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Transfer much of managed speed loop to nodes or variables -- much faster!

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This commit is contained in:
legoboyvdlp R 2020-10-05 19:18:10 +01:00
parent 1cbf30e638
commit 16df254d13
5 changed files with 153 additions and 203 deletions
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24
Models/Instruments/MCDU/MCDU.nas
View file

@ -3369,7 +3369,7 @@ var canvas_MCDU_base = {
me.fontLeft(0, 0, 0, symbol, 0, 0);
} else {
me["Simple_L1"].setText("SELECTED");
if (getprop("/it-autoflight/input/kts-mach")) {
if (fmgc.Input.ktsMach.getValue()) {
me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/mach")));
} else {
me["Simple_L4"].setText(sprintf(" %s", int(getprop("/it-autoflight/input/kts"))));
@ -3387,10 +3387,10 @@ var canvas_MCDU_base = {
}
me["Simple_L3S"].setText(" MANAGED");
if (getprop("/it-autoflight/input/kts-mach")) {
me["Simple_L3"].setText(sprintf(" %3.3f", getprop("/FMGC/internal/mng-spd")));
if (fmgc.Input.ktsMach.getValue()) {
me["Simple_L3"].setText(sprintf(" %3.3f", fmgc.FMGCInternal.mngSpd));
} else {
me["Simple_L3"].setText(sprintf(" %s", int(getprop("/FMGC/internal/mng-spd"))));
me["Simple_L3"].setText(sprintf(" %s", int(fmgc.FMGCInternal.mngSpd)));
}
me["Simple_L5S"].setText(" EXPEDITE");
@ -3510,7 +3510,7 @@ var canvas_MCDU_base = {
me.fontLeft(0, 0, 0, symbol, 0, 0);
} else {
me["Simple_L1"].setText("SELECTED");
if (getprop("/it-autoflight/input/kts-mach")) {
if (fmgc.Input.ktsMach.getValue()) {
me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/mach")));
} else {
me["Simple_L4"].setText(sprintf(" %s", int(getprop("/it-autoflight/input/kts"))));
@ -3530,10 +3530,10 @@ var canvas_MCDU_base = {
me["Simple_L2S"].setText(" CI");
me["Simple_L3S"].setText(" MANAGED");
if (getprop("/it-autoflight/input/kts-mach")) {
me["Simple_L3"].setText(sprintf(" %3.3f", getprop("/FMGC/internal/mng-spd")));
if (fmgc.Input.ktsMach.getValue()) {
me["Simple_L3"].setText(sprintf(" %3.3f", fmgc.FMGCInternal.mngSpd));
} else {
me["Simple_L3"].setText(sprintf(" %s", int(getprop("/FMGC/internal/mng-spd"))));
me["Simple_L3"].setText(sprintf(" %s", int(fmgc.FMGCInternal.mngSpd)));
}
me["Simple_R1S"].setText("DEST EFOB");
@ -3658,7 +3658,7 @@ var canvas_MCDU_base = {
me.fontLeft(0, 0, 0, symbol, 0, 0);
} else {
me["Simple_L1"].setText("SELECTED");
if (getprop("/it-autoflight/input/kts-mach")) {
if (fmgc.Input.ktsMach.getValue()) {
me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/mach")));
} else {
me["Simple_L4"].setText(sprintf(" %3.0f", getprop("/it-autoflight/input/kts")));
@ -3678,10 +3678,10 @@ var canvas_MCDU_base = {
me["Simple_L2S"].setText(" CI");
me["Simple_L3S"].setText(" MANAGED");
if (getprop("/it-autoflight/input/kts-mach")) {
me["Simple_L3"].setText(sprintf(" %3.3f", getprop("/FMGC/internal/mng-spd")));
if (fmgc.Input.ktsMach.getValue()) {
me["Simple_L3"].setText(sprintf(" %3.3f", fmgc.FMGCInternal.mngSpd));
} else {
me["Simple_L3"].setText(sprintf(" %3.0f", getprop("/FMGC/internal/mng-spd")));
me["Simple_L3"].setText(sprintf(" %3.0f", fmgc.FMGCInternal.mngSpd));
}
