Fix stall widths for the "auxilliary" (reverse flow) stalls so they

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

diff --git a/src/FDM/YASim/ControlMap.cpp b/src/FDM/YASim/ControlMap.cpp
index fd4f99b7ca6f7f13ab62965f3adf8f9fe85ba7c7..cd7174cc5545f3ec7b86fd27398052933d6e0ff5 100644 (file)
--- a/src/FDM/YASim/ControlMap.cpp
+++ b/src/FDM/YASim/ControlMap.cpp
@@ -2,7 +2,10 @@
 #include "Thruster.hpp"
 #include "PropEngine.hpp"
 #include "PistonEngine.hpp"
+#include "TurbineEngine.hpp"
 #include "Gear.hpp"
+#include "Hook.hpp"
+#include "Launchbar.hpp"
 #include "Wing.hpp"
 #include "Rotor.hpp"
 #include "Math.hpp"
@@ -186,26 +189,31 @@ void ControlMap::applyControls(float dt)
        switch(o->type) {
        case THROTTLE: ((Thruster*)obj)->setThrottle(lval);        break;
        case MIXTURE:  ((Thruster*)obj)->setMixture(lval);         break;
+        case CONDLEVER: ((TurbineEngine*)((PropEngine*)obj)->getEngine())->setCondLever(lval); break;
        case STARTER:  ((Thruster*)obj)->setStarter(lval != 0.0);  break;
        case MAGNETOS: ((PropEngine*)obj)->setMagnetos((int)lval); break;
        case ADVANCE:  ((PropEngine*)obj)->setAdvance(lval);       break;
-        case PROPPITCH: ((PropEngine*)obj)->setPropPitch(lval); break;
+        case PROPPITCH: ((PropEngine*)obj)->setPropPitch(lval);    break;
+        case PROPFEATHER: ((PropEngine*)obj)->setPropFeather((int)lval); break;
        case REHEAT:   ((Jet*)obj)->setReheat(lval);               break;
        case VECTOR:   ((Jet*)obj)->setRotation(lval);             break;
        case BRAKE:    ((Gear*)obj)->setBrake(lval);               break;
        case STEER:    ((Gear*)obj)->setRotation(lval);            break;
        case EXTEND:   ((Gear*)obj)->setExtension(lval);           break;
+       case HEXTEND:  ((Hook*)obj)->setExtension(lval);           break;
+       case LEXTEND:  ((Launchbar*)obj)->setExtension(lval);      break;
        case CASTERING:((Gear*)obj)->setCastering(lval != 0);      break;
        case SLAT:     ((Wing*)obj)->setSlat(lval);                break;
        case FLAP0:    ((Wing*)obj)->setFlap0(lval, rval);         break;
        case FLAP1:    ((Wing*)obj)->setFlap1(lval, rval);         break;
        case SPOILER:  ((Wing*)obj)->setSpoiler(lval, rval);       break;
-        case COLLECTIVE:   ((Rotor*)obj)->setCollective(lval);        break;
-        case CYCLICAIL:    ((Rotor*)obj)->setCyclicail(lval,rval);         break;
-        case CYCLICELE:    ((Rotor*)obj)->setCyclicele(lval,rval);         break;
+        case COLLECTIVE:   ((Rotor*)obj)->setCollective(lval);     break;
+        case CYCLICAIL:    ((Rotor*)obj)->setCyclicail(lval,rval); break;
+        case CYCLICELE:    ((Rotor*)obj)->setCyclicele(lval,rval); break;
         case ROTORENGINEON: ((Rotor*)obj)->setEngineOn((int)lval); break;
+       case REVERSE_THRUST: ((Jet*)obj)->setReverse(lval != 0);   break;
        case BOOST:
-           ((Thruster*)obj)->getPistonEngine()->setBoost(lval);
+           ((PistonEngine*)((Thruster*)obj)->getEngine())->setBoost(lval);
            break;
        }
     }