vPilotAccel.InitMatrix();
if( Translation->GetVt() > 1 ) {
vToEyePt = Aircraft->GetXYZep() - MassBalance->GetXYZcg();
-
+ vToEyePt *= inchtoft;
vPilotAccel = Aerodynamics->GetForces()
+ Propulsion->GetForces()
+ GroundReactions->GetForces();
vPilotAccel /= MassBalance->GetMass();
vPilotAccel += Rotation->GetPQRdot() * vToEyePt;
vPilotAccel += Rotation->GetPQR() * (Rotation->GetPQR() * vToEyePt);
+ //vPilotAccel(2)*=-1;
}
earthPosAngle += State->Getdt()*Inertial->omega();
return false;