me["Simple_L5"].setText(" EXPEDITE");

6
Nasal/ECAM/ECAM-logic.nas
View file

@ -2069,7 +2069,7 @@ var messages_config_memo = func {
toMemoLine3.colour = "c";
}
if (getprop("/controls/flight/flaps-pos") > 0 and getprop("/controls/flight/flaps-pos") < 5) {
if (pts.Controls.Flight.flapsPos.getValue() > 0 and pts.Controls.Flight.flapsPos.getValue() < 5) {
toMemoLine4.msg = " FLAPS T.O";
toMemoLine4.colour = "g";
} else {
@ -2136,7 +2136,7 @@ var messages_config_memo = func {
}
if (getprop("it-fbw/law") == 1 or getprop("instrumentation/mk-viii/inputs/discretes/momentary-flap-3-override")) {
if (getprop("/controls/flight/flaps-pos") == 4) {
if (pts.Controls.Flight.flapsPos.getValue() == 4) {
ldgMemoLine4.msg = " FLAPS CONF 3";
ldgMemoLine4.colour = "g";
} else {
@ -2144,7 +2144,7 @@ var messages_config_memo = func {
ldgMemoLine4.colour = "c";
}
} else {
if (getprop("/controls/flight/flaps-pos") == 5) {
if (pts.Controls.Flight.flapsPos.getValue() == 5) {
ldgMemoLine4.msg = " FLAPS FULL";
ldgMemoLine4.colour = "g";
} else {

323
Nasal/FMGC/FMGC.nas
View file

@ -12,31 +12,18 @@ var code2 = 0;
var gear0 = 0;
var state1 = 0;
var state2 = 0;
var flaps = 0;
var dep = "";
var arr = "";
var n1_left = 0;
var n1_right = 0;
var flaps = 0;
var modelat = 0;
var mode = 0;
var modeI = 0;
var gs = 0;
var aglalt = 0;
var cruiseft = 0;
var cruiseft_b = 0;
var newcruise = 0;
var phase = 0;
var state1 = 0;
var state2 = 0;
var wowl = 0;
var wowr = 0;
var targetalt = 0;
var targetvs = 0;
var targetfpa = 0;
var accel_agl_ft = 0;
var locarm = 0;
var apprarm = 0;
var fd1 = 0;
var fd2 = 0;
var spd = 0;
@ -65,37 +52,17 @@ var nameadf1 = "XX";
var ias = 0;
var mach = 0;
var ktsmach = 0;
var mngktsmach = 0;
var mng_spd = 0;
var mng_spd_cmd = 0;
var kts_sel = 0;
var mach_sel = 0;
var srsSPD = 0;
var mach_switchover = 0;
var decel = 0;
var mng_alt_spd_cmd = 0;
var mng_alt_spd = 0;
var mng_alt_mach_cmd = 0;
var mng_alt_mach = 0;
var mng_spd_cmd = 0;
var mng_spd = 0;
var ap1 = 0;
var ap2 = 0;
var flx = 0;
var lat = 0;
var newlat = 0;
var vert = 0;
var newvert = 0;
var newvertarm = 0;
var thr1 = 0;
var thr2 = 0;
var altsel = 0;
var crzFl = 0;
var windHdg = 0;
var windSpeed = 0;
setprop("position/gear-agl-ft", 0);
setprop("/FMGC/internal/mng-spd", 157);
setprop("/FMGC/internal/mng-spd-cmd", 157);
setprop("/FMGC/internal/mng-kts-mach", 0);
setprop("/FMGC/internal/mach-switchover", 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);
@ -116,10 +83,10 @@ var FMGCinit = func {
FMGCInternal.minspeed = 0;
FMGCInternal.maxspeed = 338;
FMGCInternal.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
setprop("/FMGC/internal/mng-spd", 157);
setprop("/FMGC/internal/mng-spd-cmd", 157);
setprop("/FMGC/internal/mng-kts-mach", 0);
setprop("/FMGC/internal/mach-switchover", 0);
FMGCInternal.mngSpd = 157;
FMGCInternal.mngSpdCmd = 157;
FMGCInternal.mngKtsMach = 0;
FMGCInternal.machSwitchover = 0;
setprop("/FMGC/internal/loc-source", "NAV0");
setprop("/FMGC/internal/optalt", 0);
setprop("/FMGC/internal/landing-time", -99);
@ -261,6 +228,13 @@ var FMGCInternal = {
fob: 0,
fuelPredGw: 0,
cg: 0,
# Managed Speed
machSwitchover: 0,
mngKtsMach: 0,
mngSpd: 0,
