1
0
Fork 0

Restore style changes by legoboy

This commit is contained in:
Inuyaksa 2021-06-14 21:32:43 +02:00
parent 5715d480b7
commit e4548f7eef

View file

@ -31,6 +31,7 @@ var hdg = 0;
var alt = 0;
var altitude = 0;
var flap = 0;
var flaps = 0;
var freqnav0uf = 0;
var freqnav0 = 0;
var namenav0 = "XX";
@ -69,8 +70,8 @@ setprop("position/gear-agl-ft", 0);
setprop("/it-autoflight/settings/accel-agl-ft", 1500); #eventually set to 1500 above runway
setprop("/it-autoflight/internal/vert-speed-fpm", 0);
setprop("/it-autoflight/output/fma-pwr", 0);
setprop("instrumentation/nav[0]/nav-id", "XXX");
setprop("instrumentation/nav[1]/nav-id", "XXX");
setprop("/instrumentation/nav[0]/nav-id", "XXX");
setprop("/instrumentation/nav[1]/nav-id", "XXX");
setprop("/FMGC/internal/ils1-mcdu", "XXX/999.99");
setprop("/FMGC/internal/ils2-mcdu", "XXX/999.99");
setprop("/FMGC/internal/vor1-mcdu", "XXX/999.99");
@ -78,6 +79,9 @@ setprop("/FMGC/internal/vor2-mcdu", "999.99/XXX");
setprop("/FMGC/internal/adf1-mcdu", "XXX/999.99");
setprop("/FMGC/internal/adf2-mcdu", "999.99/XXX");
var FMGCAlignDone = [props.globals.initNode("/FMGC/internal/align1-done", 0, "BOOL"), props.globals.initNode("/FMGC/internal/align2-done", 0, "BOOL"), props.globals.initNode("/FMGC/internal/align3-done", 0, "BOOL")];
var FMGCAlignTime = [props.globals.initNode("/FMGC/internal/align1-time", 0, "DOUBLE"), props.globals.initNode("/FMGC/internal/align2-time", 0, "DOUBLE"), props.globals.initNode("/FMGC/internal/align3-time", 0, "DOUBLE")];
var adirsSkip = props.globals.getNode("/systems/acconfig/options/adirs-skip");
var blockCalculating = props.globals.initNode("/FMGC/internal/block-calculating", 0, "BOOL");
var fuelCalculating = props.globals.initNode("/FMGC/internal/fuel-calculating", 0, "BOOL");
@ -94,9 +98,9 @@ var FMGCinit = func {
setprop("/FMGC/internal/loc-source", "NAV0");
setprop("/FMGC/internal/optalt", 0);
setprop("/FMGC/internal/landing-time", -99);
setprop("/FMGC/internal/align1-time", -99);
setprop("/FMGC/internal/align2-time", -99);
setprop("/FMGC/internal/align3-time", -99);
FMGCAlignTime[0].setValue(-99);
FMGCAlignTime[1].setValue(-99);
FMGCAlignTime[2].setValue(-99);
setprop("/FMGC/internal/block-fuel-time", -99);
setprop("/FMGC/internal/fuel-pred-time", -99);
masterFMGC.start();
@ -333,7 +337,7 @@ var updateFuel = func {
final_time = final_fuel / (2.0 * ((zfw*zfw*-2e-10) + (zfw*0.0003) + 2.8903)); # x2 for 2 engines
if (final_time < 0) {
final_time = 0;
} else if (final_time > 480) {
} elsif (final_time > 480) {
final_time = 480;
}
if (num(final_time) >= 60) {
@ -355,7 +359,7 @@ var updateFuel = func {
final_fuel = final_time * 2.0 * ((zfw*zfw*-2e-10) + (zfw*0.0003) + 2.8903); # x2 for 2 engines
if (final_fuel < 0) {
final_fuel = 0;
} else if (final_fuel > 80000) {
} elsif (final_fuel > 80000) {
final_fuel = 80000;
}
FMGCInternal.finalFuel = final_fuel / 1000;
@ -364,14 +368,14 @@ var updateFuel = func {
# Calculate alternate fuel
if (!FMGCInternal.altFuelSet and FMGCInternal.altAirportSet) {
#calc
