1004 lines
No EOL
36 KiB
Text
1004 lines
No EOL
36 KiB
Text
# A3XX FMGC/Autoflight
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# Joshua Davidson (Octal450) and Jonathan Redpath (legoboyvdlp)
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# Copyright (c) 2020 Josh Davidson (Octal450) and Matthew Maring (mattmaring)
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##################
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# Init Functions #
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##################
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var database1 = 0;
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var database2 = 0;
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var code1 = 0;
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var code2 = 0;
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var gear0 = 0;
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var state1 = 0;
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var state2 = 0;
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var flaps = 0;
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var dep = "";
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var arr = "";
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var n1_left = 0;
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var n1_right = 0;
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var flaps = 0;
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var modelat = 0;
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var mode = 0;
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var modeI = 0;
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var gs = 0;
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var alt = 0;
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var aglalt = 0;
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var cruiseft = 0;
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var cruiseft_b = 0;
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var newcruise = 0;
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var phase = 0;
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var state1 = 0;
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var state2 = 0;
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var wowl = 0;
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var wowr = 0;
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var targetalt = 0;
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var targetvs = 0;
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var targetfpa = 0;
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var accel_agl_ft = 0;
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var locarm = 0;
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var apprarm = 0;
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var gear0 = 0;
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var fd1 = 0;
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var fd2 = 0;
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var spd = 0;
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var hdg = 0;
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var alt = 0;
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var altitude = 0;
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var flap = 0;
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var freqnav0uf = 0;
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var freqnav0 = 0;
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var namenav0 = "XX";
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var freqnav1uf = 0;
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var freqnav1 = 0;
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var namenav1 = "XX";
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var freqnav2uf = 0;
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var freqnav2 = 0;
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var namenav2 = "XX";
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var freqnav3uf = 0;
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var freqnav3 = 0;
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var namenav3 = "XX";
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var freqadf0uf = 0;
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var freqadf0 = 0;
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var nameadf0 = "XX";
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var freqadf1uf = 0;
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var freqadf1 = 0;
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var nameadf1 = "XX";
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var ias = 0;
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var mach = 0;
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var ktsmach = 0;
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var mngktsmach = 0;
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var mng_spd = 0;
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var mng_spd_cmd = 0;
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var kts_sel = 0;
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var mach_sel = 0;
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var srsSPD = 0;
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var maxspeed = 0;
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var minspeed = 0;
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var mach_switchover = 0;
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var decel = 0;
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var mng_alt_spd_cmd = 0;
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var mng_alt_spd = 0;
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var mng_alt_mach_cmd = 0;
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var mng_alt_mach = 0;
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var mng_spd_cmd = 0;
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var mng_spd = 0;
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var ap1 = 0;
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var ap2 = 0;
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var flx = 0;
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var lat = 0;
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var newlat = 0;
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var vert = 0;
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var newvert = 0;
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var newvertarm = 0;
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var thr1 = 0;
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var thr2 = 0;
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var altsel = 0;
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var crzFl = 0;
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setprop("/FMGC/internal/maxspeed", 0);
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setprop("/FMGC/internal/minspeed", 0);
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setprop("position/gear-agl-ft", 0);
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setprop("/FMGC/internal/mng-spd", 157);
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setprop("/FMGC/internal/mng-spd-cmd", 157);
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setprop("/FMGC/internal/mng-kts-mach", 0);
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setprop("/FMGC/internal/mach-switchover", 0);
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setprop("it-autoflight/settings/accel-agl-ft", 1500); #eventually set to 1500 above runway
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setprop("it-autoflight/internal/vert-speed-fpm", 0);
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setprop("it-autoflight/output/fma-pwr", 0);
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setprop("instrumentation/nav[0]/nav-id", "XXX");
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setprop("instrumentation/nav[1]/nav-id", "XXX");
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setprop("/FMGC/internal/ils1-mcdu", "XXX/999.99");
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setprop("/FMGC/internal/ils2-mcdu", "XXX/999.99");
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setprop("/FMGC/internal/vor1-mcdu", "XXX/999.99");
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setprop("/FMGC/internal/vor2-mcdu", "999.99/XXX");
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setprop("/FMGC/internal/adf1-mcdu", "XXX/999.99");
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setprop("/FMGC/internal/adf2-mcdu", "999.99/XXX");
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setprop("gear/gear[0]/wow-fmgc", 1);
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var FMGCinit = func {
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setprop("/FMGC/status/to-state", 0);
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setprop("/FMGC/status/phase", "0"); # 0 is Preflight 1 is Takeoff 2 is Climb 3 is Cruise 4 is Descent 5 is Decel/Approach 6 is Go Around 7 is Done
