A3XX: Managed Speed in DES, General fixes
Allowed Managed Speed to work in DES mode, but it will not DECEL the plane, so be aware. Also fixed a few bugs with Managed Speed, and the FMGC
This commit is contained in:
parent
991b7afb5f
commit
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6 changed files with 87 additions and 43 deletions
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@ -11,7 +11,7 @@
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</sim>
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</sim>
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<options>
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<options>
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<EIS2 type="bool">1</EIS2>
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<EIS2 type="bool">0</EIS2>
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</options>
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</options>
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<sharklet type="bool">0</sharklet>
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<sharklet type="bool">0</sharklet>
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100
Nasal/FMGC.nas
100
Nasal/FMGC.nas
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@ -6,6 +6,7 @@
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##################
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##################
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setprop("/FMGC/internal/overspeed", 338);
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setprop("/FMGC/internal/overspeed", 338);
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setprop("/FMGC/internal/minspeed", 204);
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setprop("/position/gear-agl-ft", 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", 157);
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setprop("/FMGC/internal/mng-spd-cmd", 157);
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setprop("/FMGC/internal/mng-spd-cmd", 157);
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@ -16,7 +17,7 @@ setprop("/it-autoflight/internal/vert-speed-fpm", 0);
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var FMGCinit = func {
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var FMGCinit = func {
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setprop("/FMGC/status/to-state", 0);
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setprop("/FMGC/status/to-state", 0);
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setprop("/FMGC/status/phase", "0"); # 0 is preflight 1 takeoff 2 climb 3 cruise 4 descent 5 approach 6 go around 7 done
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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/tropo", 36090);
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setprop("/FMGC/internal/tropo", 36090);
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setprop("/FMGC/internal/overspeed", 338);
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setprop("/FMGC/internal/overspeed", 338);
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setprop("/FMGC/internal/mng-spd", 157);
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setprop("/FMGC/internal/mng-spd", 157);
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@ -24,6 +25,7 @@ var FMGCinit = func {
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setprop("/FMGC/internal/mng-kts-mach", 0);
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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("/FMGC/internal/mach-switchover", 0);
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setprop("/it-autoflight/settings/reduc-agl-ft", 3000);
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setprop("/it-autoflight/settings/reduc-agl-ft", 3000);
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setprop("/FMGC/internal/decel", 0);
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phasecheck.start();
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phasecheck.start();
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various.start();
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various.start();
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}
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}
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@ -80,6 +82,7 @@ var phasecheck = maketimer(0.2, func {
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var n1_left = getprop("/engines/engine[0]/n1");
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var n1_left = getprop("/engines/engine[0]/n1");
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var n1_right = getprop("/engines/engine[1]/n1");
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var n1_right = getprop("/engines/engine[1]/n1");
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var flaps = getprop("/controls/flight/flap-pos");
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var flaps = getprop("/controls/flight/flap-pos");
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var modelat = getprop("/modes/pfd/fma/roll-mode");
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var mode = getprop("/modes/pfd/fma/pitch-mode");
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var mode = getprop("/modes/pfd/fma/pitch-mode");
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var gs = getprop("/velocities/groundspeed-kt");
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var gs = getprop("/velocities/groundspeed-kt");
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var alt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
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var alt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
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@ -97,32 +100,41 @@ var phasecheck = maketimer(0.2, func {
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var targetfpa = getprop("/it-autoflight/input/fpa");
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var targetfpa = getprop("/it-autoflight/input/fpa");
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var vertmode = getprop("/modes/pfd/fma/pitch-mode");
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var vertmode = getprop("/modes/pfd/fma/pitch-mode");
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var reduc_agl_ft = getprop("/it-autoflight/settings/reduc-agl-ft");
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var reduc_agl_ft = getprop("/it-autoflight/settings/reduc-agl-ft");
