Precessing Spin attitude profile, in which the spin axis of the satellite specified in the body frame is offset through the nutation angle away from the angular momentum direction specified in the inertial frame.

Body	Get the spin axis in the body frame.
Epoch	This property is deprecated. Use SmartEpoch instead. Epoch of the attitude profile. Uses DateFormat Dimension.
InertialPrecession	Get the precession in the inertial frame.
NutationAngle	Nutation angle by which the spin axis is offset from the angular momentum direction defined in the inertial frame. Uses Angle Dimension.
Precession	Get the precession rate and offset.
ReferenceAxes	Reference axes with respect to which precessing spin is defined. The satellite's body axes or any axes dependent upon the satellite's body axes are invalid for this attitude profile; all other axes are valid choices for the reference axes.
SmartEpoch	The epoch of the attitude profile.
Spin	Get the spin rate and offset.

Implemented Interface
IAgVeAttProfile

Name
AgVeProfilePrecessingSpin