mirror of https://github.com/ArduPilot/ardupilot
autotest: nicer display of key data in Rascal
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@ -123,16 +123,17 @@ dynamics model, and external 3D model.
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<script>
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setlistener("/sim/signals/fdm-initialized", func {
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var left = screen.display.new(20, 10);
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left.add("/surface-positions/right-aileron-pos-norm");
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left.add("/surface-positions/elevator-pos-norm");
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left.add("/surface-positions/rudder-pos-norm");
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left.add("/engines/engine/rpm");
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left.add("/apm/aileron");
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left.add("/apm/elevator");
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left.add("/apm/rudder");
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left.add("/apm/throttle");
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var right = screen.display.new(-250, 20);
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right.add("/orientation/pitch-deg");
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right.add("/orientation/roll-deg");
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right.add("/position/altitude-agl-ft");
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right.add("/velocities/airspeed-kt");
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right.add("/apm/pitch");
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right.add("/apm/roll");
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right.add("/apm/altitude");
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right.add("/apm/heading");
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right.add("/apm/airspeed");
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});
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</script>
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</rascal>
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@ -38,3 +38,32 @@ var update_airdata = func( dt ) {
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setprop("/accelerations/airspeed-ktps", accel_filt);
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}
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round10 = func(v) {
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if (v == nil) return 0;
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return 0.1*int(v*10);
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}
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round100 = func(v) {
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if (v == nil) return 0;
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return 0.01*int(v*100);
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}
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var update_vars = func( dt ) {
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asl_ft = getprop("/position/altitude-ft");
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ground = getprop("/position/ground-elev-ft");
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agl_m = (asl_ft - ground) * 0.3048;
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setprop("/apm/altitude", round10(agl_m));
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setprop("/apm/pitch", round10(getprop("/orientation/pitch-deg")));
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setprop("/apm/roll", round10(getprop("/orientation/roll-deg")));
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setprop("/apm/heading", round10(getprop("/orientation/heading-deg")));
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setprop("/apm/aileron", round100(getprop("/surface-positions/right-aileron-pos-norm")));
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setprop("/apm/elevator", round100(getprop("/surface-positions/elevator-pos-norm")));
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setprop("/apm/rudder", round100(getprop("/surface-positions/rudder-pos-norm")));
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setprop("/apm/throttle", round10(getprop("/engines/engine/rpm")));
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# airspeed-kt is actually in feet per second (FDM NET bug)
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setprop("/apm/airspeed", round10(0.3048*getprop("/velocities/airspeed-kt")));
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}
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@ -10,6 +10,7 @@ var main_loop = func {
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last_time = time;
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update_airdata( dt );
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update_vars( dt );
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update_ugear( dt );
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settimer(main_loop, 0);
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