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var locarm = getprop("/it-autopilot/output/loc-armed");
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var apprarm = getprop("/it-autopilot/output/appr-armed");
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if ((((n1_left >= 85) and (n1_right >= 85)) or (gs > 90 )) and flaps < 4 and (mode == "SRS")) {
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if ((((n1_left >= 85) and (n1_right >= 85)) or (gs > 90 )) and flaps < 4 and (mode == "SRS")) {
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setprop("/FMGC/status/phase", "1");
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setprop("/FMGC/status/phase", "1");
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setprop("/systems/pressurization/mode", "TO");
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setprop("/systems/pressurization/mode", "TO");
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}
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}
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if ((aglalt >= reduc_agl_ft) and (alt <= cruiseft) and (phase == "1") and (phase != "4") and (mode != "SRS")) {
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if ((aglalt >= reduc_agl_ft) and (alt <= cruiseft) and (phase == "1") and (phase != "4") and (mode != "SRS")) {
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setprop("/FMGC/status/phase", "2");
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setprop("/FMGC/status/phase", "2");
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}
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}
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if (alt >= cruiseft_b and phase == "2" and (mode == "ALT" or mode == "ALT CRZ")) {
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if (alt >= cruiseft_b and phase == "2" and (mode == "ALT" or mode == "ALT CRZ")) {
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setprop("/FMGC/status/phase", "3");
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setprop("/FMGC/status/phase", "3");
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setprop("/systems/pressurization/mode", "CR");
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setprop("/systems/pressurization/mode", "CR");
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}
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}
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if (alt <= cruiseft and (mode == "DES" or mode == "OP DES") and phase == "3") {
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if (alt <= cruiseft and (mode == "DES" or mode == "OP DES") and phase == "3") {
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setprop("/FMGC/status/phase", "4");
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setprop("/FMGC/status/phase", "4");
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setprop("/systems/pressurization/mode", "DE");
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setprop("/systems/pressurization/mode", "DE");
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}
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}
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if (getprop("/FMGC/status/to-state") == 0 and flaps >= 4 and ((phase == "4") or (phase == "2"))) { # add man activation of approach phase in MCDU or DECEL when those things are simulated
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if (getprop("/FMGC/status/to-state") == 0 and flaps >= 3 and ((phase == "2") or (phase == "4"))) {
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setprop("/FMGC/status/phase", "5");
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setprop("/FMGC/status/phase", "5");
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}
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}
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if ((phase == "5") and (state1 == "TOGA") and (state2 == "TOGA")) { # this is the only fully correct one to FCOM
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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("/FMGC/status/phase", "6");
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setprop("/it-autoflight/input/toga", 1);
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setprop("/it-autoflight/input/toga", 1);
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}
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}
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# forget transition from APP to climb for now because it would be too complex
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if ((phase == "6") and ((vertmode == "G/A CLB") or (vertmode == "SPD CLB") or (vertmode == "CLB") or ((vertmode == "V/S") and (targetvs > 0)) or ((vertmode == "FPA") and (targetfpa > 0))) and (alt <= targetalt)) {
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if ((phase == "6") and ((vertmode == "G/A CLB") or (vertmode == "SPD CLB") or (vertmode == "CLB") or ((vertmode == "V/S") and (targetvs > 0)) or ((vertmode == "FPA") and (targetfpa > 0))) and (alt <= targetalt)) {
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setprop("/FMGC/status/phase", "2"); # going to CLIMB mode from GA
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setprop("/FMGC/status/phase", "2");
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}
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}
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if ((wowl and wowr) and (gs < 20) and (phase == "5")) {
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if ((wowl and wowr) and (gs < 20) and (phase == "5")) {
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setprop("/FMGC/status/phase", "7");
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setprop("/FMGC/status/phase", "7");
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var fd1 = getprop("/it-autoflight/input/fd1");
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var fd1 = getprop("/it-autoflight/input/fd1");
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@ -135,6 +147,27 @@ var phasecheck = maketimer(0.2, func {
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setprop("/it-autoflight/input/fd2", fd2);
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setprop("/it-autoflight/input/fd2", fd2);
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press_init();
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press_init();
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}
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}
