NavAttMsgPayload¶
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struct NavAttMsgPayload¶
- #include <NavAttMsgPayload.h>
Structure used to define the output definition for attitude guidance.
Public Members
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double timeTag¶
[s] Current vehicle time-tag associated with measurements*/
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double sigma_BN[3]¶
Current spacecraft attitude (MRPs) of body relative to inertial */.
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double omega_BN_B[3]¶
[r/s] Current spacecraft angular velocity vector of body frame B relative to inertial frame N, in B frame components
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double vehSunPntBdy[3]¶
Current sun pointing vector in body frame.
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double timeTag¶