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setprop("/FMGC/internal/maxspeed", 338);
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setprop("/FMGC/internal/mng-spd", 157);
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setprop("/FMGC/internal/mng-spd-cmd", 157);
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setprop("/FMGC/internal/mng-kts-mach", 0);
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setprop("/FMGC/internal/mach-switchover", 0);
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setprop("it-autoflight/settings/accel-agl-ft", 1500); #eventually set to 1500 above runway
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setprop("/FMGC/internal/decel", 0);
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setprop("/FMGC/internal/loc-source", "NAV0");
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setprop("/FMGC/internal/optalt", 0);
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setprop("/FMGC/internal/landing-time", -99);
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setprop("/FMGC/internal/align1-time", -99);
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setprop("/FMGC/internal/align2-time", -99);
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setprop("/FMGC/internal/align3-time", -99);
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setprop("/FMGC/internal/block-fuel-time", -99);
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setprop("/FMGC/internal/fuel-pred-time", -99);
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masterFMGC.start();
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various.start();
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various2.start();
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}
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############
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# FBW Trim #
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############
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setlistener("/gear/gear[0]/wow-fmgc", func {
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trimReset();
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});
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var trimReset = func {
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gear0 = getprop("/gear/gear[0]/wow");
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flaps = getprop("/controls/flight/flap-pos");
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if (gear0 == 1 and getprop("/FMGC/status/to-state") == 0 and (flaps >= 5 or (flaps >= 4 and getprop("/instrumentation/mk-viii/inputs/discretes/momentary-flap3-override") == 1))) {
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interpolate("/controls/flight/elevator-trim", 0.0, 1.5);
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}
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}
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###############
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# MCDU Inputs #
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###############
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var updateARPT = func {
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dep = getprop("/FMGC/internal/dep-arpt");
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arr = getprop("/FMGC/internal/arr-arpt");
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alt = getprop("/FMGC/internal/alt-airport");
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setprop("autopilot/route-manager/departure/airport", dep);
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setprop("autopilot/route-manager/destination/airport", arr);
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setprop("autopilot/route-manager/alternate/airport", alt);
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if (getprop("/autopilot/route-manager/active") != 1) {
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fgcommand("activate-flightplan", props.Node.new({"activate": 1}));
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}
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}
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setlistener("/FMGC/internal/cruise-ft", func {
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setprop("autopilot/route-manager/cruise/altitude-ft", getprop("/FMGC/internal/cruise-ft"));
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});
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########
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# FUEL #
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########
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var updateFuel = func {
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# Check engine status
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if (num(getprop("/engines/engine[0]/n1-actual")) > 0 or num(getprop("/engines/engine[1]/n1-actual")) > 0) {
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setprop("/FMGC/internal/block", sprintf("%3.1f", math.round(getprop("/consumables/fuel/total-fuel-lbs") / 1000, 0.1)));
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}
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# Calculate (final) holding fuel
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if (!getprop("/FMGC/internal/final-fuel-set") and getprop("/FMGC/internal/tofrom-set")) {
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#calc
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} else if (!getprop("/FMGC/internal/final-fuel-set")) {
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setprop("/FMGC/internal/final-fuel", 0.0); # need to calculate 30 min of fuel
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}
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if (!getprop("/FMGC/internal/final-fuel-set") and getprop("/FMGC/internal/tofrom-set")) {
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#calc
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} else if (!getprop("/FMGC/internal/final-fuel-set")) {
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setprop("/FMGC/internal/final-time", "0030");
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}
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# Calculate alternate fuel
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if (!getprop("/FMGC/internal/alt-fuel-set") and getprop("/FMGC/internal/alt-set")) {
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#calc
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} else if (!getprop("/FMGC/internal/alt-fuel-set")) {
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setprop("/FMGC/internal/alt-fuel", 0.0);
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setprop("/FMGC/internal/alt-time", "0000");
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}
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# Calculate min dest fob (final + alternate)
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if (!getprop("/FMGC/internal/min-dest-fob-set")) {
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setprop("/FMGC/internal/min-dest-fob", num(getprop("/FMGC/internal/alt-fuel") + getprop("/FMGC/internal/final-fuel")));
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}
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# Calculate trip fuel
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if (!getprop("/FMGC/internal/trip-fuel-set") and getprop("/FMGC/internal/tofrom-set")) {
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#calc
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} else if (!getprop("/FMGC/internal/trip-fuel-set")) {
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setprop("/FMGC/internal/trip-fuel", 0.0);
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}
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if (!getprop("/FMGC/internal/trip-fuel-set") and getprop("/FMGC/internal/tofrom-set")) {
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#calc
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} else if (!getprop("/FMGC/internal/trip-fuel-set")) {
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setprop("/FMGC/internal/trip-time", "0000");
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}
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# Calculate taxi fuel
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setprop("/FMGC/internal/tow", num(getprop("/FMGC/internal/block") + getprop("/FMGC/internal/zfw") - getprop("/FMGC/internal/taxi-fuel")));
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setprop("/FMGC/internal/lw", num(getprop("/FMGC/internal/tow") - getprop("/FMGC/internal/trip-fuel")));
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# Calculate reserve fuel
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if (getprop("/FMGC/internal/rte-rsv-set")) {
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if (num(getprop("/FMGC/internal/trip-fuel")) == 0.0) {
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setprop("/FMGC/internal/rte-percent", 0.0);
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} else {
