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If installing IT-AUTOFLIGHT, please do so properly -- especially, with regards to dialogs, and ensuring the removal of old autopilot nasal.

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This commit is contained in:
legoboyvdlp R 2020-09-05 16:38:27 +01:00
parent ab74236b91
commit c04c12d4ba
5 changed files with 146 additions and 139 deletions
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29
A350-common.xml
View file

@ -278,9 +278,8 @@
<item>
<label>Autopilot Dialog</label>
<binding>
<command>nasal</command>
<script>var ap_dialog = gui.Dialog.new("sim/gui/dialogs/ap_dialog/dialog", "Aircraft/A350-family/Systems/autopilot-dlg.xml");
ap_dialog.open();</script>
<command>dialog-show</command>
<dialog-name>autopilot</dialog-name>
</binding>
</item>
<item>
@ -425,6 +424,7 @@
</jsbsim>
</fdm>
<it-autoflight>
<config>
<roll>
@ -459,13 +459,14 @@
<auto-bank-max-deg>30</auto-bank-max-deg> <!-- Maximum Auto Bank Limit -->
<autothrottle-max>0.95</autothrottle-max> <!-- Thrust Max Limit Normalized -->
<autothrottle-min>0.02</autothrottle-min> <!-- Thrust Low Limit Normalized -->
<custom-fma>0</custom-fma> <!-- Call functions when modes change for a custom FMA to be implemented -->
<disable-final>0</disable-final> <!-- Disable the Final Controllers, for custom FCS integration -->
<land-enable>1</land-enable> <!-- Enable/Disable Autoland -->
<land-flap>0.7</land-flap> <!-- Minimum Flap used for Landing -->
<land-flap>0.645</land-flap> <!-- Minimum Flap used for Landing -->
<lat-agl-ft>50</lat-agl-ft> <!-- AGL when LNAV becomes active if armed -->
<reduc-agl-ft>1500</reduc-agl-ft> <!-- AGL when T/O CLB changes to SPD CLB (FLCH), set to 0 to disable -->
<retard-enable>1</retard-enable> <!-- AGL to Thrust Retard -->
<retard-ft>50</retard-ft> <!-- Enable Thrust Retard -->
<retard-ft>20</retard-ft> <!-- Enable Thrust Retard -->
<togaspd>160</togaspd> <!-- V2 + 10kts -->
</settings>
</it-autoflight>
@ -540,24 +541,6 @@
</keyboard>
</input>
<!-- Autopilot initialization -->
<autopilot>
<settings>
<kts-mach-select type="string">kts</kts-mach-select>
<max-pitch type="float">6.0</max-pitch>
<min-pitch type="float">-4.0</min-pitch>
<bank-angle-limit-deg type="int">35</bank-angle-limit-deg>
</settings>
<internal>
<target-pitch-deg type="float">0.00</target-pitch-deg>
<max-pitch type="float">6.0</max-pitch>
<min-pitch type="float">-4.0</min-pitch>
</internal>
</autopilot>
<nasal>
<A350XWB>
<file>Aircraft/A350-family/Nasal/ECAM.nas</file>

235
Nasal/it-autoflight.nas
View file

@ -114,6 +114,7 @@ var Internal = {
altPredicted: props.globals.initNode("/it-autoflight/internal/altitude-predicted", 0, "DOUBLE"),
bankLimit: props.globals.initNode("/it-autoflight/internal/bank-limit", 30, "INT"),
bankLimitAuto: 30,
bankLimitMax: [30, 5, 10, 15, 20, 25, 30],
captVs: 0,
driftAngle: props.globals.initNode("/it-autoflight/internal/drift-angle-deg", 0, "DOUBLE"),
flchActive: 0,
@ -159,10 +160,11 @@ var Text = {
vertTemp: "T/O CLB",
};
var Setting = {
var Settings = {
autoBankMaxDeg: props.globals.getNode("/it-autoflight/settings/auto-bank-max-deg", 1),
autolandWithoutAp: props.globals.getNode("/it-autoflight/settings/autoland-without-ap", 1),
autolandWithoutApTemp: 0,
customFMA: props.globals.getNode("/it-autoflight/settings/custom-fma", 1),
disableFinal: props.globals.getNode("/it-autoflight/settings/disable-final", 1),
latAglFt: props.globals.getNode("/it-autoflight/settings/lat-agl-ft", 1),
landingFlap: props.globals.getNode("/it-autoflight/settings/land-flap", 1),
@ -197,29 +199,37 @@ var Gain = {
};
var ITAF = {
init: func() {
init: func(t) { # Not everything should be reset if the reset is type 1
if (t != 1) {
Input.alt.setValue(10000);
Input.bankLimitSW.setValue(0);
Input.hdg.setValue(360);
Input.ktsMach.setBoolValue(0);
Input.kts.setValue(250);
