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public interface DragWrenchSensitive
Interface to represent solar drag wrench sensitive vehicles
Method Summary | |
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Wrench |
dragWrench(SpacecraftState state,
double density,
Vector3D relativeVelocity)
Compute the torque due to radiation pressire. |
Wrench |
dragWrench(SpacecraftState state,
double density,
Vector3D relativeVelocity,
Vector3D origin,
Frame frame)
Compute the torque due to radiation pressire. |
Method Detail |
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Wrench dragWrench(SpacecraftState state, double density, Vector3D relativeVelocity) throws OrekitException
The computation includes all spacecraft specific characteristics like shape, area and coefficients.
state
- current state information: date, kinematics, attitudedensity
- atmospheric density at spacecraft positionrelativeVelocity
- relative velocity of atmosphere with respect to spacecraft,
in the same inertial frame as spacecraft orbit
OrekitException
- if torque cannot be computedWrench dragWrench(SpacecraftState state, double density, Vector3D relativeVelocity, Vector3D origin, Frame frame) throws OrekitException
The computation includes all spacecraft specific characteristics like shape, area and coefficients.
state
- current state information: date, kinematics, attitudedensity
- atmospheric density at spacecraft positionrelativeVelocity
- relative velocity of atmosphere with respect to spacecraft,
in the same inertial frame as spacecraft orbitorigin
- point in which to express torqueframe
- the reference frame
OrekitException
- if torque cannot be computed
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