vUVWdot = mVel*Rotation->GetPQR() + Aircraft->GetBodyAccel();
- vUVW += Tc * (vlastUVWdot + vUVWdot);
+ vUVW += Tc*(vUVWdot + vlastUVWdot);
+
vAeroUVW = vUVW + State->GetTl2b()*Atmosphere->GetWindNED();
Vt = vAeroUVW.Magnitude();
if (qbar > 1e6 || qbar < 0.00)
cout << "FGTranslation::qbar is out of bounds: " << qbar << endl;
}
+ if (debug_lvl & 64) {
+ if (from == 0) { // Constructor
+ cout << IdSrc << endl;
+ cout << IdHdr << endl;
+ }
+ }
}
+