]> git.mxchange.org Git - flightgear.git/blobdiff - src/FDM/JSBSim/models/propulsion/FGElectric.cpp
Merge branch 'next' of gitorious.org:fg/flightgear into next
[flightgear.git] / src / FDM / JSBSim / models / propulsion / FGElectric.cpp
index cbcb9220a4decf33e47c3d9ff2ba76d361d26186..c591ceb63ec5e69217d6bcb31a1948c14b91b0a9 100644 (file)
@@ -39,26 +39,25 @@ HISTORY
 INCLUDES
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
-#include "FGElectric.h"
-#include "models/FGPropulsion.h"
-#include "models/propulsion/FGThruster.h"
-
 #include <iostream>
 #include <sstream>
 
+#include "FGElectric.h"
+#include "FGPropeller.h"
+
 using namespace std;
 
 namespace JSBSim {
 
-static const char *IdSrc = "$Id: FGElectric.cpp,v 1.10 2011/03/10 01:35:25 dpculp Exp $";
+static const char *IdSrc = "$Id: FGElectric.cpp,v 1.13 2011/08/03 03:21:06 jberndt Exp $";
 static const char *IdHdr = ID_ELECTRIC;
 
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 CLASS IMPLEMENTATION
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
 
-FGElectric::FGElectric(FGFDMExec* exec, Element *el, int engine_number)
-  : FGEngine(exec, el, engine_number)
+FGElectric::FGElectric(FGFDMExec* exec, Element *el, int engine_number, struct FGEngine::Inputs& input)
+  : FGEngine(exec, el, engine_number, input)
 {
   string token;
 
@@ -66,11 +65,14 @@ FGElectric::FGElectric(FGFDMExec* exec, Element *el, int engine_number)
   PowerWatts = 745.7;
   hptowatts = 745.7;
 
-  dt = FDMExec->GetDeltaT();
-
   if (el->FindElement("power"))
     PowerWatts = el->FindElementValueAsNumberConvertTo("power","WATTS");
 
+  string property_name, base_property_name;
+  base_property_name = CreateIndexedPropertyName("propulsion/engine", EngineNumber);
+  property_name = base_property_name + "/power-hp";
+  PropertyManager->Tie(property_name, &HP);
+
   Debug(0); // Call Debug() routine from constructor if needed
 }
 
@@ -87,12 +89,16 @@ void FGElectric::Calculate(void)
 {
   RunPreFunctions();
 
-  Throttle = FCS->GetThrottlePos(EngineNumber);
+  if (Thruster->GetType() == FGThruster::ttPropeller) {
+    ((FGPropeller*)Thruster)->SetAdvance(in.PropAdvance[EngineNumber]);
+    ((FGPropeller*)Thruster)->SetFeather(in.PropFeather[EngineNumber]);
+  } 
 
   RPM = Thruster->GetRPM() * Thruster->GetGearRatio();
 
-  HP = PowerWatts * Throttle / hptowatts;
+  HP = PowerWatts * in.ThrottlePos[EngineNumber] / hptowatts;
   
+  LoadThrusterInputs();
   Thruster->Calculate(HP * hptoftlbssec);
 
   RunPostFunctions();