mngSpdCmd: 0,
};
var postInit = func() {
@ -273,10 +247,12 @@ var postInit = func() {
var FMGCNodes = {
costIndex: props.globals.initNode("/FMGC/internal/cost-index", 0, "DOUBLE"),
flexSet: props.globals.initNode("/FMGC/internal/flex-set", 0, "BOOL"),
mngSpdAlt: props.globals.getNode("/FMGC/internal/mng-alt-spd"),
mngMachAlt: props.globals.getNode("/FMGC/internal/mng-alt-mach"),
toFromSet: props.globals.initNode("/FMGC/internal/tofrom-set", 0, "BOOL"),
toState: props.globals.initNode("/FMGC/internal/to-state", 0, "BOOL"),
v1: props.globals.initNode("/FMGC/internal/v1", 0, "DOUBLE"),
v1set: props.globals.initNode("/FMGC/internal/v1-set", 0, "BOOL"),
toState: props.globals.initNode("/FMGC/internal/to-state", 0, "BOOL"),
};
############
@ -623,69 +599,47 @@ var radios = maketimer(1, func() {
var masterFMGC = maketimer(0.2, func {
n1_left = pts.Engines.Engine.n1Actual[0].getValue();
n1_right = pts.Engines.Engine.n1Actual[1].getValue();
flaps = getprop("/controls/flight/flaps-pos");
modelat = getprop("/modes/pfd/fma/roll-mode");
mode = getprop("/modes/pfd/fma/pitch-mode");
modeI = getprop("/it-autoflight/mode/vert");
gs = getprop("/velocities/groundspeed-kt");
alt = getprop("/instrumentation/altimeter/indicated-altitude-ft");
aglalt = pts.Position.gearAglFt.getValue();
modelat = Modes.PFD.FMA.rollMode.getValue();
mode = Modes.PFD.FMA.pitchMode.getValue();
gs = pts.Velocities.groundspeed.getValue();
alt = pts.Instrumentation.Altimeter.indicatedFt.getValue();
# cruiseft = FMGCInternal.crzFt;
# cruiseft_b = FMGCInternal.crzFt - 200;
newcruise = getprop("/it-autoflight/internal/alt");
phase = FMGCInternal.phase;
state1 = getprop("/systems/thrust/state1");
state2 = getprop("/systems/thrust/state2");
wowl = getprop("/gear/gear[1]/wow");
wowr = getprop("/gear/gear[2]/wow");
targetalt = getprop("/it-autoflight/internal/alt");
targetvs = getprop("/it-autoflight/input/vs");
targetfpa = getprop("/it-autoflight/input/fpa");
accel_agl_ft = getprop("/it-autoflight/settings/accel-agl-ft");
locarm = getprop("/it-autopilot/output/loc-armed");
apprarm = getprop("/it-autopilot/output/appr-armed");
state1 = pts.Systems.Thrust.state[0].getValue();
state2 = pts.Systems.Thrust.state[1].getValue();
accel_agl_ft = Setting.reducAglFt.getValue();
gear0 = pts.Gear.wow[0].getBoolValue();
ap1 = getprop("/it-autoflight/output/ap1");
ap2 = getprop("/it-autoflight/output/ap2");
flx = getprop("/systems/thrust/lim-flex");
lat = getprop("/it-autoflight/mode/lat");
newlat = getprop("/modes/pfd/fma/roll-mode");
vert = getprop("/it-autoflight/mode/vert");
newvert = getprop("/modes/pfd/fma/pitch-mode");
newvertarm = getprop("/modes/pfd/fma/pitch-mode2-armed");
thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
altSel = getprop("/it-autoflight/input/alt");
altSel = Input.alt.getValue();
if ((n1_left < 85 or n1_right < 85) and gs < 90 and mode == " " and gear0 and FMGCInternal.phase == 1) { # rejected takeoff
FMGCInternal.phase = 0;
setprop("/systems/pressurization/mode", "GN");
systems.PNEU.pressMode.setValue("GN");
}
if (gear0 and FMGCInternal.phase == 0 and ((n1_left >= 85 and n1_right >= 85 and mode == "SRS") or gs >= 90)) {