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setprop("/FMGC/internal/rte-percent", num(getprop("/FMGC/internal/rte-rsv") / getprop("/FMGC/internal/trip-fuel") * 100.0));
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}
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} else if (getprop("/FMGC/internal/rte-percent-set")) {
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setprop("/FMGC/internal/rte-rsv", num(getprop("/FMGC/internal/trip-fuel") * (100.0 - getprop("/FMGC/internal/rte-percent")) / 100.0));
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} else {
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if (num(getprop("/FMGC/internal/trip-fuel")) == 0.0) {
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setprop("/FMGC/internal/rte-percent", 5.0);
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} else {
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setprop("/FMGC/internal/rte-percent", num(getprop("/FMGC/internal/rte-rsv") / getprop("/FMGC/internal/trip-fuel") * 100.0));
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}
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}
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# Calcualte extra fuel
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setprop("/FMGC/internal/extra-fuel", num(getprop("/FMGC/internal/block") - getprop("/FMGC/internal/trip-fuel") - getprop("/FMGC/internal/min-dest-fob") - getprop("/FMGC/internal/taxi-fuel") - getprop("/FMGC/internal/rte-rsv")));
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}
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############################
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# Flight Phase and Various #
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############################
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var masterFMGC = maketimer(0.2, func {
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n1_left = getprop("/engines/engine[0]/n1-actual");
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n1_right = getprop("/engines/engine[1]/n1-actual");
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flaps = getprop("/controls/flight/flap-pos");
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modelat = getprop("/modes/pfd/fma/roll-mode");
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mode = getprop("/modes/pfd/fma/pitch-mode");
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modeI = getprop("/it-autoflight/mode/vert");
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gs = getprop("/velocities/groundspeed-kt");
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alt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
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aglalt = pts.Position.gearAglFt.getValue();
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cruiseft = getprop("/FMGC/internal/cruise-ft");
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cruiseft_b = getprop("/FMGC/internal/cruise-ft") - 200;
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newcruise = getprop("/it-autoflight/internal/alt");
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phase = getprop("/FMGC/status/phase");
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state1 = getprop("/systems/thrust/state1");
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state2 = getprop("/systems/thrust/state2");
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gear0 = getprop("/gear/gear[0]/wow");
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wowl = getprop("/gear/gear[1]/wow");
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wowr = getprop("/gear/gear[2]/wow");
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targetalt = getprop("/it-autoflight/internal/alt");
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targetvs = getprop("/it-autoflight/input/vs");
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targetfpa = getprop("/it-autoflight/input/fpa");
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accel_agl_ft = getprop("/it-autoflight/settings/accel-agl-ft");
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locarm = getprop("/it-autopilot/output/loc-armed");
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apprarm = getprop("/it-autopilot/output/appr-armed");
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gear0 = getprop("/gear/gear[0]/wow");
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ap1 = getprop("/it-autoflight/output/ap1");
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ap2 = getprop("/it-autoflight/output/ap2");
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flx = getprop("/systems/thrust/lim-flex");
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lat = getprop("/it-autoflight/mode/lat");
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newlat = getprop("/modes/pfd/fma/roll-mode");
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vert = getprop("/it-autoflight/mode/vert");
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newvert = getprop("/modes/pfd/fma/pitch-mode");
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newvertarm = getprop("/modes/pfd/fma/pitch-mode2-armed");
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thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
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thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
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altSel = getprop("/it-autoflight/input/alt");
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crzFl = getprop("/FMGC/internal/cruise-fl");
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if (getprop("/gear/gear[0]/wow") != getprop("/gear/gear[0]/wow-fmgc")) {
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setprop("gear/gear[0]/wow-fmgc", getprop("/gear/gear[0]/wow"));
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}
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if ((n1_left < 85 or n1_right < 85) and gs < 90 and mode == " " and gear0 == 1 and phase == 1) { # rejected takeoff
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setprop("/FMGC/status/phase", 0);
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setprop("systems/pressurization/mode", "GN");
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}
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if (gear0 == 1 and phase == 0 and ((n1_left >= 85 and n1_right >= 85 and mode == "SRS") or gs >= 90)) {
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setprop("/FMGC/status/phase", 1);
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setprop("systems/pressurization/mode", "TO");
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}
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if (phase == 1 and ((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
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setprop("/FMGC/status/phase", 2);
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setprop("systems/pressurization/mode", "TO");
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}
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if (phase == 2 and (mode == "ALT CRZ" or mode == "ALT CRZ*")) {
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setprop("/FMGC/status/phase", 3);
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setprop("systems/pressurization/mode", "CR");
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}
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if (crzFl >= 200) {
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if (phase == 3 and (flightPlanController.arrivalDist <= 200 or altSel < 20000)) {
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setprop("/FMGC/status/phase", 4);
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setprop("systems/pressurization/mode", "DE");
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}
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} else {
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if (phase == 3 and (flightPlanController.arrivalDist <= 200 or altSel < (crzFl * 100))) { # todo - not sure about crzFl condition, investigate what happens!
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setprop("/FMGC/status/phase", 4);
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setprop("systems/pressurization/mode", "DE");
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}
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}
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if (phase == 4 and getprop("/FMGC/internal/decel")) {
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setprop("/FMGC/status/phase", 5);
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}
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if (flightPlanController.num[2].getValue() > 0 and getprop("/FMGC/flightplan[2]/active") == 1 and flightPlanController.arrivalDist <= 15 and (modelat == "NAV" or modelat == "LOC" or modelat == "LOC*") and aglalt < 9500) { #todo decel pseudo waypoint
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setprop("/FMGC/internal/decel", 1);
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} else if (getprop("/FMGC/internal/decel") == 1 and (phase == 0 or phase == 6)) {
