Declared in StateEffector
Declaration
void ComputeDerivatives(
double time,
Vector3 rDDot_BN_N,
Vector3 omegaDot_BN_B,
Vector3 sigma_BN
);Description
Computers the Derivatives of the Body along with the Kinematic Derivatives
Parameters
| Name | Description |
|---|---|
| time | The current computation time |
| rDDot_BN_N | The acceleration in the body frame |
| omegaDot_BN_B | The derivative of the attitude rate in the body frame |
| sigma_BN | The current attitude in the body frame |