Table of Contents

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

Vector3

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

Vector3

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

Vector3

Sigma_BR

Current attitude error estimate (MRPs) of the body in the reference frame.

[Unit(UnitType.NONE)]
public Vector3 Sigma_BR

Field Value

Vector3