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setprop("/FMGC/internal/decel", 0);
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}
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if ((phase == "5") and state1 == "TOGA" and state2 == "TOGA") {
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setprop("/FMGC/status/phase", 6);
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setprop("systems/pressurization/mode", "TO");
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setprop("it-autoflight/input/toga", 1);
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}
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if (phase == "6" and alt >= accel_agl_ft) { # todo when insert altn or new dest
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setprop("/FMGC/status/phase", 2);
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}
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if (getprop("/systems/navigation/adr/computation/overspeed-vfe-spd") != 1024) {
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setprop("/FMGC/internal/maxspeed", getprop("/systems/navigation/adr/computation/overspeed-vfe-spd") - 4);
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} elsif (pts.Gear.position[0].getValue() != 0 or pts.Gear.position[1].getValue() != 0 or pts.Gear.position[2].getValue() != 0) {
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setprop("/FMGC/internal/maxspeed", 284);
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} else {
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setprop("/FMGC/internal/maxspeed", getprop("/it-fbw/speeds/vmo-mmo"));
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}
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# calculate speeds
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flap = getprop("/controls/flight/flap-pos");
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weight_lbs = getprop("/fdm/jsbsim/inertia/weight-lbs") / 1000;
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tow = getprop("/FMGC/internal/tow");
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lw = getprop("/FMGC/internal/lw");
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altitude = getprop("/instrumentation/altimeter/indicated-altitude-ft");
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dest_wind = getprop("/FMGC/internal/dest-wind");
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# current appr speeds
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clean = 2 * weight_lbs * 0.45359237 + 85;
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if (altitude > 20000) {
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clean += (altitude - 20000) / 1000;
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}
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vs1g_clean = 0.0024 * weight_lbs * weight_lbs + 0.124 * weight_lbs + 88.942;
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vs1g_conf_1 = -0.0007 * weight_lbs * weight_lbs + 0.6795 * weight_lbs + 44.673;
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vs1g_conf_1f = -0.0001 * weight_lbs * weight_lbs + 0.5211 * weight_lbs + 49.027;
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vs1g_conf_2 = -0.0005 * weight_lbs * weight_lbs + 0.5488 * weight_lbs + 44.279;
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vs1g_conf_3 = -0.0005 * weight_lbs * weight_lbs + 0.5488 * weight_lbs + 43.279;
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vs1g_conf_full = -0.0007 * weight_lbs * weight_lbs + 0.6002 * weight_lbs + 38.479;
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slat = vs1g_clean * 1.23;
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flap2 = vs1g_conf_2 * 1.47;
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flap3 = vs1g_conf_3 * 1.36;
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if (getprop("/FMGC/internal/ldg-config-3-set")) {
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vls = vs1g_conf_3 * 1.23;
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} else {
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vls = vs1g_conf_full * 1.23
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}
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if (vls < 113) {
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vls = 113;
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}
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if (!getprop("/FMGC/internal/vapp-speed-set")) {
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if (dest_wind < 5) {
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vapp = vls + 5;
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} else if (dest_wind > 15) {
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vapp = vls + 15;
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} else {
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vapp = vls + dest_wind;
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}
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setprop("/FMGC/internal/computed-speeds/vapp", vapp);
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}
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aoa_prot = 15;
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aoa_max = 17.5;
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aoa_0 = -5;
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aoa = getprop("/systems/navigation/adr/output/aoa-1");
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cas = getprop("/systems/navigation/adr/output/cas-1");
|
|
|
|
alpha_prot = cas * math.sqrt((aoa - aoa_0)/(aoa_prot - aoa_0));
|
|
alpha_max = cas * math.sqrt((aoa - aoa_0)/(aoa_max - aoa_0));
|
|
|
|
# predicted to speeds
|
|
clean_to = 2 * tow * 0.45359237 + 85;
|
|
if (altitude > 20000) {
|
|
clean_to += (altitude - 20000) / 1000;
|
|
}
|
|
vs1g_clean_to = 0.0024 * tow * tow + 0.124 * tow + 88.942;
|
|
vs1g_conf_2_to = -0.0005 * tow * tow + 0.5488 * tow + 44.279;
|
|
vs1g_conf_3_to = -0.0005 * tow * tow + 0.5488 * tow + 43.279;
|
|
vs1g_conf_full_to = -0.0007 * tow * tow + 0.6002 * tow + 38.479;
|
|
slat_to = vs1g_clean_to * 1.23;
|
|
flap2_to = vs1g_conf_2_to * 1.47;
|
|
|
|
# predicted appr speeds
|
|
clean_appr = 2 * lw * 0.45359237 + 85;
|
|
if (altitude > 20000) {
|
|
clean_appr += (altitude - 20000) / 1000;
|
|
}
|
|
vs1g_clean_appr = 0.0024 * lw * lw + 0.124 * lw + 88.942;
|
|
vs1g_conf_2_appr = -0.0005 * lw * lw + 0.5488 * lw + 44.279;
|
|
vs1g_conf_3_appr = -0.0005 * lw * lw + 0.5488 * lw + 43.279;
|
|
vs1g_conf_full_appr = -0.0007 * lw * lw + 0.6002 * lw + 38.479;
|
|
slat_appr = vs1g_clean_appr * 1.23;
|
|
flap2_appr = vs1g_conf_2_appr * 1.47;
|
|
|
|
if (getprop("/FMGC/internal/ldg-config-3-set")) {
|
|
vls_appr = vs1g_conf_3_appr * 1.23;
|
|
} else {
|
|
vls_appr = vs1g_conf_full_appr * 1.23
|
|
}
|
|
|
|
if (vls_appr < 113) {
|
|
vls_appr = 113;
|
|
}
|
|
|
|
if (!getprop("/FMGC/internal/vapp-speed-set")) {
|
|
if (dest_wind < 5) {
|
|
vapp_appr = vls_appr + 5;
|
|
} else if (dest_wind > 15) {
|
|
vapp_appr = vls_appr + 15;
|
|
} else {
|
|
vapp_appr = vls_appr + dest_wind;
|
|
}
|
|
setprop("/FMGC/internal/computed-speeds/vapp_appr", vapp_appr);
|
|
}
|
|
|
|
# set the values globally
|
|
setprop("/FMGC/internal/computed-speeds/clean", clean);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_clean", vs1g_clean);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_1", vs1g_conf_1);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_1f", vs1g_conf_1f);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_2", vs1g_conf_2);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_3", vs1g_conf_3);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_full", vs1g_conf_full);
|
|
setprop("/FMGC/internal/computed-speeds/slat", slat);
|
|
setprop("/FMGC/internal/computed-speeds/flap2", flap2);
|
|
setprop("/FMGC/internal/computed-speeds/flap3", flap3);
|
|
setprop("/FMGC/internal/computed-speeds/vls", vls);
|
|
setprop("/FMGC/internal/computed-speeds/alpha_prot", alpha_prot);
|
|
setprop("/FMGC/internal/computed-speeds/alpha_max", alpha_max);
|
|
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_clean_to", vs1g_clean_to);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_2_to", vs1g_conf_2_to);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_3_to", vs1g_conf_3_to);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_full_to", vs1g_conf_full_to);
|
|
setprop("/FMGC/internal/computed-speeds/slat_to", slat_to);
|
|
setprop("/FMGC/internal/computed-speeds/flap2_to", flap2_to);
|
|
setprop("/FMGC/internal/computed-speeds/clean_to", clean_to);
|
|
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_clean_appr", vs1g_clean_appr);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_2_appr", vs1g_conf_2_appr);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_3_appr", vs1g_conf_3_appr);
|
|
setprop("/FMGC/internal/computed-speeds/vs1g_conf_full_appr", vs1g_conf_full_appr);
|
|
setprop("/FMGC/internal/computed-speeds/slat_appr", slat_appr);
|
|
setprop("/FMGC/internal/computed-speeds/flap2_appr", flap2_appr);
|
|
setprop("/FMGC/internal/computed-speeds/clean_appr", clean_appr);
|
|
setprop("/FMGC/internal/computed-speeds/vls_appr", vls_appr);
