Show YASim config error messages.

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

diff --git a/src/FDM/YASim/Rotorpart.cpp b/src/FDM/YASim/Rotorpart.cpp
index 8736990026e415f2e63c7d15d6fcdb0825477f8d..bd54f41227590436931b53b0df3e13c256481ed8 100644 (file)
--- a/src/FDM/YASim/Rotorpart.cpp
+++ b/src/FDM/YASim/Rotorpart.cpp
@@ -99,7 +99,7 @@ void Rotorpart::inititeration(float dt,float *rot)
     float b;
     b=_rotor->getBalance();
     float s =Math::sin(_phi+_direction);
-    float c =Math::cos(_phi+_direction);
+    //float c =Math::cos(_phi+_direction);
     if (s>0)
         _balance=(b>0)?(1.-s*(1.-b)):(1.-s)*(1.+b);
     else
@@ -111,7 +111,7 @@ void Rotorpart::setRotor(Rotor *rotor)
     _rotor=rotor;
 }
 
-void Rotorpart::setParameter(char *parametername, float value)
+void Rotorpart::setParameter(const char *parametername, float value)
 {
 #define p(a) if (strcmp(parametername,#a)==0) _##a = value; else
 
@@ -548,7 +548,7 @@ void Rotorpart::calcForce(float* v, float rho,  float* out, float* torque,
 
     float dirblade[3];
     Math::cross3(_normal,_directionofcentripetalforce,dirblade);
-    float vblade=Math::abs(Math::dot3(dirblade,v));
+    //float vblade=Math::abs(Math::dot3(dirblade,v));
 
     alpha=_alphaalt+(alpha-_alphaalt)*factor;
     _alpha=alpha;