public BasicManeuverStrategy3dExampleNav()
{
m_accelCommand = new AgCartVec3();
m_coriolisAccel = new AgCartVec3();
m_centripetalAccel = new AgCartVec3();
m_PQR = new AgCartVec3();
m_earthOmegaInRefAxes = new AgCartVec3();
m_ecfToRefAxesQuat = new AgQuaternion();
}
public void SetInitialState(AgEFlightPerformanceMode ePerfMode, AgEFlightPhaseOfFlight ePhaseOfFlight, IAgFlightBasicManeuverState pInitState, IAgFlightDoubleArray presultAuxInitState)
{
AgQuaternion pRefAxesQuat = new AgQuaternion();
AgCartVec3 pRefAxesAngVel = new AgCartVec3();
// generate the default ref axes coordinate frame ...
pInitState.ComputeStandardECFToRefAxesFrame(
true, AgEFlightAxesOrientation.eFwdRightDown, pRefAxesQuat, pRefAxesAngVel);
// tell the system to use that ref axes frame (can only be done during SetInitialState)...
pInitState.SetInitialECFToRefAxesFrame(AgEFlightAxesOrientation.eFwdRightDown, pRefAxesQuat, pRefAxesAngVel);
}