|
|
|
|
# Need info on these, also correct for height at altitude...
|
|
# https://www.pprune.org/archive/index.php/t-587639.html
|
|
if (getprop("/FMGC/status/to-state") == 1) {
|
|
if (flap == 0) { # 0
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_clean * 1.28);
|
|
} else if (flap == 1) { # 1
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_conf_1 * 1.23);
|
|
} else { # 1+F
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_clean * 1.13);
|
|
}
|
|
} else {
|
|
if (flap == 0) { # 0
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_clean * 1.23);
|
|
} else if (flap == 1) { # 1
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_conf_1 * 1.23);
|
|
} else if (flap == 2) { # 1+F
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_conf_1f * 1.23);
|
|
} else if (flap == 3) { # 2
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_conf_2 * 1.23);
|
|
} else if (flap == 4) { # 3
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_conf_3 * 1.23);
|
|
} else if (flap == 5) { # FULL
|
|
setprop("/FMGC/internal/computed-speeds/vls_min", vs1g_conf_full * 1.23);
|
|
}
|
|
}
|
|
|
|
if (flap == 0) { # 0
|
|
setprop("/FMGC/internal/computed-speeds/vsw", vs1g_clean);
|
|
} else if (flap == 1) { # 1
|
|
setprop("/FMGC/internal/computed-speeds/vsw", vs1g_conf_1);
|
|
} else if (flap == 2) { # 1+F
|
|
setprop("/FMGC/internal/computed-speeds/vsw", vs1g_conf_1f);
|
|
} else if (flap == 3) { # 2
|
|
setprop("/FMGC/internal/computed-speeds/vsw", vs1g_conf_2);
|
|
} else if (flap == 4) { # 3
|
|
setprop("/FMGC/internal/computed-speeds/vsw", vs1g_conf_3);
|
|
} else if (flap == 5) { # FULL
|
|
setprop("/FMGC/internal/computed-speeds/vsw", vs1g_conf_full);
|
|
}
|
|
|
|
if (flap == 0) { # 0
|
|
setprop("/FMGC/internal/minspeed", clean);
|
|
} else if (flap == 1) { # 1
|
|
setprop("/FMGC/internal/minspeed", slat);
|
|
} else if (flap == 2) { # 1+F
|
|
setprop("/FMGC/internal/minspeed", slat);
|
|
} else if (flap == 3) { # 2
|
|
setprop("/FMGC/internal/minspeed", flap2);
|
|
} else if (flap == 4) { # 3
|
|
setprop("/FMGC/internal/minspeed", flap3);
|
|
} else if (flap == 5) { # FULL
|
|
setprop("/FMGC/internal/minspeed", vapp);
|
|
}
|
|
|
|
if (gear0 == 1 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA") and flaps < 5) {
|
|
setprop("/FMGC/status/to-state", 1);
|
|
}
|
|
if (pts.Position.gearAglFt.getValue() >= 55) {
|
|
setprop("/FMGC/status/to-state", 0);
|
|
}
|
|
|
|
#handle radios, runways, v1/vr/v2
|
|
departure_rwy = fmgc.flightPlanController.flightplans[2].departure_runway;
|
|
destination_rwy = fmgc.flightPlanController.flightplans[2].destination_runway;
|
|
if (destination_rwy != nil and phase >= 2) {
|
|
var airport = airportinfo(getprop("/FMGC/internal/arr-arpt"));
|
|
setprop("/FMGC/internal/ldg-elev", airport.elevation * M2FT); # eventually should be runway elevation
|
|
magnetic_hdg = geo.normdeg(destination_rwy.heading - getprop("/environment/magnetic-variation-deg"));
|
|
runway_ils = destination_rwy.ils_frequency_mhz;
|
|
if (runway_ils != nil and !getprop("/FMGC/internal/ils1freq-set") and !getprop("/FMGC/internal/ils1crs-set")) {
|
|
setprop("/FMGC/internal/ils1freq-calculated", runway_ils);
|
|
setprop("instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
|
|
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
|
|
} else if (runway_ils != nil and !getprop("/FMGC/internal/ils1freq-set")) {
|
|
setprop("/FMGC/internal/ils1freq-calculated", runway_ils);
|
|
setprop("instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
|
|
} else if (!getprop("/FMGC/internal/ils1crs-set")) {
|
|
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
|
|
}
|
|
} else if (departure_rwy != nil and phase <= 1) {
|
|
magnetic_hdg = geo.normdeg(departure_rwy.heading - getprop("/environment/magnetic-variation-deg"));
|
|
runway_ils = departure_rwy.ils_frequency_mhz;
|
|
if (runway_ils != nil and !getprop("/FMGC/internal/ils1freq-set") and !getprop("/FMGC/internal/ils1crs-set")) {
|
|
setprop("/FMGC/internal/ils1freq-calculated", runway_ils);
|
|
setprop("instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
|
|
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
|
|
} else if (runway_ils != nil and !getprop("/FMGC/internal/ils1freq-set")) {
|
|
setprop("/FMGC/internal/ils1freq-calculated", runway_ils);
|
|
setprop("instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
|
|
} else if (!getprop("/FMGC/internal/ils1crs-set")) {
|
|
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
|
|
}
|
|
}
|
|
});
|
|
|
|
var reset_FMGC = func {
|
|
setprop("/FMGC/status/phase", "0");
|
|
fd1 = getprop("/it-autoflight/input/fd1");
|
|
fd2 = getprop("/it-autoflight/input/fd2");
|
|
spd = getprop("/it-autoflight/input/spd-kts");
|
|
hdg = getprop("/it-autoflight/input/hdg");
|
|
alt = getprop("/it-autoflight/input/alt");
|
|
ITAF.init();
|
|
FMGCinit();
|
|
flightPlanController.reset();
|
|
mcdu.MCDU_reset(0);
|
|
mcdu.MCDU_reset(1);
|
|
setprop("it-autoflight/input/fd1", fd1);
|
|
setprop("it-autoflight/input/fd2", fd2);
|
|
setprop("it-autoflight/input/spd-kts", spd);
|
|
setprop("it-autoflight/input/hdg", hdg);
