Properties for the Thrust Vector attitude control for a Finite Maneuver.
![]() | How and when the attitude will be updated. |
![]() | Defines a constraint vector in spacecraft body coordinates to complete the attitude definition. |
![]() | Gets or sets the thrust axes. |
![]() | Defines the thrust vector in the reference axes. |
Implemented Interface |
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IAgVAAttitudeControl |
IAgVAAttitudeControlFinite |