FMGCInternal.phase = 1;
setprop("/systems/pressurization/mode", "TO");
systems.PNEU.pressMode.setValue("TO");
}
if (FMGCInternal.phase == 1 and ((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
FMGCInternal.phase = 2;
setprop("/systems/pressurization/mode", "TO");
systems.PNEU.pressMode.setValue("TO");
}
if (FMGCInternal.phase == 2 and (mode == "ALT CRZ" or mode == "ALT CRZ*")) {
FMGCInternal.phase = 3;
setprop("/systems/pressurization/mode", "CR");
systems.PNEU.pressMode.setValue("CR");
}
if (FMGCInternal.crzFl >= 200) {
if (FMGCInternal.phase == 3 and (flightPlanController.arrivalDist <= 200 or altSel < 20000)) {
FMGCInternal.phase = 4;
setprop("/systems/pressurization/mode", "DE");
systems.PNEU.pressMode.setValue("DE");
}
} else {
if (FMGCInternal.phase == 3 and (flightPlanController.arrivalDist <= 200 or altSel < (FMGCInternal.crzFl * 100))) { # todo - not sure about crzFl condition, investigate what happens!
FMGCInternal.phase = 4;
setprop("/systems/pressurization/mode", "DE");
systems.PNEU.pressMode.setValue("DE");
}
}
@ -693,7 +647,7 @@ var masterFMGC = maketimer(0.2, func {
FMGCInternal.phase = 5;
}
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
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 (FMGCInternal.phase == 0 or FMGCInternal.phase == 6)) {
setprop("/FMGC/internal/decel", 0);
@ -701,8 +655,8 @@ var masterFMGC = maketimer(0.2, func {
if ((FMGCInternal.phase == 5) and state1 == "TOGA" and state2 == "TOGA") {
FMGCInternal.phase = 6;
setprop("/systems/pressurization/mode", "TO");
setprop("/it-autoflight/input/toga", 1);
systems.PNEU.pressMode.setValue("TO");
Input.toga.setValue(1);
}
if (FMGCInternal.phase == 6 and alt >= accel_agl_ft) { # todo when insert altn or new dest
@ -725,36 +679,38 @@ var masterFMGC = maketimer(0.2, func {
############################
# wind
############################
windHdg = pts.Environment.windFromHdg.getValue();
windSpeed = pts.Environment.windSpeedKt.getValue();
if (FMGCInternal.phase == 3 or FMGCInternal.phase == 4 or FMGCInternal.phase == 6) {
var windsDidChange = 0;
if (FMGCInternal.crzFt > 5000 and alt > 4980 and alt < 5020) {
if (sprintf("%03d", getprop("/environment/wind-from-heading-deg/")) != fmgc.windController.fl50_wind[0] or sprintf("%03d", getprop("/environment/wind-speed-kt/")) != fmgc.windController.fl50_wind[1]) {
fmgc.windController.fl50_wind[0] = sprintf("%03d", getprop("/environment/wind-from-heading-deg/"));
fmgc.windController.fl50_wind[1] = sprintf("%03d", getprop("/environment/wind-speed-kt/"));
if (sprintf("%03d", windHdg) != fmgc.windController.fl50_wind[0] or sprintf("%03d", windSpeed) != fmgc.windController.fl50_wind[1]) {
fmgc.windController.fl50_wind[0] = sprintf("%03d", windHdg);
fmgc.windController.fl50_wind[1] = sprintf("%03d", windSpeed);
fmgc.windController.fl50_wind[2] = "FL50";
windsDidChange = 1;
}
}
if (FMGCInternal.crzFt > 15000 and alt > 14980 and alt < 15020) {
if (sprintf("%03d", getprop("/environment/wind-from-heading-deg/")) != fmgc.windController.fl150_wind[0] or sprintf("%03d", getprop("/environment/wind-speed-kt/")) != fmgc.windController.fl150_wind[1]) {
