navAttIntMsg

struct NavAttIntMsg

#include <navAttIntMsg.h>

Structure used to define the output definition for attitude guidance.

Public Members

double timeTag

[s] Current vehicle time-tag associated with measurements*/

double sigma_BN[3]

Current spacecraft attitude (MRPs) of body relative to inertial */.

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

double vehSunPntBdy[3]

Current sun pointing vector in body frame.