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var flap = getprop("/controls/flight/flap-pos");
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if (flap == 0) {
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setprop("/FMGC/internal/overspeed", 338);
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setprop("/FMGC/internal/minspeed", 204);
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} else if (flap == 1) {
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setprop("/FMGC/internal/overspeed", 216);
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setprop("/FMGC/internal/minspeed", 188);
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} else if (flap == 2) {
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setprop("/FMGC/internal/overspeed", 207);
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setprop("/FMGC/internal/minspeed", 171);
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} else if (flap == 3) {
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setprop("/FMGC/internal/overspeed", 189);
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setprop("/FMGC/internal/minspeed", 159);
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} else if (flap == 4) {
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setprop("/FMGC/internal/overspeed", 174);
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setprop("/FMGC/internal/minspeed", 146);
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} else if (flap == 5) {
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setprop("/FMGC/internal/overspeed", 163);
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setprop("/FMGC/internal/minspeed", 136);
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}
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});
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});
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var various = maketimer(1, func {
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var various = maketimer(1, func {
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@ -145,21 +178,6 @@ var various = maketimer(1, func {
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} else {
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} else {
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setprop("/it-autoflight/settings/reduc-agl-ft", getprop("/FMGC/internal/reduc-agl-ft"));
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setprop("/it-autoflight/settings/reduc-agl-ft", getprop("/FMGC/internal/reduc-agl-ft"));
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}
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}
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var flap = getprop("/controls/flight/flap-pos");
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if (flap == 0) {
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setprop("/FMGC/internal/overspeed", 338);
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} else if (flap == 1) {
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setprop("/FMGC/internal/overspeed", 216);
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} else if (flap == 2) {
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setprop("/FMGC/internal/overspeed", 207);
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} else if (flap == 3) {
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setprop("/FMGC/internal/overspeed", 189);
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} else if (flap == 4) {
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setprop("/FMGC/internal/overspeed", 174);
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} else if (flap == 5) {
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setprop("/FMGC/internal/overspeed", 163);
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}
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});
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});
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#################
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#################
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@ -171,6 +189,7 @@ var ManagedSPD = maketimer(0.25, func {
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if (getprop("/it-autoflight/input/spd-managed") == 1) {
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if (getprop("/it-autoflight/input/spd-managed") == 1) {
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var alt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
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var alt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
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var mode = getprop("/modes/pfd/fma/pitch-mode");
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var mode = getprop("/modes/pfd/fma/pitch-mode");
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var ias = getprop("/instrumentation/airspeed-indicator/indicated-speed-kt");
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var mach = getprop("/instrumentation/airspeed-indicator/indicated-mach");
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var mach = getprop("/instrumentation/airspeed-indicator/indicated-mach");
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var ktsmach = getprop("/it-autoflight/input/kts-mach");
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var ktsmach = getprop("/it-autoflight/input/kts-mach");
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var mngktsmach = getprop("/FMGC/internal/mng-kts-mach");
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var mngktsmach = getprop("/FMGC/internal/mng-kts-mach");
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@ -179,10 +198,12 @@ var ManagedSPD = maketimer(0.25, func {
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var kts_sel = getprop("/it-autoflight/input/spd-kts");
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var kts_sel = getprop("/it-autoflight/input/spd-kts");
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var mach_sel = getprop("/it-autoflight/input/spd-mach");
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var mach_sel = getprop("/it-autoflight/input/spd-mach");
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var srsSPD = getprop("/it-autoflight/settings/togaspd");
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var srsSPD = getprop("/it-autoflight/settings/togaspd");
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var phase = getprop("/FMGC/status/phase"); # 0 is preflight 1 takeoff 2 climb 3 cruise 4 descent 5 approach 6 go around 7 done
