Declared in NavigationAttitudeMessage
Declaration
[Unit("rad/s")]
Vector3 Omega_BN_B;Description
Current spacecraft angular velocity vector of body frame B relative to inertial frame N, in B frame components.
Declared in NavigationAttitudeMessage
[Unit("rad/s")]
Vector3 Omega_BN_B;Current spacecraft angular velocity vector of body frame B relative to inertial frame N, in B frame components.