debugging. Parameters: s  stream to append formatted DayTime to. t  DayTime to append to stream s. Returns: reference to s. Definition at line 266 of file ForceModel.hpp. References ForceModel::getAccel(), ForceModel::getAMatrix(), ForceModel::partialP(), ForceModel::partialR(), and ForceModel::partialV().

void TAI2UTC (  const DayTime &  tai, DayTime &  utc )

TAI time to UTC time. Parameters: tai  TAI as input utc  UTC as output Definition at line 450 of file UTCTime.cpp. References DayTime::MJD(), and gpstk::TAImUTC(). Referenced by IERS::TAI2UTC().

void TT2UTC (  const DayTime &  tt, DayTime &  utc )

TT time to UTC time. Parameters: tt  TT as input utc  UTC as output Definition at line 417 of file UTCTime.cpp. References DayTime::MJD(), and gpstk::TAImUTC(). Referenced by UTCTime::test(), and IERS::TT2UTC().

void UT12UTC (  const DayTime &  ut1, DayTime &  utc )

UT1 time to UTC time. Parameters: ut1  UT1 as input utc  UTC as output Definition at line 391 of file UTCTime.cpp. References DayTime::MJD(), DayTime::setYDoySod(), and gpstk::UT1mUTC(). Referenced by IERS::UT12UTC().

void UTC2BDT (  const DayTime &  utc, DayTime &  bdt )

UTC time to BDT time. Parameters: utc  UTC as input bdt  BDT as output Definition at line 492 of file UTCTime.cpp. References gpstk::UTC2GPST(). Referenced by IERS::UTC2BDT().

void UTC2GPST (  const DayTime &  utc, DayTime &  gpst )

UTC time to GPS time. Parameters: utc  UTC as input gpst  GPST as output Definition at line 381 of file UTCTime.cpp. References UTCTime::asGPST(). Referenced by gpstk::UTC2BDT(), and IERS::UTC2GPST().

void UTC2TAI (  const DayTime &  utc, DayTime &  tai )

UTC time to TAI time. Parameters: utc  UTC as input tai  TAI as output Definition at line 471 of file UTCTime.cpp. Referenced by IERS::UTC2TAI().

void UTC2TT (  const DayTime &  utc, DayTime &  tt )

UTC time to TT time. Parameters: UTC  UTC as input tt  TT as output Definition at line 441 of file UTCTime.cpp. Referenced by UTCTime::test(), and IERS::UTC2TT().

void UTC2UT1 (  const DayTime &  utc, DayTime &  ut1 )

UTC time to UT1 time. Parameters: utc  UTC as input ut1  UT1 as output Definition at line 408 of file UTCTime.cpp. Referenced by IERS::UTC2UT1().

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