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var 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
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var flap = getprop("/controls/flight/flap-pos");
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var flap = getprop("/controls/flight/flap-pos");
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var overspeed = getprop("/FMGC/internal/overspeed");
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var overspeed = getprop("/FMGC/internal/overspeed");
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var minspeed = getprop("/FMGC/internal/minspeed");
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var mach_switchover = getprop("/FMGC/internal/mach-switchover");
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var mach_switchover = getprop("/FMGC/internal/mach-switchover");
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var decel = getprop("/FMGC/internal/decel");
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var mng_alt_spd_cmd = getprop("/FMGC/internal/mng-alt-spd");
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var mng_alt_spd_cmd = getprop("/FMGC/internal/mng-alt-spd");
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var mng_alt_spd = math.round(mng_alt_spd_cmd, 1);
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var mng_alt_spd = math.round(mng_alt_spd_cmd, 1);
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@ -190,6 +211,14 @@ var ManagedSPD = maketimer(0.25, func {
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var mng_alt_mach_cmd = getprop("/FMGC/internal/mng-alt-mach");
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var mng_alt_mach_cmd = getprop("/FMGC/internal/mng-alt-mach");
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var mng_alt_mach = math.round(mng_alt_mach_cmd, 0.001);
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var mng_alt_mach = math.round(mng_alt_mach_cmd, 0.001);
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if (mach > mng_alt_mach and phase == 2) {
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setprop("/FMGC/internal/mach-switchover", 1);
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}
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if (ias > mng_alt_spd and (phase == 4 or phase == 5)) {
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setprop("/FMGC/internal/mach-switchover", 0);
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}
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if (mode == "SRS" and phase == 0 or phase == 1) {
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if (mode == "SRS" and phase == 0 or phase == 1) {
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if (mngktsmach) {
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if (mngktsmach) {
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setprop("/FMGC/internal/mng-kts-mach", 0);
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setprop("/FMGC/internal/mng-kts-mach", 0);
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@ -218,8 +247,29 @@ var ManagedSPD = maketimer(0.25, func {
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if (mng_spd_cmd != mng_alt_mach) {
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if (mng_spd_cmd != mng_alt_mach) {
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setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
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setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
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}
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}
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} else if (phase == 4 or phase == 5 or phase == 6 or phase == 7) {
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} else if (phase == 4 and alt > 11100 and !mach_switchover) {
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libraries.mcpSPDKnbPull();
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if (mngktsmach) {
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setprop("/FMGC/internal/mng-kts-mach", 0);
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}
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if (mng_spd_cmd != mng_alt_spd) {
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setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
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}
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} else if (phase == 4 and alt > 11100 and mach_switchover) {
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if (!mngktsmach) {
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setprop("/FMGC/internal/mng-kts-mach", 1);
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}
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if (mng_spd_cmd != mng_alt_mach) {
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setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
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}
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} else if ((phase == 4 or phase == 5 or phase == 6) and alt <= 11050) {
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if (mngktsmach) {
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setprop("/FMGC/internal/mng-kts-mach", 0);
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}
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if (mng_spd_cmd != 250 and !decel) {
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setprop("/FMGC/internal/mng-spd-cmd", 250);
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} else if (mng_spd_cmd != minspeed and decel) {
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setprop("/FMGC/internal/mng-spd-cmd", minspeed);
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}
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}
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}
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var mng_spd_cmd = getprop("/FMGC/internal/mng-spd-cmd");
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var mng_spd_cmd = getprop("/FMGC/internal/mng-spd-cmd");
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@ -243,10 +293,6 @@ var ManagedSPD = maketimer(0.25, func {
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} else if (mach_sel != mng_spd and ktsmach) {
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} else if (mach_sel != mng_spd and ktsmach) {
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setprop("/it-autoflight/input/spd-mach", mng_spd);
