Use the density values from the environment subsystem, to properly handle

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

diff --git a/src/FDM/YASim/Airplane.cpp b/src/FDM/YASim/Airplane.cpp
index 77b13b56a377a9f10b2cbaee077ae898fcccb8c0..53df465421ad5f3165130c84b5348c2fcc4c3db7 100644 (file)
--- a/src/FDM/YASim/Airplane.cpp
+++ b/src/FDM/YASim/Airplane.cpp
@@ -667,7 +667,8 @@ void Airplane::runCruise()
 {
     setupState(_cruiseAoA, _cruiseSpeed, &_cruiseState);
     _model.setState(&_cruiseState);
-    _model.setAir(_cruiseP, _cruiseT);
+    _model.setAir(_cruiseP, _cruiseT,
+                  Atmosphere::calcStdDensity(_cruiseP, _cruiseT));
 
     // The control configuration
     _controls.reset();
@@ -691,7 +692,8 @@ void Airplane::runCruise()
     for(i=0; i<_thrusters.size(); i++) {
        Thruster* t = ((ThrustRec*)_thrusters.get(i))->thruster;
        t->setWind(wind);
-       t->setAir(_cruiseP, _cruiseT);
+       t->setAir(_cruiseP, _cruiseT,
+                  Atmosphere::calcStdDensity(_cruiseP, _cruiseT));
     }
     stabilizeThrust();
 
@@ -708,7 +710,8 @@ void Airplane::runApproach()
 {
     setupState(_approachAoA, _approachSpeed, &_approachState);
     _model.setState(&_approachState);
-    _model.setAir(_approachP, _approachT);
+    _model.setAir(_approachP, _approachT,
+                  Atmosphere::calcStdDensity(_approachP, _approachT));
 
     // The control configuration
     _controls.reset();
@@ -732,7 +735,8 @@ void Airplane::runApproach()
     for(i=0; i<_thrusters.size(); i++) {
        Thruster* t = ((ThrustRec*)_thrusters.get(i))->thruster;
        t->setWind(wind);
-       t->setAir(_approachP, _approachT);
+       t->setAir(_approachP, _approachT,
+                  Atmosphere::calcStdDensity(_approachP, _approachT));
     }
     stabilizeThrust();