# A3XX FADEC/Throttle Control System # Joshua Davidson (it0uchpods) ############################################## # Copyright (c) Joshua Davidson (it0uchpods) # ############################################## setprop("/systems/thrust/alpha-floor", 0); setprop("/systems/thrust/toga-lk", 0); setprop("/systems/thrust/epr/toga-lim", 0.0); setprop("/systems/thrust/epr/mct-lim", 0.0); setprop("/systems/thrust/epr/flx-lim", 0.0); setprop("/systems/thrust/epr/clb-lim", 0.0); setprop("/systems/thrust/n1/toga-lim", 0.0); setprop("/systems/thrust/n1/mct-lim", 0.0); setprop("/systems/thrust/n1/flx-lim", 0.0); setprop("/systems/thrust/n1/clb-lim", 0.0); setprop("/engines/flx-thr", 0.0); setprop("/controls/engines/thrust-limit", "TOGA"); setprop("/controls/engines/epr-limit", 0.0); setprop("/controls/engines/n1-limit", 0.0); setprop("/systems/thrust/state1", "IDLE"); setprop("/systems/thrust/state2", "IDLE"); setprop("/systems/thrust/lvrclb", 0); setprop("/systems/thrust/clbreduc-ft", "1500"); setprop("/systems/thrust/toga-lim", 0.0); setprop("/systems/thrust/mct-lim", 0.0); setprop("/systems/thrust/clb-lim", 0.0); setprop("/systems/thrust/lim-flex", 0); setprop("/engines/flex-derate", 0); setprop("/systems/thrust/eng-out", 0); setlistener("/sim/signals/fdm-initialized", func { var thr1 = getprop("/controls/engines/engine[0]/throttle-pos"); var thr2 = getprop("/controls/engines/engine[1]/throttle-pos"); var state1 = getprop("/systems/thrust/state1"); var state2 = getprop("/systems/thrust/state2"); var engstate1 = getprop("/engines/engine[0]/state"); var engstate2 = getprop("/engines/engine[1]/state"); var eprtoga = getprop("/systems/thrust/epr/toga-lim"); var eprmct = getprop("/systems/thrust/epr/mct-lim"); var eprflx = getprop("/systems/thrust/epr/flx-lim"); var eprclb = getprop("/systems/thrust/epr/clb-lim"); var n1toga = getprop("/systems/thrust/n1/toga-lim"); var n1mct = getprop("/systems/thrust/n1/mct-lim"); var n1flx = getprop("/systems/thrust/n1/flx-lim"); var n1clb = getprop("/systems/thrust/n1/clb-lim"); var alpha = getprop("/fdm/jsbsim/aero/alpha-deg"); var flaps = getprop("/controls/flight/flap-pos"); var alphaProt = 0; var togaLock = 0; var gs = getprop("/velocities/groundspeed-kt"); thrust_lim.start(); thrustt.start(); }); setlistener("/controls/engines/engine[0]/throttle-pos", func { engstate1 = getprop("/engines/engine[0]/state"); engstate2 = getprop("/engines/engine[1]/state"); thr1 = getprop("/controls/engines/engine[0]/throttle-pos"); if (getprop("/systems/thrust/alpha-floor") == 0 and getprop("/systems/thrust/toga-lk") == 0) { if (thr1 < 0.01) { setprop("/systems/thrust/state1", "IDLE"); unflex(); atoff_request(); } else if (thr1 >= 0.01 and thr1 < 0.60) { setprop("/systems/thrust/state1", "MAN"); unflex(); } else if (thr1 >= 0.60 and thr1 < 0.65) { setprop("/systems/thrust/state1", "CL"); unflex(); } else if (thr1 >= 0.65 and thr1 < 0.78) { setprop("/systems/thrust/state1", "MAN THR"); unflex(); } else if (thr1 >= 0.78 and thr1 < 0.83) { if (getprop("/systems/thrust/eng-out") != 1) { if (getprop("/controls/engines/thrust-limit") == "FLX") { if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) { setprop("/it-autoflight/input/athr", 1); } setprop("/controls/engines/engine[0]/throttle-fdm", 0.99); } else { setprop("/controls/engines/engine[0]/throttle-fdm", 0.95); } } setprop("/systems/thrust/state1", "MCT"); } else if (thr1 >= 0.83 and thr1 < 0.95) { setprop("/systems/thrust/state1", "MAN THR"); unflex(); } else if (thr1 >= 0.95) { if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) { setprop("/it-autoflight/input/athr", 1); } setprop("/controls/engines/engine[0]/throttle-fdm", 0.99); setprop("/systems/thrust/state1", "TOGA"); unflex(); } } else { if (thr1 < 0.01) { setprop("/systems/thrust/state1", "IDLE"); } else if (thr1 >= 0.01 and thr1 < 0.60) { setprop("/systems/thrust/state1", "MAN"); } else if (thr1 >= 0.60 and thr1 < 0.65) { setprop("/systems/thrust/state1", "CL"); } else if (thr1 >= 0.65 and thr1 < 0.78) { setprop("/systems/thrust/state1", "MAN THR"); } else if (thr1 >= 0.78 and thr1 < 0.83) { setprop("/systems/thrust/state1", "MCT"); } else if (thr1 >= 0.83 and thr1 < 0.95) { setprop("/systems/thrust/state1", "MAN THR"); } else if (thr1 >= 0.95) { setprop("/systems/thrust/state1", "TOGA"); } setprop("/controls/engines/engine[0]/throttle-fdm", 0.99); } }); setlistener("/controls/engines/engine[1]/throttle-pos", func { engstate1 = getprop("/engines/engine[0]/state"); engstate2 = getprop("/engines/engine[1]/state"); thr2 = getprop("/controls/engines/engine[1]/throttle-pos"); if (getprop("/systems/thrust/alpha-floor") == 0 and getprop("/systems/thrust/toga-lk") == 0) { if (thr2 < 0.01) { setprop("/systems/thrust/state2", "IDLE"); unflex(); atoff_request(); } else if (thr2 >= 0.01 and thr2 < 0.60) { setprop("/systems/thrust/state2", "MAN"); unflex(); } else if (thr2 >= 0.60 and thr2 < 0.65) { setprop("/systems/thrust/state2", "CL"); unflex(); } else if (thr2 >= 0.65 and thr2 < 0.78) { setprop("/systems/thrust/state2", "MAN THR"); unflex(); } else if (thr2 >= 0.78 and thr2 < 0.83) { if (getprop("/systems/thrust/eng-out") != 1) { if (getprop("/controls/engines/thrust-limit") == "FLX") { if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) { setprop("/it-autoflight/input/athr", 1); } setprop("/controls/engines/engine[1]/throttle-fdm", 0.99); } else { setprop("/controls/engines/engine[1]/throttle-fdm", 0.95); } } setprop("/systems/thrust/state2", "MCT"); } else if (thr2 >= 0.83 and thr2 < 0.95) { setprop("/systems/thrust/state2", "MAN THR"); unflex(); } else if (thr2 >= 0.95) { if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) { setprop("/it-autoflight/input/athr", 1); } setprop("/controls/engines/engine[1]/throttle-fdm", 0.99); setprop("/systems/thrust/state2", "TOGA"); unflex(); } } else { if (thr2 < 0.01) { setprop("/systems/thrust/state2", "IDLE"); } else if (thr2 >= 0.01 and thr2 < 0.60) { setprop("/systems/thrust/state2", "MAN"); } else if (thr2 >= 0.60 and thr2 < 0.65) { setprop("/systems/thrust/state2", "CL"); } else if (thr2 >= 0.65 and thr2 < 0.78) { setprop("/systems/thrust/state2", "MAN THR"); } else if (thr2 >= 0.78 and thr2 < 0.83) { setprop("/systems/thrust/state2", "MCT"); } else if (thr2 >= 0.83 and thr2 < 0.95) { setprop("/systems/thrust/state2", "MAN THR"); } else if (thr2 >= 0.95) { setprop("/systems/thrust/state2", "TOGA"); } setprop("/controls/engines/engine[1]/throttle-fdm", 0.99); } }); # Alpha Floor and Toga Lock setlistener("/it-autoflight/input/athr", func { if (getprop("/systems/thrust/alpha-floor") == 1) { setprop("/it-autoflight/input/athr", 1); } else { setprop("/systems/thrust/toga-lk", 0); } }); # Checks if all throttles are in the IDLE position, before tuning off the A/THR. var atoff_request = func { state1 = getprop("/systems/thrust/state1"); state2 = getprop("/systems/thrust/state2"); if ((state1 == "IDLE") and (state2 == "IDLE") and (getprop("/systems/thrust/alpha-floor") == 0) and (getprop("/systems/thrust/toga-lk") == 0)) { setprop("/it-autoflight/input/athr", 0); } } var thrust_lim = maketimer(0.04, func { state1 = getprop("/systems/thrust/state1"); state2 = getprop("/systems/thrust/state2"); engstate1 = getprop("/engines/engine[0]/state"); engstate2 = getprop("/engines/engine[1]/state"); thr1 = getprop("/controls/engines/engine[0]/throttle-pos"); thr2 = getprop("/controls/engines/engine[1]/throttle-pos"); eprtoga = getprop("/systems/thrust/epr/toga-lim"); eprmct = getprop("/systems/thrust/epr/mct-lim"); eprflx = getprop("/systems/thrust/epr/flx-lim"); eprclb = getprop("/systems/thrust/epr/clb-lim"); n1toga = getprop("/systems/thrust/n1/toga-lim"); n1mct = getprop("/systems/thrust/n1/mct-lim"); n1flx = getprop("/systems/thrust/n1/flx-lim"); n1clb = getprop("/systems/thrust/n1/clb-lim"); gs = getprop("/velocities/groundspeed-kt"); if (getprop("/FMGC/internal/flex-set") == 1 and getprop("/systems/fadec/n1mode1") == 0 and getprop("/systems/fadec/n1mode2") == 0 and getprop("/gear/gear[1]/wow") == 1 and getprop("/gear/gear[2]/wow") == 1 and gs < 40) { setprop("/systems/thrust/lim-flex", 1); } else if (getprop("/FMGC/internal/flex-set") == 0 and engstate1 != 3 and engstate2 != 3) { setprop("/systems/thrust/lim-flex", 0); } if (getprop("/controls/engines/engine[0]/reverser") == "1" or getprop("/controls/engines/engine[1]/reverser") == "1") { setprop("/controls/engines/thrust-limit", "MREV"); setprop("/controls/engines/epr-limit", 1.000); setprop("/controls/engines/n1-limit", 0.0); } else if (getprop("/gear/gear[1]/wow") == 0 or getprop("/gear/gear[2]/wow") == 0 or (engstate1 != 3 and engstate2 != 3)) { if ((state1 == "TOGA" or state2 == "TOGA" or (state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83)) or getprop("/systems/thrust/alpha-floor") == 1 or getprop("/systems/thrust/toga-lk") == 1) { setprop("/controls/engines/thrust-limit", "TOGA"); setprop("/controls/engines/epr-limit", eprtoga); setprop("/controls/engines/n1-limit", n1toga); } else if ((state1 == "MCT" or state2 == "MCT" or (state1 == "MAN THR" and thr1 < 0.83) or (state2 == "MAN THR" and thr2 < 0.83)) and getprop("/systems/thrust/lim-flex") == 0) { setprop("/controls/engines/thrust-limit", "MCT"); setprop("/controls/engines/epr-limit", eprmct); setprop("/controls/engines/n1-limit", n1mct); } else if ((state1 == "MCT" or state2 == "MCT" or (state1 == "MAN THR" and thr1 < 0.83) or (state2 == "MAN THR" and thr2 < 0.83)) and getprop("/systems/thrust/lim-flex") == 1) { setprop("/controls/engines/thrust-limit", "FLX"); setprop("/controls/engines/epr-limit", eprflx); setprop("/controls/engines/n1-limit", n1flx); } else if (state1 == "CL" or state2 == "CL" or state1 == "MAN" or state2 == "MAN" or state1 == "IDLE" or state2 == "IDLE") { setprop("/controls/engines/thrust-limit", "CLB"); setprop("/controls/engines/epr-limit", eprclb); setprop("/controls/engines/n1-limit", n1clb); } } else if (getprop("/FMGC/internal/flex-set") == 1 and getprop("/systems/fadec/n1mode1") == 0 and getprop("/systems/fadec/n1mode2") == 0) { if ((state1 == "TOGA" or state2 == "TOGA" or (state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83)) or getprop("/systems/thrust/alpha-floor") == 