} else if (FMGCInternal.altFuelSet and FMGCInternal.altAirportSet) {
} elsif (FMGCInternal.altFuelSet and FMGCInternal.altAirportSet) {
#dummy calc for now
alt_fuel = 1000 * num(FMGCInternal.altFuel);
zfw = 1000 * FMGCInternal.zfw;
alt_time = alt_fuel / (2.0 * ((zfw*zfw*-2e-10) + (zfw*0.0003) + 2.8903)); # x2 for 2 engines
if (alt_time < 0) {
alt_time = 0;
} else if (alt_time > 480) {
} elsif (alt_time > 480) {
alt_time = 480;
}
if (num(alt_time) >= 60) {
@ -381,7 +385,7 @@ var updateFuel = func {
} else {
FMGCInternal.altTime = sprintf("%04d", alt_time);
}
} else if (!FMGCInternal.altFuelSet) {
} elsif (!FMGCInternal.altFuelSet) {
FMGCInternal.altFuel = 0.0;
FMGCInternal.altTime = "0000";
}
@ -412,7 +416,7 @@ var updateFuel = func {
trip_fuel = 4.018e+02 + (dist*3.575e+01) + (dist*dist*-4.260e-02) + (dist*dist*dist*-1.446e-05) + (dist*dist*dist*dist*4.101e-09) + (dist*dist*dist*dist*dist*-6.753e-13) + (dist*dist*dist*dist*dist*dist*5.074e-17) + (crz*-2.573e+01) + (dist*crz*-1.583e-01) + (dist*dist*crz*8.147e-04) + (dist*dist*dist*crz*4.485e-08) + (dist*dist*dist*dist*crz*-7.656e-12) + (dist*dist*dist*dist*dist*crz*4.503e-16) + (crz*crz*4.427e-01) + (dist*crz*crz*-1.137e-03) + (dist*dist*crz*crz*-4.409e-06) + (dist*dist*dist*crz*crz*-3.345e-11) + (dist*dist*dist*dist*crz*crz*4.985e-15) + (crz*crz*crz*-2.471e-03) + (dist*crz*crz*crz*1.223e-05) + (dist*dist*crz*crz*crz*9.660e-09) + (dist*dist*dist*crz*crz*crz*-2.127e-14) + (crz*crz*crz*crz*5.714e-06) + (dist*crz*crz*crz*crz*-3.546e-08) + (dist*dist*crz*crz*crz*crz*-7.536e-12) + (crz*crz*crz*crz*crz*-4.061e-09) + (dist*crz*crz*crz*crz*crz*3.355e-11) + (crz*crz*crz*crz*crz*crz*-1.451e-12);
if (trip_fuel < 400) {
trip_fuel = 400;
} else if (trip_fuel > 80000) {
} elsif (trip_fuel > 80000) {
trip_fuel = 80000;
}
@ -422,7 +426,7 @@ var updateFuel = func {
trip_time = 9.095e-02 + (dist*-3.968e-02) + (dist*dist*4.302e-04) + (dist*dist*dist*2.005e-07) + (dist*dist*dist*dist*-6.876e-11) + (dist*dist*dist*dist*dist*1.432e-14) + (dist*dist*dist*dist*dist*dist*-1.177e-18) + (crz*7.348e-01) + (dist*crz*3.310e-03) + (dist*dist*crz*-8.700e-06) + (dist*dist*dist*crz*-4.214e-10) + (dist*dist*dist*dist*crz*5.652e-14) + (dist*dist*dist*dist*dist*crz*-6.379e-18) + (crz*crz*-1.449e-02) + (dist*crz*crz*-7.508e-06) + (dist*dist*crz*crz*4.529e-08) + (dist*dist*dist*crz*crz*3.699e-13) + (dist*dist*dist*dist*crz*crz*8.466e-18) + (crz*crz*crz*1.108e-04) + (dist*crz*crz*crz*-4.126e-08) + (dist*dist*crz*crz*crz*-9.645e-11) + (dist*dist*dist*crz*crz*crz*-1.544e-16) + (crz*crz*crz*crz*-4.123e-07) + (dist*crz*crz*crz*crz*1.831e-10) + (dist*dist*crz*crz*crz*crz*7.438e-14) + (crz*crz*crz*crz*crz*7.546e-10) + (dist*crz*crz*crz*crz*crz*-1.921e-13) + (crz*crz*crz*crz*crz*crz*-5.453e-13);
if (trip_time < 10) {
trip_time = 10;
} else if (trip_time > 480) {
} elsif (trip_time > 480) {
trip_time = 480;
}
# if (low air conditioning) {
@ -430,7 +434,7 @@ var updateFuel = func {
#}
# if (total anti-ice) {
# trip_fuel = trip_fuel * 1.045;
#} else if (engine anti-ice) {
#} elsif (engine anti-ice) {
