X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FAIModel%2FAIFlightPlanCreate.cxx;h=64df906f5fb51400a9848fd04f6da461a09d8b98;hb=acbcf94bde0ea73132a1dfadc0ebfd161d25f96d;hp=f30d44f70ee524a2f78698cc20cf7ec6534ee1fc;hpb=6e42458a5551c5d015f6058ca5b81a61b6e82049;p=flightgear.git

diff --git a/src/AIModel/AIFlightPlanCreate.cxx b/src/AIModel/AIFlightPlanCreate.cxx
index f30d44f70..64df906f5 100644
--- a/src/AIModel/AIFlightPlanCreate.cxx
+++ b/src/AIModel/AIFlightPlanCreate.cxx
@@ -373,13 +373,13 @@ void FGAIFlightPlan::createTakeOff(FGAIAircraft *ac, bool firstFlight, FGAirport
     double accel    = ac->getPerformance()->acceleration();
     double vTaxi    = ac->getPerformance()->vTaxi();
     double vRotate  = ac->getPerformance()->vRotate();
-    double vTakeoff = ac->getPerformance()->vTakeoff();
+//    double vTakeoff = ac->getPerformance()->vTakeoff();
     double vClimb   = ac->getPerformance()->vClimb();
     // Acceleration = dV / dT
     // Acceleration X dT = dV
     // dT = dT / Acceleration
     //d = (Vf^2 - Vo^2) / (2*a)
-    double accelTime = (vRotate - vTaxi) / accel;
+//    double accelTime = (vRotate - vTaxi) / accel;
     //cerr << "Using " << accelTime << " as total acceleration time" << endl;
     double accelDistance = (vRotate*vRotate - vTaxi*vTaxi) / (2*accel);
     //cerr << "Using " << accelDistance << " " << accel << " " << vRotate << endl;
@@ -430,7 +430,7 @@ void FGAIFlightPlan::createTakeOff(FGAIAircraft *ac, bool firstFlight, FGAirport
 void FGAIFlightPlan::createClimb(FGAIAircraft *ac, bool firstFlight, FGAirport *apt, double speed, double alt, const string &fltType)
 {
   waypoint *wpt;
-  bool planLoaded = false;
+//  bool planLoaded = false;
   string fPLName;
   double vClimb   = ac->getPerformance()->vClimb();
 
@@ -529,10 +529,10 @@ void FGAIFlightPlan::createParking(FGAIAircraft *ac, FGAirport *apt, double radi
 {
   waypoint* wpt;
   double aptElev = apt->getElevation();
-  double lat, lat2;
-  double lon, lon2;
-  double az2;
-  double heading;
+  double lat = 0.0, lat2 = 0.0;
+  double lon = 0.0, lon2 = 0.0;
+  double az2 = 0.0;
+  double heading = 0.0;
 
   double vTaxi        = ac->getPerformance()->vTaxi();
   double vTaxiReduced = vTaxi * (2.0/3.0);