This interface is deprecated. The \"Spin Aligned\" attitude definition is now deprecated because it may become ill-posed when configured with non-inertial spin vectors. It is recommended that instead \"Precessing Spin\" should be used.
![]() | Returns the available reference vectors |
![]() | Get the spin axis in the body frame. |
![]() | This property is deprecated. Use SmartEpoch instead. Epoch of the offset. Uses DateFormat Dimension. |
![]() | The nutation angle. Uses Angle Dimension. |
![]() | Get the precession data. |
![]() | The reference vector. Vectors dependent on the satellite's body axes are invalid for this attitude profile; all other vectors are valid choices for the reference vector. |
![]() | Epoch of the offset. |
![]() | Get the spin data. |
Implemented Interface |
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IAgVeAttProfile |