fly/flightgear
1
0
Fork 0
Code Activity

cleanup: extract globals->get_controls()

Browse source
This commit is contained in:
mfranz 2007-07-29 17:36:30 +00:00
parent 2bcf5b7fe7
commit d1fb32b315
2 changed files with 13 additions and 14 deletions
Show stats Download patch file Download diff file Expand all files Collapse all files

25
src/FDM/UFO.cxx
View file

@ -73,34 +73,33 @@ void FGUFO::init() {
// Run an iteration of the EOM (equations of motion)
void FGUFO::update( double dt ) {
// cout << "FGLaRCsim::update()" << endl;
if (is_suspended())
return;
lowpass::set_delta(dt);
double time_step = dt;
FGControls *ctrl = globals->get_controls();
// read the throttle
double throttle = globals->get_controls()->get_throttle( 0 );
double brake_left = globals->get_controls()->get_brake_left();
double brake_right = globals->get_controls()->get_brake_right();
double throttle = ctrl->get_throttle( 0 );
double brake_left = ctrl->get_brake_left();
double brake_right = ctrl->get_brake_right();
if (brake_left > 0.5 || brake_right > 0.5)
throttle = -throttle;
throttle = Throttle->filter(throttle);
double velocity = Throttle->filter(throttle) * Speed_Max->getDoubleValue(); // meters/sec
// read and lowpass-filter the state of the control surfaces
double aileron = Aileron->filter(globals->get_controls()->get_aileron());
double elevator = Elevator->filter(globals->get_controls()->get_elevator());
double rudder = Rudder->filter(globals->get_controls()->get_rudder());
double aileron = Aileron->filter(ctrl->get_aileron());
double elevator = Elevator->filter(ctrl->get_elevator());
double rudder = Rudder->filter(ctrl->get_rudder());
aileron += Aileron_Trim->filter(globals->get_controls()->get_aileron_trim());
elevator += Elevator_Trim->filter(globals->get_controls()->get_elevator_trim());
rudder += Rudder_Trim->filter(globals->get_controls()->get_rudder_trim());
double velocity = throttle * Speed_Max->getDoubleValue(); // meters/sec
aileron += Aileron_Trim->filter(ctrl->get_aileron_trim());
elevator += Elevator_Trim->filter(ctrl->get_elevator_trim());
rudder += Rudder_Trim->filter(ctrl->get_rudder_trim());
double old_pitch = get_Theta();
double pitch_rate = SGD_PI_4; // assume I will be pitching up