Auxiliary->in.Tl2b = Propagate->GetTl2b();
Auxiliary->in.Tb2l = Propagate->GetTb2l();
Auxiliary->in.vPQR = Propagate->GetPQR();
- Auxiliary->in.vPQRdot = Accelerations->GetPQRdot();
+ Auxiliary->in.vPQRi = Propagate->GetPQRi();
+ Auxiliary->in.vPQRidot = Accelerations->GetPQRidot();
Auxiliary->in.vUVW = Propagate->GetUVW();
Auxiliary->in.vUVWdot = Accelerations->GetUVWdot();
Auxiliary->in.vVel = Propagate->GetVel();
// Nz is Acceleration in "g's", along normal axis (-Z body axis)
Nz = -vNcg(eZ);
Ny = vNcg(eY);
- vPilotAccel = in.vBodyAccel + in.vPQRdot * in.ToEyePt;
- vPilotAccel += in.vPQR * (in.vPQR * in.ToEyePt);
+ vPilotAccel = in.vBodyAccel + in.vPQRidot * in.ToEyePt;
+ vPilotAccel += in.vPQRi * (in.vPQRi * in.ToEyePt);
vNwcg = mTb2w * vNcg;
vNwcg(eZ) = 1.0 - vNwcg(eZ);