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

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

diff --git a/src/FDM/JSBSim/FGTrim.cpp b/src/FDM/JSBSim/FGTrim.cpp
index 4b7313d26031c2bcfdb4e768b9794880be2fa10f..a4921e277a72fa07260f1a20de4656a0e44782d1 100644 (file)
--- a/src/FDM/JSBSim/FGTrim.cpp
+++ b/src/FDM/JSBSim/FGTrim.cpp
@@ -554,7 +554,7 @@ bool FGTrim::checkLimits(void) {
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
 void FGTrim::setupPullup() {
-  float g,q,cgamma;
+  double g,q,cgamma;
   g=fdmex->GetInertial()->gravity();
   cgamma=cos(fgic->GetFlightPathAngleRadIC());
   cout << "setPitchRateInPullup():  " << g << ", " << cgamma << ", "
@@ -601,7 +601,7 @@ void FGTrim::updateRates(void){
     fgic->SetQRadpsIC(q);
     fgic->SetRRadpsIC(r);
   } else if( mode == tPullup && fabs(targetNlf-1) > 0.01) {
-      float g,q,cgamma;
+      double g,q,cgamma;
       g=fdmex->GetInertial()->gravity();
       cgamma=cos(fgic->GetFlightPathAngleRadIC());
       q=g*(targetNlf-cgamma)/fgic->GetVtrueFpsIC();