Uses of Class
fr.cnes.dynvol.gentleman.exceptions.calc.GtmInitException

Packages that use GtmInitException

Package	Description
fr.cnes.dynvol.gentleman.calc.data.forces	package linked to forces data
fr.cnes.dynvol.gentleman.calc.data.orbit	Package linked to initial orbit characteristics
fr.cnes.dynvol.gentleman.calc.data.propagation	Package for propagation data
fr.cnes.dynvol.gentleman.calc.data.vehicle	Package for vehicle characteristics.
fr.cnes.dynvol.gentleman.calc.propagation	Simulation package
fr.cnes.dynvol.gentleman.calc.util	Utilities package.
fr.cnes.dynvol.gentleman.gui.main	Package with main GUI classes.
fr.cnes.dynvol.gentleman.main	package for main classes.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.calc.data.forces

Constructors in fr.cnes.dynvol.gentleman.calc.data.forces that throw GtmInitException

Constructor and Description
GtmSimpleForces(int nz, int nt, boolean isDrag, boolean isSrp, boolean isSrpRediff, boolean isMoon, boolean isSun, fr.cnes.sirius.patrius.assembly.Assembly assembly, fr.cnes.sirius.patrius.bodies.ExtendedOneAxisEllipsoid ellips) Constructor.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.calc.data.orbit

Methods in fr.cnes.dynvol.gentleman.calc.data.orbit that throw GtmInitException

Modifier and Type	Method and Description
protected void	GtmLeoSimpleOrbit.buildOrbit() Method to build the initial ApsisOrbit orbit corresponding to the required hp/ha/inc.
protected void	GtmGeoSimpleOrbit.buildOrbit() Method to build the initial equinoctial orbit corresponding to the required hp/ha/inc and longitude.
protected abstract void	AbstractGtmSimpleOrbit.buildOrbit() Method to build the initial orbit initialization.

Constructors in fr.cnes.dynvol.gentleman.calc.data.orbit that throw GtmInitException

Constructor and Description
GtmGeoSimpleOrbit(fr.cnes.sirius.patrius.time.AbsoluteDate date, double dhp, double dha, double inc, double longi) Constructor
GtmLeoSimpleOrbit(fr.cnes.sirius.patrius.time.AbsoluteDate date, double hp, double ha, double inc) Constructor

Uses of GtmInitException in fr.cnes.dynvol.gentleman.calc.data.propagation

Constructors in fr.cnes.dynvol.gentleman.calc.data.propagation that throw GtmInitException

Constructor and Description
GtmPropagationData(double duration, double outputStep, double minStep, double maxStep, double tolAbsPos, double tolAbsVel, double tolRelPos, double tolRelVel) Constructor.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.calc.data.vehicle

Constructors in fr.cnes.dynvol.gentleman.calc.data.vehicle that throw GtmInitException

Constructor and Description
GtmSimpleVehicle(double dryMass, double mainArea, double spX, double spY, double spZ, double ergMass, double thrust, double isp) Constructor without aerodynamic properties.
GtmSimpleVehicle(double dryMass, double mainArea, double spX, double spY, double spZ, double cd, double ergMass, double thrust, double isp) Constructor with aerodynamic properties.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.calc.propagation

Methods in fr.cnes.dynvol.gentleman.calc.propagation that throw GtmInitException

Modifier and Type	Method and Description
void	AbstractGtmPropagator.propagate() Method to propagate the trajectory using PSIMU
void	AbstractGtmPropagator.setAttitude(fr.cnes.sirius.patrius.attitudes.AttitudeLaw law) Method to initialize attitude laws
protected void	GtmLeoPropagator.setDefaultAttitude() Method to initialize default attitude law
protected void	GtmGeoPropagator.setDefaultAttitude() Method to initialized attitude laws
protected abstract void	AbstractGtmPropagator.setDefaultAttitude() Method to initialize default attitude law
void	GtmLeoPropagator.setPropagationData(double duration, double outputStep) Method to initialize the numerical integration data.
void	GtmGeoPropagator.setPropagationData(double duration, double outputStep) Method to initialize the numerical integration data.
abstract void	AbstractGtmPropagator.setPropagationData(double duration, double outputStep) Method to initialize the numerical integration data only with duration and output step.
void	AbstractGtmPropagator.setPropagationData(GtmPropagationData data) Method to initialize the numerical integration data with full data.
void	AbstractGtmPropagator.setVehicle(fr.cnes.sirius.patrius.assembly.Vehicle veh) Vehicle initialization with a complete Vehicle object

Constructors in fr.cnes.dynvol.gentleman.calc.propagation that throw GtmInitException

Constructor and Description
AbstractGtmPropagator() Constructor.
GtmGeoPropagator() Constructor.
GtmLeoPropagator() Constructor.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.calc.util

Methods in fr.cnes.dynvol.gentleman.calc.util that throw GtmInitException

Modifier and Type	Method and Description
static List<fr.cnes.sirius.patrius.time.AbsoluteDate>	GtmDates.getListOfManeuverDates(String dirName, String fileName) Method to get list of maneuver dates.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.gui.main

Constructors in fr.cnes.dynvol.gentleman.gui.main that throw GtmInitException

Constructor and Description
WidGtm() Constructor.
WidGtmDataPanel() Constructor.

Uses of GtmInitException in fr.cnes.dynvol.gentleman.main

Methods in fr.cnes.dynvol.gentleman.main that throw GtmInitException

Modifier and Type	Method and Description
void	GtmBatch.propagate() Method used to propagate and so, ceate a spececraft list.

Constructors in fr.cnes.dynvol.gentleman.main that throw GtmInitException

Constructor and Description
GtmBatch(String inputFile, String outputDir, String saveSuffix) Constructor.