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 | IERS |
| Class to easy handle IERS Earth Orientation Data globally. 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... | |
Functions | |
| std::ostream & | gpstk::operator<< (std::ostream &s, const gpstk::ForceModel &fm) |
| Stream output for CommonTime 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 CommonTime objects. | |
| void | gpstk::GPST2UTC (const CommonTime &gpst, UTCTime &utc) |
| GPS time to UTC time. | |
| void | gpstk::UTC2GPST (const UTCTime &utc, CommonTime &gpst) |
| UTC time to GPS time. | |
| void | gpstk::UT12UTC (const UTCTime &ut1, UTCTime &utc) |
| UT1 time to UTC time. | |
| void | gpstk::UTC2UT1 (const UTCTime &utc, UTCTime &ut1) |
| UTC time to UT1 time. | |
| void | gpstk::TT2UTC (const CommonTime &tt, UTCTime &utc) |
| TT time to UTC time. | |
| void | gpstk::UTC2TT (const UTCTime &utc, CommonTime &tt) |
| UTC time to TT time. | |
| void | gpstk::TAI2UTC (const CommonTime &tai, UTCTime &utc) |
| TAI time to UTC time. | |
| void | gpstk::UTC2TAI (const UTCTime &utc, CommonTime &tai) |
| UTC time to TAI time. | |
| void | gpstk::BDT2UTC (const CommonTime &bdt, UTCTime &utc) |
| BDT time to UTC time. | |
| void | gpstk::UTC2BDT (const UTCTime &utc, CommonTime &bdt) |
| UTC time to BDT time. | |
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BDT time to UTC time.
Definition at line 489 of file UTCTime.cpp. References gpstk::GPST2UTC(). |
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GPS time to UTC time.
Referenced by gpstk::BDT2UTC(). |
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Stream output for CommonTime objects. Typically used for debugging.
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Stream output for OrbitPropagator objects. Typically used for debugging.
Definition at line 342 of file SatOrbitPropagator.cpp. |
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Stream output for CommonTime objects. Typically used for debugging.
Definition at line 266 of file ForceModel.hpp. References ForceModel::getAccel(), ForceModel::getAMatrix(), ForceModel::partialP(), ForceModel::partialR(), and ForceModel::partialV(). |
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TAI time to UTC time.
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TT time to UTC time.
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UT1 time to UTC time.
Definition at line 399 of file UTCTime.cpp. References gpstk::UT1mUTC(). |
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UTC time to BDT time.
Definition at line 500 of file UTCTime.cpp. References gpstk::UTC2GPST(). |
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UTC time to GPS time.
Definition at line 389 of file UTCTime.cpp. Referenced by gpstk::UTC2BDT(). |
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UTC time to TAI time.
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UTC time to TT time.
Definition at line 449 of file UTCTime.cpp. Referenced by gpstk::ECEFPosVelToJ2k(), gpstk::J2kPosVelToECEF(), and gpstk::J2kToECEFMatrix(). |
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UTC time to UT1 time.
Definition at line 416 of file UTCTime.cpp. Referenced by gpstk::J2kToECEFMatrix(). |
1.3.9.1