# trip_fuel = trip_fuel * 1.02;
#}
@ -439,7 +443,7 @@ var updateFuel = func {
trip_fuel = trip_fuel + (landing_weight_correction * (FMGCInternal.lw * 1000 - 121254.24421) / 2204.622622);
if (trip_fuel < 400) {
trip_fuel = 400;
} else if (trip_fuel > 80000) {
} elsif (trip_fuel > 80000) {
trip_fuel = 80000;
}
@ -467,7 +471,7 @@ var updateFuel = func {
FMGCInternal.rtePercent = 15.0; # need reasearch on this value
}
}
} else if (FMGCInternal.rtePercentSet) {
} elsif (FMGCInternal.rtePercentSet) {
FMGCInternal.rteRsv = num(FMGCInternal.tripFuel * FMGCInternal.rtePercent / 100.0);
} else {
if (num(FMGCInternal.tripFuel) <= 0.0) {
@ -497,7 +501,7 @@ var updateFuel = func {
extra_time = extra_fuel / (2.0 * ((lw*lw*-2e-10) + (lw*0.0003) + 2.8903)); # x2 for 2 engines
if (extra_time < 0) {
extra_time = 0;
} else if (extra_time > 480) {
} elsif (extra_time > 480) {
extra_time = 480;
}
if (num(extra_time) >= 60) {
@ -605,76 +609,48 @@ var radios = maketimer(1, func() {
adf1();
});
var prop_n1_left = pts.Engines.Engine.n1Actual[0];
var prop_n1_right = pts.Engines.Engine.n1Actual[1];
#var prop_nmodelat = Modes.PFD.FMA.rollMode;
#var prop_mode = Modes.PFD.FMA.pitchMode;
var prop_gs = pts.Velocities.groundspeed;
var prop_alt = pts.Instrumentation.Altimeter.indicatedFt;
var prop_state1 = pts.Systems.Thrust.state[0];
var prop_state2 = pts.Systems.Thrust.state[1];
#var prop_accel_agl_ft = Setting.reducAglFt;
var prop_gear0 = pts.Gear.wow[0];
#var prop_altSel = Input.alt;
var newphase = nil;
var masterFMGC = maketimer(0.2, func {
n1_left = prop_n1_left.getValue();
n1_right = prop_n1_right.getValue();
n1_left = pts.Engines.Engine.n1Actual[0].getValue();
n1_right = pts.Engines.Engine.n1Actual[1].getValue();
modelat = Modes.PFD.FMA.rollMode.getValue();
mode = Modes.PFD.FMA.pitchMode.getValue();
gs = prop_gs.getValue();
alt = prop_alt.getValue();
gs = pts.Velocities.groundspeed.getValue();
alt = pts.Instrumentation.Altimeter.indicatedFt.getValue();
# cruiseft = FMGCInternal.crzFt;
# cruiseft_b = FMGCInternal.crzFt - 200;
state1 = prop_state1.getValue();
state2 = prop_state2.getValue();
state1 = pts.Systems.Thrust.state[0].getValue();
state2 = pts.Systems.Thrust.state[1].getValue();
accel_agl_ft = Setting.reducAglFt.getValue();
gear0 = prop_gear0.getBoolValue();
gear0 = pts.Gear.wow[0].getValue();
altSel = Input.alt.getValue();
var phase = FMGCInternal.phase;
var newphase = phase;
if (phase == 0) {
newphase = FMGCInternal.phase;
if (FMGCInternal.phase == 0) {
if (gear0 and ((n1_left >= 85 and n1_right >= 85 and mode == "SRS") or gs >= 90)) {
newphase = 1;
systems.PNEU.pressMode.setValue("TO");
}
}
else if (phase == 1) {
} elsif (FMGCInternal.phase == 1) {
if (gear0) {
if ((n1_left < 85 or n1_right < 85) and gs < 90 and mode == " ") { # rejected takeoff
newphase = 0;
systems.PNEU.pressMode.setValue("GN");
}
}
else if (((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
} elsif (((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
newphase = 2;
systems.PNEU.pressMode.setValue("TO");
}
}
else if (phase == 2) {