|
|
setprop("it-autoflight/input/alt", alt);
|
|
setprop("systems/pressurization/mode", "GN");
|
|
setprop("systems/pressurization/vs", "0");
|
|
setprop("systems/pressurization/targetvs", "0");
|
|
setprop("systems/pressurization/vs-norm", "0");
|
|
setprop("systems/pressurization/auto", 1);
|
|
setprop("systems/pressurization/deltap", "0");
|
|
setprop("systems/pressurization/outflowpos", "0");
|
|
setprop("systems/pressurization/deltap-norm", "0");
|
|
setprop("systems/pressurization/outflowpos-norm", "0");
|
|
altitude = getprop("/instrumentation/altimeter/indicated-altitude-ft");
|
|
setprop("systems/pressurization/cabinalt", altitude);
|
|
setprop("systems/pressurization/targetalt", altitude);
|
|
setprop("systems/pressurization/diff-to-target", "0");
|
|
setprop("systems/pressurization/ditchingpb", 0);
|
|
setprop("systems/pressurization/targetvs", "0");
|
|
setprop("systems/ventilation/cabin/fans", 0); # aircon fans
|
|
setprop("systems/ventilation/avionics/fan", 0);
|
|
setprop("systems/ventilation/avionics/extractvalve", "0");
|
|
setprop("systems/ventilation/avionics/inletvalve", "0");
|
|
setprop("systems/ventilation/lavatory/extractfan", 0);
|
|
setprop("systems/ventilation/lavatory/extractvalve", "0");
|
|
setprop("systems/pressurization/ambientpsi", "0");
|
|
setprop("systems/pressurization/cabinpsi", "0");
|
|
}
|
|
|
|
var various = maketimer(1, func {
|
|
if (getprop("/engines/engine[0]/state") == 3 and getprop("/engines/engine[1]/state") != 3) {
|
|
setprop("it-autoflight/settings/accel-agl-ft", getprop("/FMGC/internal/eng-out-reduc"));
|
|
} else if (getprop("/engines/engine[0]/state") != 3 and getprop("/engines/engine[1]/state") == 3) {
|
|
setprop("it-autoflight/settings/accel-agl-ft", getprop("/FMGC/internal/eng-out-reduc"));
|
|
} else {
|
|
setprop("it-autoflight/settings/accel-agl-ft", getprop("/FMGC/internal/accel-agl-ft"));
|
|
}
|
|
|
|
setprop("/FMGC/internal/gw", math.round(getprop("/fdm/jsbsim/inertia/weight-lbs"), 100));
|
|
});
|
|
|
|
var various2 = maketimer(0.5, func {
|
|
nav0();
|
|
nav1();
|
|
nav2();
|
|
nav3();
|
|
adf0();
|
|
adf1();
|
|
});
|
|
|
|
var nav0 = func {
|
|
var freqnav0uf = getprop("/instrumentation/nav[0]/frequencies/selected-mhz");
|
|
var freqnav0 = sprintf("%.2f", freqnav0uf);
|
|
var namenav0 = getprop("/instrumentation/nav[0]/nav-id");
|
|
if (freqnav0 >= 108.10 and freqnav0 <= 111.95) {
|
|
if (namenav0 != "") {
|
|
setprop("/FMGC/internal/ils1-mcdu", namenav0 ~ "/" ~ freqnav0);
|
|
} else {
|
|
setprop("/FMGC/internal/ils1-mcdu", freqnav0);
|
|
}
|
|
}
|
|
}
|
|
|
|
var nav1 = func {
|
|
var freqnav1uf = getprop("/instrumentation/nav[1]/frequencies/selected-mhz");
|
|
var freqnav1 = sprintf("%.2f", freqnav1uf);
|
|
var namenav1 = getprop("/instrumentation/nav[1]/nav-id");
|
|
if (freqnav1 >= 108.10 and freqnav1 <= 111.95) {
|
|
if (namenav1 != "") {
|
|
setprop("/FMGC/internal/ils2-mcdu", freqnav1 ~ "/" ~ namenav1);
|
|
} else {
|
|
setprop("/FMGC/internal/ils2-mcdu", freqnav1);
|
|
}
|
|
}
|
|
}
|
|
|
|
var nav2 = func {
|
|
var freqnav2uf = getprop("/instrumentation/nav[2]/frequencies/selected-mhz");
|
|
var freqnav2 = sprintf("%.2f", freqnav2uf);
|
|
var namenav2 = getprop("/instrumentation/nav[2]/nav-id");
|
|
if (freqnav2 >= 108.00 and freqnav2 <= 117.95) {
|
|
if (namenav2 != "") {
|
|
setprop("/FMGC/internal/vor1-mcdu", namenav2 ~ "/" ~ freqnav2);
|
|
} else {
|
|
setprop("/FMGC/internal/vor1-mcdu", freqnav2);
|
|
}
|
|
}
|
|
}
|
|
|
|
var nav3 = func {
|
|
var freqnav3uf = getprop("/instrumentation/nav[3]/frequencies/selected-mhz");
|
|
var freqnav3 = sprintf("%.2f", freqnav3uf);
|
|
var namenav3 = getprop("/instrumentation/nav[3]/nav-id");
|
|
if (freqnav3 >= 108.00 and freqnav3 <= 117.95) {
|
|
if (namenav3 != "") {
|
|
setprop("/FMGC/internal/vor2-mcdu", freqnav3 ~ "/" ~ namenav3);
|
|
} else {
|
|
setprop("/FMGC/internal/vor2-mcdu", freqnav3);
|
|
}
|
|
}
|
|
}
|
|
|
|
var adf0 = func {
|
|
var freqadf0uf = getprop("/instrumentation/adf[0]/frequencies/selected-khz");
|
|
var freqadf0 = sprintf("%.2f", freqadf0uf);
|
|
var nameadf0 = getprop("/instrumentation/adf[0]/ident");
|
|
if (freqadf0 >= 190 and freqadf0 <= 1750) {
|
|
if (nameadf0 != "") {
|
|
setprop("/FMGC/internal/adf1-mcdu", nameadf0 ~ "/" ~ freqadf0);
|
|
} else {
|
|
setprop("/FMGC/internal/adf1-mcdu", freqadf0);
|
|
}
|
|
}
|
|
}
|
|
|
|
var adf1 = func {
|
|
var freqadf1uf = getprop("/instrumentation/adf[1]/frequencies/selected-khz");
|
|
var freqadf1 = sprintf("%.2f", freqadf1uf);
|
|
var nameadf1 = getprop("/instrumentation/adf[1]/ident");
|
|
if (freqadf1 >= 190 and freqadf1 <= 1750) {
|
|
if (nameadf1 != "") {
|
|
setprop("/FMGC/internal/adf2-mcdu", freqadf1 ~ "/" ~ nameadf1);
|
|
} else {
|
|
setprop("/FMGC/internal/adf2-mcdu", freqadf1);
|
|
}
|
|
}
|
|
}
|
|
|
|
#################
|
|
# Managed Speed #
|
|
#################
|
|
|
|
var ManagedSPD = maketimer(0.25, func {
|
|
if (getprop("/FMGC/internal/cruise-lvl-set") == 1 and getprop("/FMGC/internal/cost-index-set") == 1) {
|
|
if (getprop("/it-autoflight/input/spd-managed") == 1) {
|
|
altitude = getprop("/instrumentation/altimeter/indicated-altitude-ft");
