X-Git-Url: https://git.mxchange.org/?a=blobdiff_plain;f=src%2FFDM%2FUFO.cxx;h=ca9b773a7dee5b407bebadeb93b0527e5943cbb0;hb=ee98995d30e75cda88c9866f3cb6a761fda7d078;hp=efa296d82af2000e5310e152a1c9c72b432a915d;hpb=907e2942bb25f1f0146312ef25c897f5c0661e16;p=flightgear.git

diff --git a/src/FDM/UFO.cxx b/src/FDM/UFO.cxx
index efa296d82..ca9b773a7 100644
--- a/src/FDM/UFO.cxx
+++ b/src/FDM/UFO.cxx
@@ -31,16 +31,16 @@
 
 #include "UFO.hxx"
 
-const double throttle_damp = 0.05;
-const double aileron_damp = 0.01;
-const double elevator_damp = 0.01;
+const double throttle_damp = 0.2;
+const double aileron_damp = 0.05;
+const double elevator_damp = 0.05;
 
 FGUFO::FGUFO( double dt )
   : Throttle(0.0),
     Aileron(0.0),
     Elevator(0.0)
 {
-    set_delta_t( dt );
+//     set_delta_t( dt );
 }
 
 
@@ -56,10 +56,15 @@ void FGUFO::init() {
 
 
 // Run an iteration of the EOM (equations of motion)
-void FGUFO::update( int multiloop ) {
+void FGUFO::update( double dt ) {
     // cout << "FGLaRCsim::update()" << endl;
 
-    double time_step = get_delta_t() * multiloop;
+    if (is_suspended())
+      return;
+
+    int multiloop = _calc_multiloop(dt);
+
+    double time_step = dt;
 
     // read the throttle
     double th = globals->get_controls()->get_throttle( 0 );