fmgc.windController.fl150_wind[0] = sprintf("%03d", getprop("/environment/wind-from-heading-deg/"));
fmgc.windController.fl150_wind[1] = sprintf("%03d", getprop("/environment/wind-speed-kt/"));
if (sprintf("%03d", windHdg) != fmgc.windController.fl150_wind[0] or sprintf("%03d", windSpeed) != fmgc.windController.fl150_wind[1]) {
fmgc.windController.fl150_wind[0] = sprintf("%03d", windHdg);
fmgc.windController.fl150_wind[1] = sprintf("%03d", windSpeed);
fmgc.windController.fl150_wind[2] = "FL150";
windsDidChange = 1;
}
}
if (FMGCInternal.crzFt > 25000 and alt > 24980 and alt < 25020) {
if (sprintf("%03d", getprop("/environment/wind-from-heading-deg/")) != fmgc.windController.fl250_wind[0] or sprintf("%03d", getprop("/environment/wind-speed-kt/")) != fmgc.windController.fl250_wind[1]) {
fmgc.windController.fl250_wind[0] = sprintf("%03d", getprop("/environment/wind-from-heading-deg/"));
fmgc.windController.fl250_wind[1] = sprintf("%03d", getprop("/environment/wind-speed-kt/"));
if (sprintf("%03d", windHdg) != fmgc.windController.fl250_wind[0] or sprintf("%03d", windSpeed) != fmgc.windController.fl250_wind[1]) {
fmgc.windController.fl250_wind[0] = sprintf("%03d", windHdg);
fmgc.windController.fl250_wind[1] = sprintf("%03d", windSpeed);
fmgc.windController.fl250_wind[2] = "FL250";
windsDidChange = 1;
}
}
if (FMGCInternal.crzSet and alt > FMGCInternal.crzFt - 20 and alt < FMGCInternal.crzFt + 20) {
if (sprintf("%03d", getprop("/environment/wind-from-heading-deg/")) != fmgc.windController.flcrz_wind[0] or sprintf("%03d", getprop("/environment/wind-speed-kt/")) != fmgc.windController.flcrz_wind[1]) {
fmgc.windController.flcrz_wind[0] = sprintf("%03d", getprop("/environment/wind-from-heading-deg/"));
fmgc.windController.flcrz_wind[1] = sprintf("%03d", getprop("/environment/wind-speed-kt/"));
if (sprintf("%03d", windHdg) != fmgc.windController.flcrz_wind[0] or sprintf("%03d", windSpeed) != fmgc.windController.flcrz_wind[1]) {
fmgc.windController.flcrz_wind[0] = sprintf("%03d", windHdg);
fmgc.windController.flcrz_wind[1] = sprintf("%03d", windSpeed);
fmgc.windController.flcrz_wind[2] = "FL" ~ FMGCInternal.crzFl;
windsDidChange = 1;
}
@ -767,9 +723,9 @@ var masterFMGC = maketimer(0.2, func {
############################
# calculate speeds
############################
flap = getprop("/controls/flight/flaps-pos");
flap = pts.Controls.Flight.flapsPos.getValue();
weight_lbs = pts.Fdm.JSBsim.Inertia.weightLbs.getValue() / 1000;
altitude = getprop("/instrumentation/altimeter/indicated-altitude-ft");
altitude = pts.Instrumentation.Altimeter.indicatedFt.getValue();
# current speeds
FMGCInternal.clean = 2 * weight_lbs * 0.45359237 + 85;
@ -943,7 +899,7 @@ var masterFMGC = maketimer(0.2, func {
}
}
if (gear0 and flaps < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
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 (!FMGCInternal.takeoffState) {
fmgc.FMGCNodes.toState.setValue(1);
}
@ -961,7 +917,7 @@ var masterFMGC = maketimer(0.2, func {
departure_rwy = fmgc.flightPlanController.flightplans[2].departure_runway;
destination_rwy = fmgc.flightPlanController.flightplans[2].destination_runway;
if (destination_rwy != nil and phase >= 2) {
