- printf("Pos = (%.2f,%.2f,%.2f) (Phi,Theta,Psi)=(%.2f,%.2f,%.2f)\n",
- FG_Longitude * 3600.0 * RAD_TO_DEG,
- FG_Latitude * 3600.0 * RAD_TO_DEG,
- FG_Altitude, FG_Phi, FG_Theta, FG_Psi);
- printf("Kts = %.0f Elev = %.2f, Aileron = %.2f, Rudder = %.2f Power = %.2f\n",
- FG_V_equiv_kts, FG_Elevator, FG_Aileron, FG_Rudder, FG_Throttle[0]);
+ fgPrintf( FG_FLIGHT, FG_DEBUG,
+ "Pos = (%.2f,%.2f,%.2f) (Phi,Theta,Psi)=(%.2f,%.2f,%.2f)\n",
+ FG_Longitude * 3600.0 * RAD_TO_DEG,
+ FG_Latitude * 3600.0 * RAD_TO_DEG,
+ FG_Altitude, FG_Phi, FG_Theta, FG_Psi);
+ fgPrintf( FG_FLIGHT, FG_DEBUG,
+ "Kts = %.0f Elev = %.2f, Aileron = %.2f, Rudder = %.2f Power = %.2f\n",
+ FG_V_equiv_kts, FG_Elevator, FG_Aileron, FG_Rudder, FG_Throttle[0]);