X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FYASim%2FPropeller.cpp;h=af19e705088467c79f54d15a7c72d3797f10562d;hb=d66903e9ad63b91182ccc25d9bb82f18f8dd98b6;hp=661a3842edff1c3d9fdef29a5ae9581295768009;hpb=2aaa1803d3d4d01ef6036561fb1338a0402751f2;p=flightgear.git

diff --git a/src/FDM/YASim/Propeller.cpp b/src/FDM/YASim/Propeller.cpp
index 661a3842e..af19e7050 100644
--- a/src/FDM/YASim/Propeller.cpp
+++ b/src/FDM/YASim/Propeller.cpp
@@ -24,6 +24,7 @@ Propeller::Propeller(float radius, float v, float omega,
     _matchTakeoff = false;
     _manual = false;
     _proppitch = 0;
+    _propfeather = 0;
 }
 
 void Propeller::setTakeoff(float omega0, float power0)
@@ -36,12 +37,18 @@ void Propeller::setTakeoff(float omega0, float power0)
     float density = Atmosphere::getStdDensity(0);
     _tc0 = (torque * gamma) / (0.5f * density * V2 * _f0);
 }
+
+void Propeller::setStops(float fine_stop, float coarse_stop)
+{
+    _fine_stop = fine_stop;
+    _coarse_stop = coarse_stop;
+}
     
 void Propeller::modPitch(float mod)
 {
     _j0 *= mod;
-    if(_j0 < 0.25f*_baseJ0) _j0 = 0.25f*_baseJ0;
-    if(_j0 > 4*_baseJ0)     _j0 = 4*_baseJ0;
+    if(_j0 < _fine_stop*_baseJ0) _j0 = _fine_stop*_baseJ0;
+    if(_j0 > _coarse_stop*_baseJ0)     _j0 = _coarse_stop*_baseJ0;
 }
 
 void Propeller::setManualPitch()
@@ -55,12 +62,19 @@ void Propeller::setPropPitch(float proppitch)
     _proppitch = Math::clamp(proppitch, 0, 1);
 }
 
+void Propeller::setPropFeather(int state)
+{
+    // 0 = normal, 1 = feathered
+    _propfeather = (state != 0);
+}
+
 void Propeller::calc(float density, float v, float omega,
 		     float* thrustOut, float* torqueOut)
 {
     // For manual pitch, exponentially modulate the J0 value between
     // 0.25 and 4.  A prop pitch of 0.5 results in no change from the
     // base value.
+    // TODO: integrate with _fine_stop and _coarse_stop variables
     if (_manual) 
         _j0 = _baseJ0 * Math::pow(2, 2 - 4*_proppitch);