if (destination_rwy != nil and FMGCInternal.phase >= 2) {
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"));
@ -976,7 +932,7 @@ var masterFMGC = maketimer(0.2, func {
} else if (!getprop("/FMGC/internal/ils1crs-set")) {
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
}
} else if (departure_rwy != nil and phase <= 1) {
} else if (departure_rwy != nil and FMGCInternal.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")) {
@ -994,25 +950,28 @@ var masterFMGC = maketimer(0.2, func {
var reset_FMGC = func {
FMGCInternal.phase = 0;
fd1 = getprop("/it-autoflight/input/fd1");
fd2 = getprop("/it-autoflight/input/fd2");
spd = getprop("/it-autoflight/input/kts");
hdg = getprop("/it-autoflight/input/hdg");
alt = getprop("/it-autoflight/input/alt");
fd1 = Input.fd1.getValue();
fd2 = Input.fd2.getValue()
spd = Input.spd.getValue();
hdg = Input.hdg.getValue();
alt = Input.alt.getValue();
ITAF.init();
FMGCinit();
flightPlanController.reset();
windController.reset();
windController.init();
mcdu.MCDU_reset(0);
mcdu.MCDU_reset(1);
setprop("it-autoflight/input/fd1", fd1);
setprop("it-autoflight/input/fd2", fd2);
setprop("it-autoflight/input/kts", spd);
setprop("it-autoflight/input/hdg", hdg);
setprop("it-autoflight/input/alt", alt);
setprop("/systems/pressurization/mode", "GN");
mcdu.ReceivedMessagesDatabase.clearDatabase();
Input.fd1.setValue(fd1);
Input.fd2.setValue(fd2);
Input.kts.setValue(spd);
Input.hdg.setValue(hdg);
Input.alt.setValue(alt);
systems.PNEU.pressMode.setValue("GN");
setprop("/systems/pressurization/vs", "0");
setprop("/systems/pressurization/targetvs", "0");
setprop("/systems/pressurization/vs-norm", "0");
@ -1021,7 +980,7 @@ var reset_FMGC = func {
setprop("/systems/pressurization/outflowpos", "0");
setprop("/systems/pressurization/deltap-norm", "0");
setprop("/systems/pressurization/outflowpos-norm", "0");
altitude = getprop("/instrumentation/altimeter/indicated-altitude-ft");
altitude = pts.Instrumentation.Altimeter.indicatedFt.getValue();
setprop("/systems/pressurization/cabinalt", altitude);
setprop("/systems/pressurization/targetalt", altitude);
setprop("/systems/pressurization/diff-to-target", "0");
@ -1030,7 +989,6 @@ var reset_FMGC = func {
setprop("/systems/pressurization/ambientpsi", "0");
setprop("/systems/pressurization/cabinpsi", "0");
mcdu.ReceivedMessagesDatabase.clearDatabase();
}
#################
@ -1039,121 +997,110 @@ var reset_FMGC = func {
var ManagedSPD = maketimer(0.25, func {
if (FMGCInternal.crzSet and FMGCInternal.costIndexSet) {
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/kts");
mach_sel = getprop("/it-autoflight/input/mach");
if (Custom.Input.spdManaged.getBoolValue()) {
altitude = pts.Instrumentation.Altimeter.indicatedFt.getValue();
mode = Modes.PFD.FMA.pitchMode.getValue();
ias = pts.Instrumentation.AirspeedIndicator.indicatedSpdKt.getValue();
mach = pts.Instrumentation.AirspeedIndicator.indicatedMach.getValue();
ktsmach = Input.ktsMach.getValue();
kts_sel = Input.kts.getValue();
mach_sel = Input.mach.getValue();
srsSPD = getprop("/it-autoflight/settings/togaspd");
phase = FMGCInternal.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/flaps-pos");
