Properties for the Thrust Vector attitude
control for an Impulsive Maneuver.
![]() |
True if the spherical magnitude should be allowed to be less than zero. |
![]() |
Defines a constraint vector in spacecraft body coordinates to complete the attitude definition. |
![]() |
The direction of the thrust. The AssignSpherical parameters Lat, Lon, Radius correspond to Elevation, Azimuth, and Magnitude. |
![]() |
This property is deprecated. Use DeltaVVector instead. |
![]() |
The thrust axes. |
Implemented Interface |
---|
IAgVAAttitudeControlImpulsive |