geodyn Directory Reference

Files
file	ASConstant.hpp
file	AtmosphericDrag.cpp
	This class computes the acceleration due to drag on a satellite using an Earth atmosphere model that conforms to the computeDensity abstract method.
file	AtmosphericDrag.hpp
	This class computes the acceleration due to drag on a satellite using an Earth atmosphere model that conforms to the computeDensity abstract method.
file	CiraExponentialDrag.cpp
	Computes the acceleration due to drag on a satellite using an exponential Earth atmosphere model.
file	CiraExponentialDrag.hpp
	Computes the acceleration due to drag on a satellite using an exponential Earth atmosphere model.
file	EarthBody.cpp
	Class to handle earth planet, it'll be taken as the central body of the spacecraft.
file	EarthBody.hpp
	Class to handle earth planet, it'll be taken as the central body of the spacecraft.
file	EarthOceanTide.cpp
file	EarthOceanTide.hpp
file	EarthPoleTide.cpp
file	EarthPoleTide.hpp
file	EarthSolidTide.cpp
	Class to do Earth Solid Tide correction.
file	EarthSolidTide.hpp
	Class to do Earth Solid Tide correction.
file	EGM96GravityModel.cpp
	EGM96 gravity model.
file	EGM96GravityModel.hpp
	EGM96 gravity model.
file	EquationOfMotion.hpp
	Class to provides the mechanism for passing a method that computes the derivatives to an integrator.
file	ForceModel.hpp
	Force Model is a simple interface which allows uniformity among the various force models.
file	ForceModelList.cpp
	ForceModelList is a countainer for force models.
file	ForceModelList.hpp
	ForceModelList is a countainer for force models.
file	HarrisPriesterDrag.cpp
	The HarrisPriester class computes the Harris-Priester atmosphere model.
file	HarrisPriesterDrag.hpp
	The HarrisPriester class computes the Harris-Priester atmosphere model.
file	IERS.cpp
	This class ease handling IERS earth orientation data.
file	IERS.hpp
	This class ease handling IERS earth orientation data.
file	IERSConventions.cpp
file	IERSConventions.hpp
file	Integrator.hpp
	This is an abstract base class for objects solving a ODE system with integrator.
file	JGM3GravityModel.cpp
	JGM3 gravity model.
file	JGM3GravityModel.hpp
	JGM3 gravity model.
file	KeplerOrbit.cpp
	Class to do Kepler orbit computation.
file	KeplerOrbit.hpp
	Class to do Kepler orbit computation.
file	LEOSatOrbit.cpp
	This class handle equation of motion for low earth orbit satellites.
file	LEOSatOrbit.hpp
	This class handle equation of motion for low earth orbit satellites.
file	MoonForce.cpp
	This class calculate the gravitational effect of the moon.
file	MoonForce.hpp
	This class calculate the gravitational effect of the moon.
file	Msise00Drag.cpp
	This class computes the NRLMSISE atmosphere model.
file	Msise00Drag.hpp
	This class computes the NRLMSISE atmosphere model.
file	NavSatOrbit.cpp
	This class handle equation of motion for navigation satellites.
file	NavSatOrbit.hpp
	This class handle equation of motion for navigation satellites.
file	PvtStore.cpp
file	PvtStore.hpp
file	ReferenceFrames.cpp
	Class to do Reference frame transformation.
file	ReferenceFrames.hpp
	Class to do Reference frame transformation.
file	RelativityEffect.cpp
	Calculate Relativity Effect to earth satellite.
file	RelativityEffect.hpp
	Calculate Relativity Effect to earth satellite.
file	RungeKuttaFehlberg.cpp
	This class do integrations with Runge Kutta Fehlberg algorithm.
file	RungeKuttaFehlberg.hpp
	This class do integrations with Runge Kutta Fehlberg algorithm.
file	SatOrbit.cpp
	This Class handle general orbit for different satellite orbit type.
file	SatOrbit.hpp
	This Class handle general orbit for different satellite orbit type.
file	SatOrbitPropagator.cpp
file	SatOrbitPropagator.hpp
file	SatOrbitStore.cpp
file	SatOrbitStore.hpp
file	SolarRadiationPressure.cpp
	This class provides a generic model for the influence of solar radiation pressure on a satellite.
file	SolarRadiationPressure.hpp
	This class provides a generic model for the influence of solar radiation pressure on a satellite.
file	Spacecraft.cpp
	The Spacecraft class encapsulates physical parameters.
file	Spacecraft.hpp
	The Spacecraft class encapsulates physical parameters.
file	SphericalHarmonicGravity.cpp
file	SphericalHarmonicGravity.hpp
file	SunForce.cpp
	This class calculate the gravitational effect of the Sun.
file	SunForce.hpp
	This class calculate the gravitational effect of the Sun.
file	UTCTime.cpp
	class to convert among different time systems
file	UTCTime.hpp
	class to convert among different time systems

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