- #include <NavAttMsgPayload.h>
Structure used to define the output definition for attitude guidance.
[s] Current vehicle time-tag associated with measurements*/
Current spacecraft attitude (MRPs) of body relative to inertial */.
[r/s] Current spacecraft angular velocity vector of body frame B relative to inertial frame N, in B frame components
Current sun pointing vector in body frame.
- double timeTag¶