YASim airborne start-up

[flightgear.git] / src / FDM / YASim / Rotor.cpp

diff --git a/src/FDM/YASim/Rotor.cpp b/src/FDM/YASim/Rotor.cpp
index 797bf21ab4a01d81bc8b41780a48a633b062e159..79e5fd128ebc975304296913534d06d4b348eb17 100644 (file)
--- a/src/FDM/YASim/Rotor.cpp
+++ b/src/FDM/YASim/Rotor.cpp
@@ -1,3 +1,8 @@
+
+#ifdef HAVE_CONFIG_H
+#  include "config.h"
+#endif
+
 #include <simgear/debug/logstream.hxx>
 
 #include "Math.hpp"
@@ -1302,7 +1307,7 @@ void Rotor::compile()
         &(torque[1]),&(lift[1])); //pitch b
     rps[0]->calculateAlpha(v_wind,rho_null,0,0,0,
         &(torque[3]),&(lift[3])); //pitch 0
-    SG_LOG(SG_GENERAL, SG_INFO,
+    SG_LOG(SG_FLIGHT, SG_INFO,
         "Rotor: coefficients for airfoil:" << endl << setprecision(6)
         << " drag0: " << _dragcoef0*_number_of_parts/_number_of_blades/_c2
         << " drag1: " << _dragcoef1*_number_of_parts/_number_of_blades/_c2
@@ -1538,6 +1543,8 @@ void Rotorgear::calcForces(float* torqueOut)
         }
         total_torque*=-1;
         _ddt_omegarel=0;
+
+#if 0
         float rel_torque_engine=1;
         if (total_torque<=0)
             rel_torque_engine=0;
@@ -1546,6 +1553,7 @@ void Rotorgear::calcForces(float* torqueOut)
                 rel_torque_engine=1/max_torque_of_engine*total_torque;
             else
                 rel_torque_engine=0;
+#endif
 
         //add the rotor brake and the gear fritcion
         float dt=0.1f;