} elsif (FMGCInternal.phase == 2) {
if ((mode == "ALT CRZ" or mode == "ALT CRZ*")) {
newphase = 3;
systems.PNEU.pressMode.setValue("CR");
}
}
else if (phase == 3) {
} elsif (FMGCInternal.phase == 3) {
if (FMGCInternal.crzFl >= 200) {
if ((flightPlanController.arrivalDist <= 200 or altSel < 20000)) {
newphase = 4;
@ -686,33 +662,21 @@ var masterFMGC = maketimer(0.2, func {
systems.PNEU.pressMode.setValue("DE");
}
}
}
else if (phase == 4) {
} elsif (FMGCInternal.phase == 4) {
if (getprop("/FMGC/internal/decel")) {
newphase = 5;
}
else if (altSel == (FMGCInternal.crzFl * 100)) { # back to CRZ state
elsif (altSel == (FMGCInternal.crzFl * 100)) { # back to CRZ state
newphase = 3;
systems.PNEU.pressMode.setValue("CR");
}
}
else if (phase == 5) {
} elsif (FMGCInternal.phase == 5) {
if (state1 == "TOGA" and state2 == "TOGA") {
newphase = 6;
systems.PNEU.pressMode.setValue("TO");
Input.toga.setValue(1);
}
}
else if (phase == 6) {
} elsif (FMGCInternal.phase == 6) {
if (alt >= accel_agl_ft) { # todo when insert altn or new dest
newphase = 2;
}
@ -723,7 +687,7 @@ var masterFMGC = maketimer(0.2, func {
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 pts.Position.gearAglFt.getValue() < 9500) { #todo decel pseudo waypoint
setprop("/FMGC/internal/decel", 1);
} else if (getprop("/FMGC/internal/decel") == 1 and (phase == 0 or phase == 6)) {
} elsif (getprop("/FMGC/internal/decel") == 1 and (FMGCInternal.phase == 0 or FMGCInternal.phase == 6)) {
setprop("/FMGC/internal/decel", 0);
}
@ -737,7 +701,7 @@ var masterFMGC = maketimer(0.2, func {
FMGCInternal.maxspeed = fmgc.FMGCInternal.vmo_mmo;
}
if (newphase != phase) { # phase changed
if (newphase != FMGCInternal.phase) { # phase changed
FMGCInternal.phase = newphase;
FMGCNodes.phase.setValue(newphase);
}
@ -825,7 +789,7 @@ var masterFMGC = maketimer(0.2, func {
if (!fmgc.FMGCInternal.vappSpeedSet) {
if (FMGCInternal.destWind < 5) {
FMGCInternal.vapp = FMGCInternal.vls + 5;
} else if (FMGCInternal.destWind > 15) {
} elsif (FMGCInternal.destWind > 15) {
FMGCInternal.vapp = FMGCInternal.vls + 15;
} else {
FMGCInternal.vapp = FMGCInternal.vls + FMGCInternal.destWind;
@ -833,7 +797,7 @@ var masterFMGC = maketimer(0.2, func {
}
# predicted takeoff speeds
if (phase == 1) {
if (FMGCInternal.phase == 1) {
FMGCInternal.clean_to = FMGCInternal.clean;
FMGCInternal.vs1g_clean_to = FMGCInternal.vs1g_clean;
FMGCInternal.vs1g_conf_2_to = FMGCInternal.vs1g_conf_2;
@ -855,7 +819,7 @@ var masterFMGC = maketimer(0.2, func {
}
# predicted approach (temp go-around) speeds
if (phase == 5 or phase == 6) {
if (FMGCInternal.phase == 5 or FMGCInternal.phase == 6) {
FMGCInternal.clean_appr = FMGCInternal.clean;
FMGCInternal.vs1g_clean_appr = FMGCInternal.vs1g_clean;
FMGCInternal.vs1g_conf_2_appr = FMGCInternal.vs1g_conf_2;
@ -889,7 +853,7 @@ var masterFMGC = maketimer(0.2, func {
if (!fmgc.FMGCInternal.vappSpeedSet) {
if (FMGCInternal.destWind < 5) {
FMGCInternal.vapp_appr = FMGCInternal.vls_appr + 5;
} else if (FMGCInternal.destWind > 15) {
} elsif (FMGCInternal.destWind > 15) {
