Declared in AttitudeErrorMessage
Declaration
[Unit("rad/s²")]
Vector3 OmegaDot_RN_B;Description
Reference frame inertial body acceleration of the reference frame relative to the inertial frame in the body coordinates. components.
Declared in AttitudeErrorMessage
[Unit("rad/s²")]
Vector3 OmegaDot_RN_B;Reference frame inertial body acceleration of the reference frame relative to the inertial frame in the body coordinates. components.