AttGuidMsgPayload

struct AttGuidMsgPayload

#include <AttGuidMsgPayload.h>

Structure used to define the output definition for attitude guidance.

Public Members

double sigma_BR[3]: Current attitude error estimate (MRPs) of B relative to R*/.

double omega_BR_B[3]: [r/s] Current body error estimate of B relateive to R in B frame compoonents */

double omega_RN_B[3]: [r/s] Reference frame rate vector of the of R relative to N in B frame components */

double domega_RN_B[3]: [r/s2] Reference frame inertial body acceleration of R relative to N in B frame components */