Uses of Class
fr.cnes.genopus.nonWidget.exception.NonWidgetException

Packages that use NonWidgetException

Package	Description
fr.cnes.genopus.nonWidget.attitudes	Package containing some objects related to attitudes intended to be added to PATRIUS.
fr.cnes.genopus.nonWidget.forces	Package containing some objects related to force intended to be added to PATRIUS.
fr.cnes.genopus.nonWidget.maneuvers	Package containing some objects related to maneuvers intended to be added to PATRIUS.
fr.cnes.genopus.nonWidget.vehicle	Package containing some objects related to vehicle intended to be added to PATRIUS.
fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs	Package containing some objects related to vehicle aerodynamic coefficients functions intended to be added to PATRIUS.
fr.cnes.genopus.nonWidget.vehicle.geometry	Package containing some objects related to vehicle geometry intended to be added to PATRIUS.

Uses of NonWidgetException in fr.cnes.genopus.nonWidget.attitudes

Methods in fr.cnes.genopus.nonWidget.attitudes that throw NonWidgetException

Modifier and Type	Method and Description
static double[]	CustomAeroAttitudeLaw.aircraftToAero(double slopeVel, double azimuthVel, double yaw, double pitch, double roll) Method to compute aerodynamic frame orientation angles with respect aircraft frame.
ArrayList<org.orekit.propagation.events.EventDetector>	CustomAttitudesSequence.getLoggedAttLawsDetectors() Get the list of logged switches events.

Uses of NonWidgetException in fr.cnes.genopus.nonWidget.forces

Methods in fr.cnes.genopus.nonWidget.forces that throw NonWidgetException

Modifier and Type	Method and Description
CustomAtmosphere	CustomDragForce.cloneAtmosphere() Get the atmosphere model as a new instance (to avoid problems related to threads).
void	CustomForceModels.updateAssembly(fr.cnes.sirius.patrius.assembly.Assembly assembly) Method to update the force models depending on the assembly (DragForce, CustomPatriusSolarRadiationPressure and CustomRediffusedRadiationPressure).

Constructors in fr.cnes.genopus.nonWidget.forces that throw NonWidgetException

Constructor and Description
CustomDragForce(CustomDragForce otherDragForce, fr.cnes.sirius.patrius.assembly.Assembly assembly) Creates a new instance from the data in another one but with a different assembly.
CustomDragForce(double k, CustomAtmosphere atmosphere, fr.cnes.sirius.patrius.assembly.Assembly assembly) Creates a new instance.

Uses of NonWidgetException in fr.cnes.genopus.nonWidget.maneuvers

Methods in fr.cnes.genopus.nonWidget.maneuvers that throw NonWidgetException

Modifier and Type	Method and Description
void	CustomManeuverSequence.addManeuver(CustomManeuverInterface man) Method to add a maneuver to the maneuver sequence.
List<org.orekit.propagation.events.EventDetector>	CustomManeuverSequence.getLoggedManeuversDetectors() Get list of maneuvers events.
void	CustomManeuverSequence.setManeuversDetectors(fr.cnes.sirius.patrius.events.CodedEventsLogger logger) Set list of maneuvers events.

Uses of NonWidgetException in fr.cnes.genopus.nonWidget.vehicle

Methods in fr.cnes.genopus.nonWidget.vehicle that throw NonWidgetException

Modifier and Type	Method and Description
double	CustomAerodynamicProperties.getConstantDragCoef() Get the drag coefficient.
double	CustomAerodynamicProperties.getConstantLiftCoef() Get the lift coefficient.

Uses of NonWidgetException in fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs

Methods in fr.cnes.genopus.nonWidget.vehicle.aeroCoeffs that throw NonWidgetException

Modifier and Type	Method and Description
protected static double	CustomAeroCoeffByAoA.angleOfAttackFromSpacecraftState(org.orekit.propagation.SpacecraftState state, org.orekit.bodies.ExtendedOneAxisEllipsoid earthShape) Computes the angle of attack from the spacecraft state and the Earth shape.
protected double	CustomAeroCoeffByAltitude.computeXVariable(org.orekit.propagation.SpacecraftState state) Computes the x variable from the spacecraft state.
protected abstract double	CustomAeroCoeffByOneVarAbstract.computeXVariable(org.orekit.propagation.SpacecraftState state) Computes the x variable from the spacecraft state.
protected double	CustomAeroCoeffByMach.computeXVariable(org.orekit.propagation.SpacecraftState state) Computes the x variable from the spacecraft state.
protected double	CustomAeroCoeffByAoA.computeXVariable(org.orekit.propagation.SpacecraftState state) Computes the x variable from the spacecraft state.
protected static double	CustomAeroCoeffByMach.machFromSpacecraftState(org.orekit.propagation.SpacecraftState state, org.orekit.forces.atmospheres.Atmosphere atmosphere) Computes the mach number from the spacecraft state and an atmosphere model.

Uses of NonWidgetException in fr.cnes.genopus.nonWidget.vehicle.geometry

Methods in fr.cnes.genopus.nonWidget.vehicle.geometry that throw NonWidgetException

Modifier and Type	Method and Description
double	CustomParallelepiped.getHeight() Get z direction dimension (m).
static double	CustomParallelepiped.getHeightFromSurfs(double surfX, double surfY, double surfZ) Get parallelepiped height (Z direction dimension).
double	CustomParallelepiped.getLength() Get x direction dimension (m).
double	CustomCylinder.getLength() Get length corresponding to transversal surface (x length) (m).
static double	CustomParallelepiped.getLengthFromSurfs(double surfX, double surfY, double surfZ) Get parallelepiped length (X direction dimension).
static double	CustomCylinder.getLenthFromTSurfaceAndRadius(double tarnsversalSurf, double radius) Get length from the transversal surface and radius.
double	CustomParallelepiped.getWidth() Get y direction dimension (m).
static double	CustomParallelepiped.getWidthFromSurfs(double surfX, double surfY, double surfZ) Get parallelepiped width (Y direction dimension).