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