|
|
mode = getprop("/modes/pfd/fma/pitch-mode");
|
|
ias = getprop("/instrumentation/airspeed-indicator/indicated-speed-kt");
|
|
mach = getprop("/instrumentation/airspeed-indicator/indicated-mach");
|
|
ktsmach = getprop("/it-autoflight/input/kts-mach");
|
|
mngktsmach = getprop("/FMGC/internal/mng-kts-mach");
|
|
mng_spd = getprop("/FMGC/internal/mng-spd");
|
|
mng_spd_cmd = getprop("/FMGC/internal/mng-spd-cmd");
|
|
kts_sel = getprop("/it-autoflight/input/spd-kts");
|
|
mach_sel = getprop("/it-autoflight/input/spd-mach");
|
|
srsSPD = getprop("/it-autoflight/settings/togaspd");
|
|
phase = getprop("/FMGC/status/phase"); # 0 is Preflight 1 is Takeoff 2 is Climb 3 is Cruise 4 is Descent 5 is Decel/Approach 6 is Go Around 7 is Done
|
|
flap = getprop("/controls/flight/flap-pos");
|
|
maxspeed = getprop("/FMGC/internal/maxspeed");
|
|
minspeed = getprop("/FMGC/internal/minspeed");
|
|
mach_switchover = getprop("/FMGC/internal/mach-switchover");
|
|
decel = getprop("/FMGC/internal/decel");
|
|
|
|
mng_alt_spd_cmd = getprop("/FMGC/internal/mng-alt-spd");
|
|
mng_alt_spd = math.round(mng_alt_spd_cmd, 1);
|
|
|
|
mng_alt_mach_cmd = getprop("/FMGC/internal/mng-alt-mach");
|
|
mng_alt_mach = math.round(mng_alt_mach_cmd, 0.001);
|
|
|
|
if (mach > mng_alt_mach and (phase == 2 or phase == 3)) {
|
|
setprop("/FMGC/internal/mach-switchover", 1);
|
|
}
|
|
|
|
if (ias > mng_alt_spd and (phase == 4 or phase == 5)) {
|
|
setprop("/FMGC/internal/mach-switchover", 0);
|
|
}
|
|
|
|
if ((mode == " " or mode == "SRS") and (phase == 0 or phase == 1)) {
|
|
if (mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 0);
|
|
}
|
|
if (mng_spd_cmd != srsSPD) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", srsSPD);
|
|
}
|
|
} else if ((phase == 2 or phase == 3) and altitude <= 10050) {
|
|
if (mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 0);
|
|
}
|
|
if (mng_spd_cmd != 250 and !decel) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", 250);
|
|
} else if (mng_spd_cmd != minspeed and decel) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", minspeed);
|
|
}
|
|
} else if ((phase == 2 or phase == 3) and altitude > 10070 and !mach_switchover) {
|
|
if (mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 0);
|
|
}
|
|
if (mng_spd_cmd != mng_alt_spd) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
|
|
}
|
|
} else if ((phase == 2 or phase == 3) and altitude > 10070 and mach_switchover) {
|
|
if (!mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 1);
|
|
}
|
|
if (mng_spd_cmd != mng_alt_mach) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
|
|
}
|
|
} else if (phase == 4 and altitude > 11000 and !mach_switchover) {
|
|
if (mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 0);
|
|
}
|
|
if (mng_spd_cmd != mng_alt_spd) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
|
|
}
|
|
} else if (phase == 4 and altitude > 11000 and mach_switchover) {
|
|
if (!mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 1);
|
|
}
|
|
if (mng_spd_cmd != mng_alt_mach) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
|
|
}
|
|
} else if ((phase == 4 or phase == 5 or phase == 6) and altitude > 11000 and !mach_switchover) {
|
|
if (mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 0);
|
|
}
|
|
if (mng_spd_cmd != mng_alt_spd and !decel) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
|
|
} else if (mng_spd_cmd != minspeed and decel) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", minspeed);
|
|
}
|
|
} else if ((phase == 4 or phase == 5 or phase == 6) and altitude <= 10980) {
|
|
if (mngktsmach) {
|
|
setprop("/FMGC/internal/mng-kts-mach", 0);
|
|
}
|
|
if (mng_spd_cmd != 250 and !decel) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", 250);
|
|
} else if (mng_spd_cmd != minspeed and decel) {
|
|
setprop("/FMGC/internal/mng-spd-cmd", minspeed);
|
|
}
|
|
}
|
|
|
|
mng_spd_cmd = getprop("/FMGC/internal/mng-spd-cmd");
|
|
|
|
if (mng_spd_cmd > maxspeed -5) {
|
|
setprop("/FMGC/internal/mng-spd", maxspeed -5);
|
|
} else {
|
|
setprop("/FMGC/internal/mng-spd", mng_spd_cmd);
|
|
}
|
|
|
|
if (ktsmach and !mngktsmach) {
|
|
setprop("it-autoflight/input/kts-mach", 0);
|
|
} else if (!ktsmach and mngktsmach) {
|
|
setprop("it-autoflight/input/kts-mach", 1);
|
|
}
|
|
|
|
mng_spd = getprop("/FMGC/internal/mng-spd");
|
|
|
|
if (kts_sel != mng_spd and !ktsmach) {
|
|
setprop("it-autoflight/input/spd-kts", mng_spd);
|
|
} else if (mach_sel != mng_spd and ktsmach) {
|
|
setprop("it-autoflight/input/spd-mach", mng_spd);
|
|
}
|
|
} else {
|
|
ManagedSPD.stop();
|
|
}
|
|
} else {
|
|
ManagedSPD.stop();
|
|
libraries.mcpSPDKnbPull();
|
|
}
|
|
});
|
|
|
|
var switchDatabase = func {
|
|
database1 = getprop("/FMGC/internal/navdatabase");
|
|
database2 = getprop("/FMGC/internal/navdatabase2");
|
|
code1 = getprop("/FMGC/internal/navdatabasecode");
|
|
code2 = getprop("/FMGC/internal/navdatabasecode2");
|
|
setprop("/FMGC/internal/navdatabase", database2);
|
|
setprop("/FMGC/internal/navdatabase2", database1);
|
|
setprop("/FMGC/internal/navdatabasecode", code2);
|
|