FMGCInternal.vapp_appr = FMGCInternal.vls_appr + 15;
} else {
FMGCInternal.vapp_appr = FMGCInternal.vls_appr + FMGCInternal.destWind;
@ -925,7 +889,7 @@ var masterFMGC = maketimer(0.2, func {
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_clean * 1.23;
}
} else if (flap == 1) { # 1
} elsif (flap == 1) { # 1
FMGCInternal.vsw = FMGCInternal.vs1g_conf_2;
FMGCInternal.minspeed = FMGCInternal.slat;
@ -934,7 +898,7 @@ var masterFMGC = maketimer(0.2, func {
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_1 * 1.23;
}
} else if (flap == 2) { # 1+F
} elsif (flap == 2) { # 1+F
FMGCInternal.vsw = FMGCInternal.vs1g_conf_1f;
FMGCInternal.minspeed = FMGCInternal.slat;
@ -943,7 +907,7 @@ var masterFMGC = maketimer(0.2, func {
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_1f * 1.23;
}
} else if (flap == 3) { # 2
} elsif (flap == 3) { # 2
FMGCInternal.vsw = FMGCInternal.vs1g_conf_2;
FMGCInternal.minspeed = FMGCInternal.flap2;
@ -952,7 +916,7 @@ var masterFMGC = maketimer(0.2, func {
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_2 * 1.23;
}
} else if (flap == 4) { # 3
} elsif (flap == 4) { # 3
FMGCInternal.vsw = FMGCInternal.vs1g_conf_3;
FMGCInternal.minspeed = FMGCInternal.flap3;
@ -961,7 +925,7 @@ var masterFMGC = maketimer(0.2, func {
} else {
FMGCInternal.vls_min = FMGCInternal.vs1g_conf_3 * 1.23;
}
} else if (flap == 5) { # FULL
} elsif (flap == 5) { # FULL
FMGCInternal.vsw = FMGCInternal.vs1g_conf_full;
if (FMGCInternal.vappSpeedSet) {
FMGCInternal.minspeed = FMGCInternal.vapp_appr;
@ -976,7 +940,6 @@ var masterFMGC = maketimer(0.2, func {
}
}
#if (gear0 and pts.Controls.Flight.flapsPos.getValue() < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
if (gear0 and flap < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
if (!FMGCInternal.takeoffState) {
fmgc.FMGCNodes.toState.setValue(1);
@ -994,49 +957,47 @@ var masterFMGC = maketimer(0.2, func {
############################
#handle radios, runways, v1/vr/v2
############################
var airportRadiosPhase = nil;
var updateAirportRadios = func {
var phase = FMGCInternal.phase;
print("# Update airport radios");
airportRadiosPhase = FMGCInternal.phase;
departure_rwy = fmgc.flightPlanController.flightplans[2].departure_runway;
destination_rwy = fmgc.flightPlanController.flightplans[2].destination_runway;
if (phase >= 2 and destination_rwy != nil) {
if (airportRadiosPhase >= 2 and destination_rwy != nil) {
var airport = airportinfo(FMGCInternal.arrApt);
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("/instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
setprop("/instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
} elsif (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);
setprop("/instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
} elsif (!getprop("/FMGC/internal/ils1crs-set")) {
setprop("/instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
}
} else if (phase <= 1 and departure_rwy != nil) {
} elsif (airportRadiosPhase <= 1 and departure_rwy != nil) {
