X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FYASim%2FAirplane.cpp;h=82b10d7d144844c255759b23206c5a6867243f0e;hb=adeeed1a0e9dba19ba9e02f3fb28ba080e6ff021;hp=be30389c1a8580a36d676008eccf5d6dbb005b86;hpb=4535c84b993fb9b6adecc9a699309b329f23c4ee;p=flightgear.git

diff --git a/src/FDM/YASim/Airplane.cpp b/src/FDM/YASim/Airplane.cpp
index be30389c1..82b10d7d1 100644
--- a/src/FDM/YASim/Airplane.cpp
+++ b/src/FDM/YASim/Airplane.cpp
@@ -1,5 +1,3 @@
-#include <stdio.h>
-
 #include "Atmosphere.hpp"
 #include "ControlMap.hpp"
 #include "Gear.hpp"
@@ -892,13 +890,6 @@ void Airplane::solve()
 	_tailIncidence = clamp(_tailIncidence, -0.174f, 0.174f);
         _approachElevator.val = clamp(_approachElevator.val, -1.f, 1.f);
 
-        fprintf(stderr, "p0 %6f p1 %6f e %5f d %5f\n",
-                apitch0, apitch1, _approachElevator.val, elevDelta); // DEBUG
-
-        fprintf(stderr, "l %5f d %5f aoa %5f inc %5f ele %5f\n",
-                _liftRatio, _dragFactor, _cruiseAoA, _tailIncidence,
-                _approachElevator.val);
-
         if(norm(dragFactor) < 1.00001 &&
            norm(liftFactor) < 1.00001 &&
            abs(aoaDelta) < .000017 &&