1 or getprop("/systems/thrust/toga-lk") == 1) { setprop("/controls/engines/thrust-limit", "TOGA"); setprop("/controls/engines/epr-limit", eprtoga); setprop("/controls/engines/n1-limit", n1toga); } else { setprop("/controls/engines/thrust-limit", "FLX"); setprop("/controls/engines/epr-limit", eprflx); setprop("/controls/engines/n1-limit", n1flx); } } else { setprop("/controls/engines/thrust-limit", "TOGA"); setprop("/controls/engines/epr-limit", eprtoga); setprop("/controls/engines/n1-limit", n1toga); } }); var unflex = func { state1 = getprop("/systems/thrust/state1"); state2 = getprop("/systems/thrust/state2"); if (state1 != "MCT" and state2 != "MCT" and getprop("/gear/gear[1]/wow") == 0 and getprop("/gear/gear[2]/wow") == 0) { setprop("/systems/thrust/lim-flex", 0); } } var thrust_loop = func { state1 = getprop("/systems/thrust/state1"); state2 = getprop("/systems/thrust/state2"); if (getprop("/gear/gear[1]/wow") == 0 and getprop("/gear/gear[2]/wow") == 0 and (getprop("/engines/engine[0]/state") != 3 or getprop("/engines/engine[1]/state") != 3)) { setprop("/systems/thrust/eng-out", 1); } else { setprop("/systems/thrust/eng-out", 0); } if (state1 == "CL" and state2 == "CL" and getprop("/systems/thrust/eng-out") != 1) { setprop("/systems/thrust/lvrclb", 0); } else if (state1 == "MCT" and state2 == "MCT" and getprop("/systems/thrust/lim-flex") != 1 and getprop("/systems/thrust/eng-out") == 1) { setprop("/systems/thrust/lvrclb", 0); } else { var status = getprop("/systems/thrust/lvrclb"); if (status == 0) { if (getprop("/gear/gear[0]/wow") == 0) { if (getprop("/systems/thrust/state1") == "MAN" or getprop("/systems/thrust/state2") == "MAN") { setprop("/systems/thrust/lvrclb", 1); } else { if (getprop("/instrumentation/altimeter/indicated-altitude-ft") >= getprop("/systems/thrust/clbreduc-ft") and getprop("/gear/gear[1]/wow") == 0 and getprop("/gear/gear[2]/wow") == 0) { setprop("/systems/thrust/lvrclb", 1); } else if ((state1 == "CL" and state2 != "CL") or (state1 != "CL" and state2 == "CL") and getprop("/systems/thrust/eng-out") != 1) { setprop("/systems/thrust/lvrclb", 1); } else { setprop("/systems/thrust/lvrclb", 0); } } } } else if (status == 1) { setprop("/systems/thrust/lvrclb", 0); } } alpha = getprop("/fdm/jsbsim/aero/alpha-deg"); flaps = getprop("/controls/flight/flap-pos"); if (flaps == 0) { alphaProt = 9.5; } else if (flaps == 1 or flaps == 2 or flaps == 3) { alphaProt = 15.0; } else if (flaps == 4) { alphaProt = 14.0; } else if (flaps == 5) { alphaProt = 13.0; } togaLock = alphaProt - 1; if (getprop("/gear/gear[1]/wow") == 0 and getprop("/gear/gear[2]/wow") == 0 and getprop("/it-fbw/law") == 0 and (getprop("/systems/thrust/eng-out") == 0 or (getprop("/systems/thrust/eng-out") == 1 and flaps == 0)) and getprop("/systems/fadec/n1mode1") == 0 and getprop("/systems/fadec/n1mode2") == 0) { if (alpha > alphaProt and getprop("/position/gear-agl-ft") >= 100) { setprop("/systems/thrust/alpha-floor", 1); setprop("/systems/thrust/toga-lk", 0); setprop("/it-autoflight/input/athr", 1); } else if (getprop("/systems/thrust/alpha-floor") == 1 and alpha < togaLock) { setprop("/systems/thrust/alpha-floor", 0); setprop("/it-autoflight/input/athr", 1); setprop("/systems/thrust/toga-lk", 1); } } else { setprop("/systems/thrust/alpha-floor", 0); setprop("/systems/thrust/toga-lk", 0); } } # Timers var thrustt = maketimer(0.5, thrust_loop);