mach_switchover = getprop("/FMGC/internal/mach-switchover");
flap = pts.Controls.Flight.flapsPos.getValue();
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);
mng_alt_spd = math.round(FMGCNodes.mngSpdAlt.getValue(), 1);
mng_alt_mach = math.round(FMGCNodes.mngMachAlt.getValue(), 0.001);
if (mach > mng_alt_mach and (FMGCInternal.phase == 2 or FMGCInternal.phase == 3)) {
setprop("/FMGC/internal/mach-switchover", 1);
FMGCInternal.machSwitchover = 1;
}
if (ias > mng_alt_spd and (FMGCInternal.phase == 4 or FMGCInternal.phase == 5)) {
setprop("/FMGC/internal/mach-switchover", 0);
FMGCInternal.machSwitchover = 0;
}
if ((mode == " " or mode == "SRS") and (FMGCInternal.phase == 0 or FMGCInternal.phase == 1)) {
if (mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 0);
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (mng_spd_cmd != srsSPD) {
setprop("/FMGC/internal/mng-spd-cmd", srsSPD);
if (FMGCInternal.mngSpdCmd != srsSPD) {
FMGCInternal.mngSpdCmd = srsSPD;
}
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude <= 10050) {
if (mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 0);
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (mng_spd_cmd != 250 and !decel) {
setprop("/FMGC/internal/mng-spd-cmd", 250);
} else if (mng_spd_cmd != FMGCInternal.minspeed and decel) {
setprop("/FMGC/internal/mng-spd-cmd", FMGCInternal.minspeed);
if (FMGCInternal.mngSpdCmd != 250 and !decel) {
FMGCInternal.mngSpdCmd = 250;
} else if (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
}
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and !mach_switchover) {
if (mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 0);
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and !FMGCInternal.machSwitchover) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (mng_spd_cmd != mng_alt_spd) {
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
if (FMGCInternal.mngSpdCmd != mng_alt_spd) {
FMGCInternal.mngSpdCmd = mng_alt_spd;
}
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and mach_switchover) {
if (!mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 1);
} else if ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and FMGCInternal.machSwitchover) {
if (!FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 1;
}
if (mng_spd_cmd != mng_alt_mach) {
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
if (FMGCInternal.mngSpdCmd != mng_alt_mach) {
FMGCInternal.mngSpdCmd = mng_alt_mach;
}
} else if (FMGCInternal.phase == 4 and altitude > 11000 and !mach_switchover) {
if (mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 0);
} else if (FMGCInternal.phase == 4 and altitude > 11000 and !FMGCInternal.machSwitchover) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (mng_spd_cmd != mng_alt_spd) {
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
if (FMGCInternal.mngSpdCmd != mng_alt_spd) {
FMGCInternal.mngSpdCmd = mng_alt_spd;
}
} else if (FMGCInternal.phase == 4 and altitude > 11000 and mach_switchover) {
if (!mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 1);
} else if (FMGCInternal.phase == 4 and altitude > 11000 and FMGCInternal.machSwitchover) {
