Package | Description |
---|---|
org.orekit.forces |
This package provides the interface for force models that will be used by the
NumericalPropagator , as well as
some classical spacecraft models for surface forces (spherical, box and solar array ...). |
Constructor | Description |
---|---|
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets,
PVCoordinatesProvider sun,
double solarArrayArea,
org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis,
double dragCoeff,
double absorptionCoeff,
double reflectionCoeff) |
Build a spacecraft model with best lighting of solar array.
|
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets,
PVCoordinatesProvider sun,
double solarArrayArea,
org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis,
double dragCoeff,
double liftRatio,
double absorptionCoeff,
double reflectionCoeff) |
Build a spacecraft model with best lighting of solar array.
|
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets,
PVCoordinatesProvider sun,
double solarArrayArea,
org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis,
AbsoluteDate referenceDate,
org.hipparchus.geometry.euclidean.threed.Vector3D referenceNormal,
double rotationRate,
double dragCoeff,
double absorptionCoeff,
double reflectionCoeff) |
Build a spacecraft model with linear rotation of solar array.
|
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[] facets,
PVCoordinatesProvider sun,
double solarArrayArea,
org.hipparchus.geometry.euclidean.threed.Vector3D solarArrayAxis,
AbsoluteDate referenceDate,
org.hipparchus.geometry.euclidean.threed.Vector3D referenceNormal,
double rotationRate,
double dragCoeff,
double liftRatio,
double absorptionCoeff,
double reflectionCoeff) |
Build a spacecraft model with linear rotation of solar array.
|
Copyright © 2002-2019 CS Systèmes d'information. All rights reserved.