Class AttitudeErrorMessage
- Namespace
- NominalSystems.Messages
- Assembly
- NominalSystems.Messages.dll
[Nominal] Message used to define the output definition for attitude error, the difference between the reference and current attitude of a spacecraft.
public sealed class AttitudeErrorMessage : Message
- Inheritance
-
AttitudeErrorMessage
Fields
OmegaDot_RN_B
Reference frame inertial body acceleration of the reference frame relative to the inertial frame in the body coordinates. components.
[Unit(UnitType.RADIAN_PER_SECOND_SQUARED)]
public Vector3 OmegaDot_RN_B
Field Value
Omega_BR_B
Current body error estimate of the body relative to the reference frame using the body-frame coordinates.
[Unit(UnitType.RADIAN_PER_SECOND)]
public Vector3 Omega_BR_B
Field Value
Omega_RN_B
Reference frame rate vector of the of reference frame relative to the inertial frame in the body coordinates.
[Unit(UnitType.RADIAN_PER_SECOND)]
public Vector3 Omega_RN_B
Field Value
Sigma_BR
Current attitude error estimate (MRPs) of the body in the reference frame.
[Unit(UnitType.NONE)]
public Vector3 Sigma_BR