Class SGP4
java.lang.Object
org.orekit.propagation.AbstractPropagator
org.orekit.propagation.analytical.AbstractAnalyticalPropagator
org.orekit.propagation.analytical.tle.TLEPropagator
org.orekit.propagation.analytical.tle.SGP4
- All Implemented Interfaces:
Propagator,PVCoordinatesProvider
This class contains methods to compute propagated coordinates with the SGP4 model.
The user should not bother in this class since it is handled internaly by the
TLEPropagator.
This implementation is largely inspired from the paper and source code Revisiting Spacetrack Report #3 and is fully compliant with its results and tests cases.
- Author:
- Felix R. Hoots, Ronald L. Roehrich, December 1980 (original fortran), David A. Vallado, Paul Crawford, Richard Hujsak, T.S. Kelso (C++ translation and improvements), Fabien Maussion (java translation)
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Field Summary
Fields inherited from class org.orekit.propagation.analytical.tle.TLEPropagator
a, a0dp, beta0, beta02, c1, c2, c4, coef, coef1, cosi0, e, e0sq, eeta, eta, etasq, i, omega, omgdot, perige, s4, sini0, t2cof, theta2, tle, tsi, utc, xl, xmdot, xn0dp, xnodcf, xnode, xnodotFields inherited from interface org.orekit.propagation.Propagator
DEFAULT_MASS -
Constructor Summary
ConstructorsConstructorDescriptionSGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass) Constructor for a unique initial TLE.SGP4(TLE initialTLE, AttitudeProvider attitudeProvider, double mass, Frame teme) Constructor for a unique initial TLE. -
Method Summary
Modifier and TypeMethodDescriptionprotected voidInitialization proper to each propagator (SGP or SDP).protected voidsxpPropagate(double tSince) Propagation proper to each propagator (SGP or SDP).Methods inherited from class org.orekit.propagation.analytical.tle.TLEPropagator
createHarvester, getDefaultTleGenerationAlgorithm, getFrame, getJacobiansColumnsNames, getMass, getMU, getPVCoordinates, getTLE, propagateOrbit, resetInitialState, resetIntermediateState, selectExtrapolator, selectExtrapolator, selectExtrapolator, selectExtrapolator, selectExtrapolatorMethods inherited from class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
acceptStep, addEventDetector, basicPropagate, clearEventsDetectors, clearMatricesComputation, getEphemerisGenerator, getEventDetectors, getPvProvider, propagateMethods inherited from class org.orekit.propagation.AbstractPropagator
addAdditionalDataProvider, getAdditionalDataProviders, getAttitudeProvider, getHarvester, getInitialState, getManagedAdditionalData, getMultiplexer, getStartDate, initializeAdditionalData, initializePropagation, isAdditionalDataManaged, propagate, removeAdditionalDataProvider, setAttitudeProvider, setStartDate, setupMatricesComputation, stateChanged, updateAdditionalData, updateUnmanagedDataMethods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitMethods inherited from interface org.orekit.propagation.Propagator
clearStepHandlers, getPosition, getPVCoordinates, getVelocity, setStepHandler, setStepHandler
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Constructor Details
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SGP4
Constructor for a unique initial TLE.This constructor uses the
default data context.- Parameters:
initialTLE- the TLE to propagate.attitudeProvider- provider for attitude computationmass- spacecraft mass (kg)- See Also:
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SGP4
Constructor for a unique initial TLE.- Parameters:
initialTLE- the TLE to propagate.attitudeProvider- provider for attitude computationmass- spacecraft mass (kg)teme- the TEME frame to use for propagation.- Since:
- 10.1
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Method Details
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sxpInitialize
protected void sxpInitialize()Initialization proper to each propagator (SGP or SDP).- Specified by:
sxpInitializein classTLEPropagator
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sxpPropagate
protected void sxpPropagate(double tSince) Propagation proper to each propagator (SGP or SDP).- Specified by:
sxpPropagatein classTLEPropagator- Parameters:
tSince- the offset from initial epoch (min)
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