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("/instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
setprop("/instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
} elsif (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);
setprop("/instrumentation/nav[0]/frequencies/selected-mhz", runway_ils);
} elsif (!getprop("/FMGC/internal/ils1crs-set")) {
setprop("/instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
}
}
};
setlistener(FMGCNodes.phase, updateAirportRadios,0,0);
setlistener(flightPlanController.changed, updateAirportRadios);
setlistener(flightPlanController.changed, updateAirportRadios,0,0);
var reset_FMGC = func {
FMGCInternal.phase = 0;
@ -1054,6 +1015,7 @@ var reset_FMGC = func {
windController.init();
mcdu.MCDU_reset(0);
mcdu.MCDU_reset(1);
Simbrief.SimbriefParser.inhibit = 0;
mcdu.ReceivedMessagesDatabase.clearDatabase();
mcdu.FlightLogDatabase.reset(); # track reset events without loosing recorded data
@ -1118,59 +1080,59 @@ var ManagedSPD = maketimer(0.25, func {
if (FMGCInternal.mngSpdCmd != srsSPD) {
FMGCInternal.mngSpdCmd = srsSPD;
}
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude <= 10050) {
} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude <= 10050) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (FMGCInternal.mngSpdCmd != 250 and !decel) {
FMGCInternal.mngSpdCmd = 250;
} else if (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
} elsif (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
}
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and !FMGCInternal.machSwitchover) {
} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and !FMGCInternal.machSwitchover) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (FMGCInternal.mngSpdCmd != mng_alt_spd) {
FMGCInternal.mngSpdCmd = mng_alt_spd;
}
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and FMGCInternal.machSwitchover) {
} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and FMGCInternal.machSwitchover) {
if (!FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 1;
}
if (FMGCInternal.mngSpdCmd != mng_alt_mach) {
FMGCInternal.mngSpdCmd = mng_alt_mach;
}
} else if (FMGCInternal.phase == 4 and altitude > 11000 and !FMGCInternal.machSwitchover) {
} elsif (FMGCInternal.phase == 4 and altitude > 11000 and !FMGCInternal.machSwitchover) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (FMGCInternal.mngSpdCmd != mng_alt_spd) {
FMGCInternal.mngSpdCmd = mng_alt_spd;
}
} else if (FMGCInternal.phase == 4 and altitude > 11000 and FMGCInternal.machSwitchover) {
} elsif (FMGCInternal.phase == 4 and altitude > 11000 and FMGCInternal.machSwitchover) {
if (!FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 1;
}
if (FMGCInternal.mngSpdCmd != mng_alt_mach) {
FMGCInternal.mngSpdCmd = mng_alt_mach;
}
} else if ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude > 11000 and !FMGCInternal.machSwitchover) {
} elsif ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude > 11000 and !FMGCInternal.machSwitchover) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (FMGCInternal.mngSpdCmd != mng_alt_spd and !decel) {