Input.mach.setValue(0.5);
Input.trk.setBoolValue(0);
Input.trueCourse.setBoolValue(0);
Input.useNav2Radio.setBoolValue(0);
}
Input.ap1.setBoolValue(0);
Input.ap2.setBoolValue(0);
Input.athr.setBoolValue(0);
if (t != 1) {
Input.fd1.setBoolValue(0);
Input.fd2.setBoolValue(0);
Input.hdg.setValue(360);
Input.alt.setValue(10000);
}
Input.vs.setValue(0);
Input.fpa.setValue(0);
Input.lat.setValue(5);
Input.vert.setValue(7);
Input.trk.setBoolValue(0);
Input.trueCourse.setBoolValue(0);
Input.toga.setBoolValue(0);
Input.bankLimitSW.setValue(0);
Input.useNav2Radio.setBoolValue(0);
Output.ap1.setBoolValue(0);
Output.ap2.setBoolValue(0);
Output.athr.setBoolValue(0);
if (t != 1) {
Output.fd1.setBoolValue(0);
Output.fd2.setBoolValue(0);
}
Output.hdgInHld.setBoolValue(0);
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
@ -229,16 +239,15 @@ var ITAF = {
Output.vert.setValue(7);
Internal.minVs.setValue(-500);
Internal.maxVs.setValue(500);
Internal.bankLimit.setValue(30);
Internal.bankLimitAuto = 30;
Internal.alt.setValue(10000);
Internal.altCaptureActive = 0;
Input.kts.setValue(250);
Input.mach.setValue(0.5);
Text.thr.setValue("PITCH");
Text.arm.setValue(" ");
Text.lat.setValue("T/O");
Text.vert.setValue("T/O CLB");
if (Settings.customFMA.getBoolValue()) {
updateFMA.arm();
}
me.updateLatText("T/O");
me.updateVertText("T/O CLB");
loopTimer.start();
slowLoopTimer.start();
},
@ -247,10 +256,10 @@ var ITAF = {
Output.vertTemp = Output.vert.getValue();
Output.ap1Temp = Output.ap1.getBoolValue();
Output.ap2Temp = Output.ap2.getBoolValue();
Setting.autolandWithoutApTemp = Setting.autolandWithoutAp.getBoolValue();
Settings.autolandWithoutApTemp = Settings.autolandWithoutAp.getBoolValue();
# Kill Autoland if the system should not autoland without AP, and AP is off
if (Setting.autolandWithoutApTemp) { # Only evaluate the rest if this setting is on
if (Settings.autolandWithoutApTemp) { # Only evaluate the rest if this setting is on
if (!Output.ap1Temp and !Output.ap2Temp) {
if (Output.latTemp == 4) {
me.activateLOC();
@ -312,35 +321,35 @@ var ITAF = {
# Autoland Logic
if (Output.latTemp == 2) {
if (Position.gearAglFtTemp <= 150) {
if (Output.ap1Temp or Output.ap2Temp or Setting.autolandWithoutApTemp) {
if (Output.ap1Temp or Output.ap2Temp or Settings.autolandWithoutApTemp) {
me.setLatMode(4);
}
}
}
if (Output.vertTemp == 2) {
if (Position.gearAglFtTemp <= 100 and Position.gearAglFtTemp >= 5) {
if (Output.ap1Temp or Output.ap2Temp or Setting.autolandWithoutApTemp) {
if (Output.ap1Temp or Output.ap2Temp or Settings.autolandWithoutApTemp) {
me.setVertMode(6);
}
}
} else if (Output.vertTemp == 6) {
if (!Output.ap1Temp and !Output.ap2Temp and !Setting.autolandWithoutApTemp) {
if (!Output.ap1Temp and !Output.ap2Temp and !Settings.autolandWithoutApTemp) {
me.activateLOC();
me.activateGS();
} else {
if (Position.gearAglFtTemp <= 50 and Position.gearAglFtTemp >= 5) {
Text.vert.setValue("FLARE");
if (Position.gearAglFtTemp <= 50 and Position.gearAglFtTemp >= 5 and Text.vert.getValue() != "FLARE") {
me.updateVertText("FLARE");
}
if (Gear.wow1Temp and Gear.wow2Temp) {
Text.lat.setValue("RLOU");
Text.vert.setValue("ROLLOUT");
if (Gear.wow1Temp and Gear.wow2Temp and Text.vert.getValue() != "ROLLOUT") {
me.updateLatText("RLOU");
me.updateVertText("ROLLOUT");
}
}
}
# FLCH Engagement
if (Text.vertTemp == "T/O CLB") {
me.checkFLCH(Setting.reducAglFt.getValue());
me.checkFLCH(Settings.reducAglFt.getValue());
}
# Altitude Capture/Sync Logic
@ -363,14 +372,14 @@ var ITAF = {
# Altitude Hold Min/Max Reset
if (Internal.altCaptureActive) {
if (abs(Internal.altDiff) <= 25) {
if (abs(Internal.altDiff) <= 25 and Text.vert.getValue() != "ALT HLD") {
me.resetClimbRateLim();
Text.vert.setValue("ALT HLD");
me.updateVertText("ALT HLD");
}
}