if (!FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 1;
}
if (mng_spd_cmd != mng_alt_mach) {
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_mach);
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 !mach_switchover) {
if (mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 0);
} else if ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude > 11000 and !FMGCInternal.machSwitchover) {
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (mng_spd_cmd != mng_alt_spd and !decel) {
setprop("/FMGC/internal/mng-spd-cmd", mng_alt_spd);
} else if (mng_spd_cmd != FMGCInternal.minspeed and decel) {
setprop("/FMGC/internal/mng-spd-cmd", FMGCInternal.minspeed);
if (FMGCInternal.mngSpdCmd != mng_alt_spd and !decel) {
FMGCInternal.mngSpdCmd = mng_alt_spd;
} else if (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) {
if (mngktsmach) {
setprop("/FMGC/internal/mng-kts-mach", 0);
if (FMGCInternal.mngKtsMach) {
FMGCInternal.mngKtsMach = 0;
}
if (mng_spd_cmd != 250 and !decel) {
setprop("/FMGC/internal/mng-spd-cmd", 250);
} else if (mng_spd_cmd != FMGCInternal.minspeed and decel) {
setprop("/FMGC/internal/mng-spd-cmd", FMGCInternal.minspeed);
if (FMGCInternal.mngSpdCmd != 250 and !decel) {
FMGCInternal.mngSpdCmd = 250;
} else if (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
}
}
mng_spd_cmd = getprop("/FMGC/internal/mng-spd-cmd");
if (mng_spd_cmd > FMGCInternal.maxspeed - 5) {
setprop("/FMGC/internal/mng-spd", FMGCInternal.maxspeed - 5);
if (FMGCInternal.mngSpdCmd > FMGCInternal.maxspeed - 5) {
FMGCInternal.mngSpd = (FMGCInternal.maxspeed - 5);
} else {
setprop("/FMGC/internal/mng-spd", mng_spd_cmd);
FMGCInternal.mngSpd = FMGCInternal.mngSpdCmd;
}
if (ktsmach and !mngktsmach) {
setprop("/it-autoflight/input/kts-mach", 0);
} else if (!ktsmach and mngktsmach) {
setprop("/it-autoflight/input/kts-mach", 1);
if (ktsmach and !FMGCInternal.mngKtsMach) {
Input.ktsMach.setValue(0);
} else if (!ktsmach and FMGCInternal.mngKtsMach) {
Input.ktsMach.setValue(1);
}
mng_spd = getprop("/FMGC/internal/mng-spd");
if (kts_sel != mng_spd and !ktsmach) {
setprop("/it-autoflight/input/kts", mng_spd);
} else if (mach_sel != mng_spd and ktsmach) {
setprop("/it-autoflight/input/mach", mng_spd);
if (kts_sel != FMGCInternal.mngSpd and !ktsmach) {
Input.kts.setValue(FMGCInternal.mngSpd);
} else if (mach_sel != FMGCInternal.mngSpd and ktsmach) {
Input.mach.setValue(FMGCInternal.mngSpd);
}
} else {
ManagedSPD.stop();

2
Nasal/Libraries/property-tree-setup.nas
View file

@ -76,6 +76,8 @@ var Engines = {
var Environment = {
magVar: props.globals.getNode("/environment/magnetic-variation-deg"),
tempDegC: props.globals.getNode("/environment/temperature-degc"),
windFromHdg: props.globals.getNode("/environment/wind-from-heading-deg"),
windSpeedKt: props.globals.getNode("/environment/wind-speed-kt"),
};
var Fdm = {

1
Nasal/Systems/pneumatics.nas
View file

@ -98,6 +98,7 @@ var PNEU = {
ramAir: props.globals.getNode("/systems/air-conditioning/valves/ram-air"),
hotAir: props.globals.getNode("/systems/air-conditioning/valves/hot-air"),
},
pressMode: props.globals.getNode("/systems/pressurization/mode", 1),
init: func() {
me.resetFail();