FMGCInternal.mngSpdCmd = mng_alt_spd;
} else if (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
} elsif (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
}
} else if ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude <= 10980) {
} elsif ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude <= 10980) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (FMGCInternal.mngSpdCmd != 250 and !decel) {
FMGCInternal.mngSpdCmd = 250;
} else if (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
} elsif (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
}
}
@ -1183,13 +1145,13 @@ var ManagedSPD = maketimer(0.25, func {
if (ktsmach and !FMGCInternal.mngKtsMach) {
Input.ktsMach.setValue(0);
} else if (!ktsmach and FMGCInternal.mngKtsMach) {
} elsif (!ktsmach and FMGCInternal.mngKtsMach) {
Input.ktsMach.setValue(1);
}
if (kts_sel != FMGCInternal.mngSpd and !ktsmach) {
Input.kts.setValue(FMGCInternal.mngSpd);
} else if (mach_sel != FMGCInternal.mngSpd and ktsmach) {
} elsif (mach_sel != FMGCInternal.mngSpd and ktsmach) {
Input.mach.setValue(FMGCInternal.mngSpd);
}
} else {
@ -1231,9 +1193,9 @@ setlistener("/systems/navigation/adr/operating-1", func() {
timer48gpsAlign1.stop();
}
if (getprop("/FMGC/internal/align1-time") == -99) {
if (FMGCAlignTime[0].getValue() == -99) {
timer48gpsAlign1.start();
setprop("/FMGC/internal/align1-time", pts.Sim.Time.elapsedSec.getValue());
FMGCAlignTime[0].setValue(pts.Sim.Time.elapsedSec.getValue());
}
}, 0, 0);
@ -1243,9 +1205,9 @@ setlistener("/systems/navigation/adr/operating-2", func() {
timer48gpsAlign2.stop();
}
if (getprop("/FMGC/internal/align2-time") == -99) {
if (FMGCAlignTime[1].getValue() == -99) {
timer48gpsAlign2.start();
setprop("/FMGC/internal/align2-time", pts.Sim.Time.elapsedSec.getValue());
FMGCAlignTime[1].setValue(pts.Sim.Time.elapsedSec.getValue());
}
}, 0, 0);
@ -1255,9 +1217,9 @@ setlistener("/systems/navigation/adr/operating-3", func() {
timer48gpsAlign3.stop();
}
if (getprop("/FMGC/internal/align3-time") == -99) {
if (FMGCAlignTime[2].getValue() == -99) {
timer48gpsAlign3.start();
setprop("/FMGC/internal/align3-time", pts.Sim.Time.elapsedSec.getValue());
FMGCAlignTime[2].setValue(pts.Sim.Time.elapsedSec.getValue());
}
}, 0, 0);
@ -1304,25 +1266,25 @@ var timer30secLanding = maketimer(1, func() {
});
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);
if (pts.Sim.Time.elapsedSec.getValue() > (FMGCAlignTime[0].getValue() + 48) or adirsSkip.getValue()) {
FMGCAlignDone[0].setValue(1);
FMGCAlignTime[0].setValue(-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);
if (pts.Sim.Time.elapsedSec.getValue() > (FMGCAlignTime[1].getValue() + 48) or adirsSkip.getValue()) {
FMGCAlignDone[1].setValue(1);
FMGCAlignTime[1].setValue(-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);
if (pts.Sim.Time.elapsedSec.getValue() > (FMGCAlignTime[2].getValue() + 48) or adirsSkip.getValue()) {
FMGCAlignDone[2].setValue(1);
FMGCAlignTime[2].setValue(-99);
timer48gpsAlign3.stop();
}
});