setprop("/FMGC/internal/navdatabasecode2", code1);
|
|
}
|
|
|
|
# Landing to phase 7
|
|
setlistener("gear/gear[1]/wow", func() {
|
|
if (getprop("/gear/gear[1]/wow") == 0 and timer30secLanding.isRunning) {
|
|
timer30secLanding.stop();
|
|
setprop("/FMGC/internal/landing-time", -99);
|
|
}
|
|
|
|
if (getprop("/gear/gear[1]/wow") == 1 and getprop("/FMGC/internal/landing-time") == -99) {
|
|
timer30secLanding.start();
|
|
setprop("/FMGC/internal/landing-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
}, 0, 0);
|
|
|
|
# Align IRS 1
|
|
setlistener("systems/navigation/adr/operating-1", func() {
|
|
if (timer48gpsAlign1.isRunning) {
|
|
timer48gpsAlign1.stop();
|
|
}
|
|
|
|
if (getprop("/FMGC/internal/align1-time") == -99) {
|
|
timer48gpsAlign1.start();
|
|
setprop("/FMGC/internal/align1-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
}, 0, 0);
|
|
|
|
# Align IRS 2
|
|
setlistener("systems/navigation/adr/operating-2", func() {
|
|
if (timer48gpsAlign2.isRunning) {
|
|
timer48gpsAlign2.stop();
|
|
}
|
|
|
|
if (getprop("/FMGC/internal/align2-time") == -99) {
|
|
timer48gpsAlign2.start();
|
|
setprop("/FMGC/internal/align2-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
}, 0, 0);
|
|
|
|
# Align IRS 3
|
|
setlistener("systems/navigation/adr/operating-3", func() {
|
|
if (timer48gpsAlign3.isRunning) {
|
|
timer48gpsAlign3.stop();
|
|
}
|
|
|
|
if (getprop("/FMGC/internal/align3-time") == -99) {
|
|
timer48gpsAlign3.start();
|
|
setprop("/FMGC/internal/align3-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
}, 0, 0);
|
|
|
|
# Calculate Block Fuel
|
|
setlistener("/FMGC/internal/block-calculating", func() {
|
|
if (timer3blockFuel.isRunning) {
|
|
setprop("/FMGC/internal/block-fuel-time", -99);
|
|
timer3blockFuel.start();
|
|
setprop("/FMGC/internal/block-fuel-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
|
|
if (getprop("/FMGC/internal/block-fuel-time") == -99) {
|
|
timer3blockFuel.start();
|
|
setprop("/FMGC/internal/block-fuel-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
}, 0, 0);
|
|
|
|
# Calculate Fuel Prediction
|
|
setlistener("/FMGC/internal/fuel-calculating", func() {
|
|
if (timer5fuelPred.isRunning) {
|
|
setprop("/FMGC/internal/fuel-pred-time", -99);
|
|
timer5fuelPred.start();
|
|
setprop("/FMGC/internal/fuel-pred-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
|
|
if (getprop("/FMGC/internal/fuel-pred-time") == -99) {
|
|
timer5fuelPred.start();
|
|
setprop("/FMGC/internal/fuel-pred-time", pts.Sim.Time.elapsedSec.getValue());
|
|
}
|
|
}, 0, 0);
|
|
|
|
# Maketimers
|
|
var timer30secLanding = maketimer(1, func() {
|
|
if (pts.Sim.Time.elapsedSec.getValue() > getprop("/FMGC/internal/landing-time") + 30) {
|
|
setprop("/FMGC/status/phase", 7);
|
|
setprop("/FMGC/internal/landing-time", -99);
|
|
timer30secLanding.stop();
|
|
}
|
|
});
|
|
|
|
var timer48gpsAlign1 = maketimer(1, func() {
|
|
if (pts.Sim.Time.elapsedSec.getValue() > getprop("/FMGC/internal/align1-time") + 48 or getprop("/systems/acconfig/options/adirs-skip")) {
|
|
setprop("/FMGC/internal/align1-done", 1);
|
|
setprop("/FMGC/internal/align1-time", -99);
|
|
timer48gpsAlign1.stop();
|
|
}
|
|
});
|
|
|
|
var timer48gpsAlign2 = maketimer(1, func() {
|
|
if (pts.Sim.Time.elapsedSec.getValue() > getprop("/FMGC/internal/align2-time") + 48 or getprop("/systems/acconfig/options/adirs-skip")) {
|
|
setprop("/FMGC/internal/align2-done", 1);
|
|
setprop("/FMGC/internal/align2-time", -99);
|
|
timer48gpsAlign2.stop();
|
|
}
|
|
});
|
|
|
|
var timer48gpsAlign3 = maketimer(1, func() {
|
|
if (pts.Sim.Time.elapsedSec.getValue() > getprop("/FMGC/internal/align3-time") + 48 or getprop("/systems/acconfig/options/adirs-skip")) {
|
|
setprop("/FMGC/internal/align3-done", 1);
|
|
setprop("/FMGC/internal/align3-time", -99);
|
|
timer48gpsAlign3.stop();
|
|
}
|
|
});
|
|
|
|
var timer3blockFuel = maketimer(1, func() {
|
|
if (pts.Sim.Time.elapsedSec.getValue() > getprop("/FMGC/internal/block-fuel-time") + 3) {
|
|
setprop("/FMGC/internal/block", sprintf("%3.1f", math.round(getprop("/consumables/fuel/total-fuel-lbs") / 1000, 0.1)));
|
|
setprop("/FMGC/internal/block-set", 1);
|
|
if (!getprop("/FMGC/internal/zfw-set")) {
|
|
setprop("/FMGC/internal/zfw", sprintf("%3.1f", math.round((getprop("/fdm/jsbsim/inertia/weight-lbs") - getprop("/consumables/fuel/total-fuel-lbs")) / 1000, 0.1)));
|
|
setprop("/FMGC/internal/zfw-set", 1);
|
|
}
|
|
setprop("/FMGC/internal/block-calculating", 0);
|
|
setprop("/FMGC/internal/block-fuel-time", -99);
|
|
timer3blockFuel.stop();
|
|
}
|
|
});
|
|
|
|
var timer5fuelPred = maketimer(1, func() {
|
|
if (pts.Sim.Time.elapsedSec.getValue() > getprop("/FMGC/internal/fuel-pred-time") + 5) {
|
|
if (!getprop("/FMGC/internal/zfw-set")) {
|
|
setprop("/FMGC/internal/zfw", sprintf("%3.1f", math.round((getprop("/fdm/jsbsim/inertia/weight-lbs") - getprop("/consumables/fuel/total-fuel-lbs")) / 1000, 0.1)));
|
|
setprop("/FMGC/internal/zfw-set", 1);
|
|
}
|
|
updateFuel();
|
|
setprop("/FMGC/internal/fuel-calculating", 0);
|
|
setprop("/FMGC/internal/fuel-pred-time", -99);
|
|
timer5fuelPred.stop();
|
|
}
|
|
}); |