Declared in SpacecraftStateMessage
Declaration
[Unit("kg·m²/s")]
Vector3 TotalOrbitalAngularMomentum_BN_N;Description
Total orbital angular momentum about the body relative to the inertial frame.
Declared in SpacecraftStateMessage
[Unit("kg·m²/s")]
Vector3 TotalOrbitalAngularMomentum_BN_N;Total orbital angular momentum about the body relative to the inertial frame.