Make yasim accept the launchbar and hook properties. They are not tied to anything...

[flightgear.git] / src / FDM / JSBSim / FGNozzle.cpp

diff --git a/src/FDM/JSBSim/FGNozzle.cpp b/src/FDM/JSBSim/FGNozzle.cpp
index fa890f2ee884589d2ec3f0f3b4092c4031babfd3..c159c12a78acd23bf7e6b6515883a4c79efe5e67 100644 (file)
--- a/src/FDM/JSBSim/FGNozzle.cpp
+++ b/src/FDM/JSBSim/FGNozzle.cpp
@@ -50,7 +50,7 @@ CLASS IMPLEMENTATION
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
 
-FGNozzle::FGNozzle(FGFDMExec* FDMExec, FGConfigFile* Nzl_cfg) : FGThruster(FDMExec)
+FGNozzle::FGNozzle(FGFDMExec* FDMExec, FGConfigFile* Nzl_cfg, int num) : FGThruster(FDMExec)
 {
   string token;
 
@@ -66,11 +66,14 @@ FGNozzle::FGNozzle(FGFDMExec* FDMExec, FGConfigFile* Nzl_cfg) : FGThruster(FDMEx
   }
 
   Thrust = 0;
-  ReverserAngle = 0.0;
   Type = ttNozzle;
   Area2 = (Diameter*Diameter/4.0)*M_PI;
   AreaT = Area2/ExpR;
 
+  char property_name[80];
+  snprintf(property_name, 80, "propulsion/c-thrust[%u]", EngineNum);
+  PropertyManager->Tie( property_name, &ThrustCoeff );
+
   Debug(0);
 }
 
@@ -78,6 +81,10 @@ FGNozzle::FGNozzle(FGFDMExec* FDMExec, FGConfigFile* Nzl_cfg) : FGThruster(FDMEx
 
 FGNozzle::~FGNozzle()
 {
+  char property_name[80];
+  snprintf(property_name, 80, "propulsion/c-thrust[%u]", EngineNum);
+  PropertyManager->Untie( property_name );
+
   Debug(1);
 }
 
@@ -87,7 +94,9 @@ double FGNozzle::Calculate(double CfPc)
 {
   double pAtm = fdmex->GetAtmosphere()->GetPressure();
   Thrust = max((double)0.0, (CfPc * AreaT + (PE - pAtm)*Area2) * nzlEff);
-  vFn(1) = Thrust * cos(ReverserAngle);
+  vFn(1) = Thrust;
+
+  ThrustCoeff = max((double)0.0, CfPc / ((pAtm - PE) * Area2));
 
   return Thrust;
 }
@@ -101,7 +110,7 @@ double FGNozzle::GetPowerRequired(void)
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-string FGNozzle::GetThrusterLabels(int id)
+string FGNozzle::GetThrusterLabels(int id, string delimeter)
 {
   std::ostringstream buf;
 
@@ -112,7 +121,7 @@ string FGNozzle::GetThrusterLabels(int id)
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
-string FGNozzle::GetThrusterValues(int id)
+string FGNozzle::GetThrusterValues(int id, string delimeter)
 {
   std::ostringstream buf;