| 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.
|
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