fr.cnes.dynvol.gentleman.calc.propagation

Class GtmLeoPropagator

java.lang.Object

fr.cnes.dynvol.gentleman.calc.propagation.AbstractGtmPropagator

fr.cnes.dynvol.gentleman.calc.propagation.GtmLeoPropagator

public class GtmLeoPropagator
extends AbstractGtmPropagator

Example allowing to numerically propagate a LEO orbit with maneuver sequence then to get corresponding TLEs.

Author:

goesterjf

Field Summary

Fields inherited from class fr.cnes.dynvol.gentleman.calc.propagation.AbstractGtmPropagator

assembly, attitudeLaw, ellips, forces, iniOrbit, integData, listOfevents, maneuverSequence, massModel, output, psimu, sun, vehicle

Constructor Summary

Constructors

Constructor and Description
GtmLeoPropagator() Constructor.

Method Summary

Modifier and Type	Method and Description
protected void	setDefaultAttitude() Method to initialize default attitude law
void	setPropagationData(double duration, double outputStep) Method to initialize the numerical integration data.

Methods inherited from class fr.cnes.dynvol.gentleman.calc.propagation.AbstractGtmPropagator

getAmountOfPoints, getAssembly, getEllipsoid, getIniOrbit, getIniVariables, getLastVariables, getListOfEngines, getListOfTanks, getMassModel, getPsimu, getSpacecraftStateList, getVariables, propagate, setAttitude, setEllipsoid, setEvents, setForces, setFramesConfiguration, setIniOrbit, setManeuvers, setOutputDir, setPropagationData, setVehicle

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Detail

GtmLeoPropagator

public GtmLeoPropagator()
                 throws GtmInitException

Constructor.

Throws:

GtmInitException - occured when initializing the Earth ellipsoid

Method Detail

setPropagationData

public void setPropagationData(double duration,
                               double outputStep)
                        throws GtmInitException

Method to initialize the numerical integration data.

Specified by:

setPropagationData in class AbstractGtmPropagator

Parameters:

duration - duration of the simulation (s)

outputStep - output step (s)

Throws:

GtmInitException - occured when initializing integrator data

setDefaultAttitude

protected void setDefaultAttitude()
                           throws GtmInitException

Method to initialize default attitude law

Specified by:

setDefaultAttitude in class AbstractGtmPropagator

Throws:

GtmInitException - exception occured when initialization of the default attitude