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setprop("/it-autoflight/input/spd-mach", mng_spd);
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}
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}
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if (mach >= mng_alt_mach and phase == 2) {
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setprop("/FMGC/internal/mach-switchover", 1);
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}
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} else {
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} else {
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ManagedSPD.stop();
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ManagedSPD.stop();
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}
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}
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@ -10,7 +10,7 @@ var MCDU_init = func {
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var MCDU_reset = func {
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var MCDU_reset = func {
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setprop("/it-autoflight/settings/togaspd", 157);
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setprop("/it-autoflight/settings/togaspd", 157);
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setprop("/MCDU[0]/last-fmgc-page", "STATUS");
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setprop("/MCDU[0]/last-fmgc-page", "STATUS");
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setprop("/MCDU[0]/page", "STATUS");
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setprop("/MCDU[0]/page", "MCDU");
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setprop("/MCDU[0]/scratchpad", "");
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setprop("/MCDU[0]/scratchpad", "");
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setprop("/MCDUC/flight-num", "");
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setprop("/MCDUC/flight-num", "");
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setprop("/MCDUC/thracc-set", 0);
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setprop("/MCDUC/thracc-set", 0);
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@ -46,6 +46,8 @@ var lskbutton = func(btn) {
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if (btn == "1") {
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if (btn == "1") {
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if (getprop("/MCDU[0]/page") == "MCDU") {
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if (getprop("/MCDU[0]/page") == "MCDU") {
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setprop("/MCDU[0]/page", getprop("/MCDU[0]/last-fmgc-page"));
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setprop("/MCDU[0]/page", getprop("/MCDU[0]/last-fmgc-page"));
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setprop("/MCDU[0]/scratchpad-msg", "1");
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setprop("/MCDU[0]/scratchpad", "GPS PRIMARY");
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} else if (getprop("/MCDU[0]/page") == "TO") {
|
} else if (getprop("/MCDU[0]/page") == "TO") {
|
||||||
PerfTOInput("L1");
|
PerfTOInput("L1");
|
||||||
}
|
}
|
||||||
|
@ -214,8 +216,6 @@ var initInputA = func(key) {
|
||||||
setprop("/FMGC/internal/arr-arpt", fromto[1]);
|
setprop("/FMGC/internal/arr-arpt", fromto[1]);
|
||||||
setprop("/FMGC/internal/tofrom-set", 1);
|
setprop("/FMGC/internal/tofrom-set", 1);
|
||||||
fmgc.updateARPT();
|
fmgc.updateARPT();
|
||||||
setprop("/MCDU[0]/scratchpad-msg", "1");
|
|
||||||
setprop("/MCDU[0]/scratchpad", "GPS PRIMARY");
|
|
||||||
} else {
|
} else {
|
||||||
setprop("/MCDU[0]/scratchpad-msg", "1");
|
setprop("/MCDU[0]/scratchpad-msg", "1");
|
||||||
setprop("/MCDU[0]/scratchpad", "NOT ALLOWED");
|
setprop("/MCDU[0]/scratchpad", "NOT ALLOWED");
|
||||||
|
|
|
@ -10,7 +10,7 @@ var MCDU_init = func {
|
||||||
var MCDU_reset = func {
|
var MCDU_reset = func {
|
||||||
setprop("/it-autoflight/settings/togaspd", 157);
|
setprop("/it-autoflight/settings/togaspd", 157);
|
||||||
setprop("/MCDU[1]/last-fmgc-page", "STATUS");
|
setprop("/MCDU[1]/last-fmgc-page", "STATUS");
|
||||||
setprop("/MCDU[1]/page", "STATUS");
|
setprop("/MCDU[1]/page", "MCDU");
|
||||||
setprop("/MCDU[1]/scratchpad", "");
|
setprop("/MCDU[1]/scratchpad", "");
|
||||||
setprop("/MCDUC/flight-num", "");
|
setprop("/MCDUC/flight-num", "");
|
||||||
setprop("/MCDUC/thracc-set", 0);
|
setprop("/MCDUC/thracc-set", 0);
|
||||||
|
@ -46,6 +46,8 @@ var lskbutton = func(btn) {
|
||||||
if (btn == "1") {
|
if (btn == "1") {
|
||||||
if (getprop("/MCDU[1]/page") == "MCDU") {
|
if (getprop("/MCDU[1]/page") == "MCDU") {
|
||||||
setprop("/MCDU[1]/page", getprop("/MCDU[1]/last-fmgc-page"));
|
setprop("/MCDU[1]/page", getprop("/MCDU[1]/last-fmgc-page"));
|
||||||
|
setprop("/MCDU[1]/scratchpad-msg", "1");
|
||||||
|
setprop("/MCDU[1]/scratchpad", "GPS PRIMARY");
|
||||||
} else if (getprop("/MCDU[1]/page") == "TO") {
|
} else if (getprop("/MCDU[1]/page") == "TO") {
|
||||||
PerfTOInput("L1");
|
PerfTOInput("L1");
|
||||||
}
|
}
|
||||||
|
@ -214,8 +216,6 @@ var initInputA = func(key) {
|
||||||
setprop("/FMGC/internal/arr-arpt", fromto[1]);
|
setprop("/FMGC/internal/arr-arpt", fromto[1]);
|
||||||
setprop("/FMGC/internal/tofrom-set", 1);
|
setprop("/FMGC/internal/tofrom-set", 1);
|
||||||
fmgc.updateARPT();
|
fmgc.updateARPT();
|
||||||
setprop("/MCDU[1]/scratchpad-msg", "1");
|
|
||||||
setprop("/MCDU[1]/scratchpad", "GPS PRIMARY");
|
|
||||||
} else {
|
} else {
|
||||||
setprop("/MCDU[1]/scratchpad-msg", "1");
|
setprop("/MCDU[1]/scratchpad-msg", "1");
|
||||||
setprop("/MCDU[1]/scratchpad", "NOT ALLOWED");
|
setprop("/MCDU[1]/scratchpad", "NOT ALLOWED");
|
||||||
|
|
|
@ -72,7 +72,6 @@
|
||||||
</equals>
|
</equals>
|
||||||
</condition>
|
</condition>
|
||||||
<expression>
|
<expression>
|
||||||
<floor>
|
|
||||||
<product>
|
<product>
|
||||||
<div>
|
<div>
|
||||||
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
|
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
|
||||||
|
@ -80,7 +79,6 @@
|
||||||
</div>
|
</div>
|
||||||
<property>/it-autoflight/input/spd-mach</property>
|
<property>/it-autoflight/input/spd-mach</property>
|
||||||
</product>
|
</product>
|
||||||
</floor>
|
|
||||||
</expression>
|
</expression>
|
||||||
</input>
|
</input>
|
||||||
<output>/FMGC/internal/target-ias-pfd</output>
|
<output>/FMGC/internal/target-ias-pfd</output>
|
||||||
|
|
Reference in a new issue