Declared in SpacecraftStateMessage
Declaration
[Unit("kg·m²")]
Vector3 RotationalAngularMomentum_CN_B;Description
Contribution of the state effector to total rotational angular momentum of the center of mass relative to the body frame.
Declared in SpacecraftStateMessage
[Unit("kg·m²")]
Vector3 RotationalAngularMomentum_CN_B;Contribution of the state effector to total rotational angular momentum of the center of mass relative to the body frame.