SCMassPropsMsgPayload

struct SCMassPropsMsgPayload

#include <SCMassPropsMsgPayload.h>

This structure is used in the messaging system to communicate what the mass properties of the vehicle are currently.

Public Members

double massSC

kg Current spacecraft mass

double c_B[3]

m Center of mass of spacecraft with respect to point B

double ISC_PntB_B[3][3]

kgm2 Inertia tensor of spacecraft (relative to body)