# Thrust Mode Selector
if (Output.athr.getBoolValue() and Output.vertTemp != 7 and Setting.retardEnable.getBoolValue() and Position.gearAglFt.getValue() <= Setting.retardAltitude.getValue() and Misc.flapNorm.getValue() >= Setting.landingFlap.getValue() - 0.001) {
if (Output.athr.getBoolValue() and Output.vertTemp != 7 and Settings.retardEnable.getBoolValue() and Position.gearAglFt.getValue() <= Settings.retardAltitude.getValue() and Misc.flapNorm.getValue() >= Settings.landingFlap.getValue() - 0.001) {
Output.thrMode.setValue(1);
Text.thr.setValue("RETARD");
if (Gear.wow1Temp or Gear.wow2Temp) { # Disconnect A/THR on either main gear touch
@ -388,14 +397,14 @@ var ITAF = {
if (Internal.altTemp >= Position.indicatedAltitudeFtTemp) {
Output.thrMode.setValue(2);
Text.thr.setValue("PITCH");
if (Internal.flchActive) { # Set before mode change to prevent it from overwriting by mistake
Text.vert.setValue("SPD CLB");
if (Internal.flchActive and Text.vert.getValue() != "SPD CLB") { # Set before mode change to prevent it from overwriting by mistake
me.updateVertText("SPD CLB");
}
} else {
Output.thrMode.setValue(1);
Text.thr.setValue("PITCH");
if (Internal.flchActive) { # Set before mode change to prevent it from overwriting by mistake
Text.vert.setValue("SPD DES");
if (Internal.flchActive and Text.vert.getValue() != "SPD DES") { # Set before mode change to prevent it from overwriting by mistake
me.updateVertText("SPD DES");
}
}
} else if (Output.vertTemp == 7) {
@ -421,22 +430,11 @@ var ITAF = {
} else {
Internal.bankLimitAuto = 30;
}
math.clamp(Internal.bankLimitAuto, 15, Setting.autoBankMaxDeg.getValue()); # Limit to max degree
if (Input.bankLimitSWTemp == 0) {
if (Internal.bankLimitAuto > Internal.bankLimitMax[Input.bankLimitSWTemp]) {
Internal.bankLimit.setValue(Internal.bankLimitMax[Input.bankLimitSWTemp]);
} else {
Internal.bankLimit.setValue(Internal.bankLimitAuto);
} else if (Input.bankLimitSWTemp == 1) {
Internal.bankLimit.setValue(5);
} else if (Input.bankLimitSWTemp == 2) {
Internal.bankLimit.setValue(10);
} else if (Input.bankLimitSWTemp == 3) {
Internal.bankLimit.setValue(15);
} else if (Input.bankLimitSWTemp == 4) {
Internal.bankLimit.setValue(20);
} else if (Input.bankLimitSWTemp == 5) {
Internal.bankLimit.setValue(25);
} else if (Input.bankLimitSWTemp == 6) {
Internal.bankLimit.setValue(30);
}
# If in LNAV mode and route is not longer active, switch to HDG HLD
@ -488,11 +486,11 @@ var ITAF = {
# Reset system once flight complete
if (!Output.ap1.getBoolValue() and !Output.ap2.getBoolValue() and Gear.wow0.getBoolValue() and Velocities.groundspeedKt.getValue() < 60 and Output.vert.getValue() != 7) { # Not in T/O or G/A
me.init();
me.init(1);
}
# Calculate Roll and Pitch Rate Kp
if (!Setting.disableFinal.getBoolValue()) {
if (!Settings.disableFinal.getBoolValue()) {
Gain.rollKpLowTemp = Gain.rollKpLow.getValue();
Gain.rollKpHighTemp = Gain.rollKpHigh.getValue();
Gain.pitchKpLowTemp = Gain.pitchKpLow.getValue();
@ -558,7 +556,7 @@ var ITAF = {
},
apOffFunction: func() {
if (!Output.ap1.getBoolValue() and !Output.ap2.getBoolValue()) { # Only do if both APs are off
if (!Setting.disableFinal.getBoolValue()) {
if (!Settings.disableFinal.getBoolValue()) {
Controls.aileron.setValue(0);
Controls.elevator.setValue(0);
Controls.rudder.setValue(0);
@ -608,11 +606,11 @@ var ITAF = {
setLatMode: func(n) {
Output.vertTemp = Output.vert.getValue();
if (n == 0) { # HDG SEL
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
Output.apprArm.setBoolValue(0);
me.updateLnavArm(0);
me.updateLocArm(0);
me.updateApprArm(0);
Output.lat.setValue(0);
Text.lat.setValue("HDG");
me.updateLatText("HDG");
if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
me.setVertMode(1);
} else {
@ -621,16 +619,16 @@ var ITAF = {
} else if (n == 1) { # LNAV
me.checkLNAV(0);
} else if (n == 2) { # VOR/LOC
Output.lnavArm.setBoolValue(0);
me.updateLnavArm(0);
me.armTextCheck();
me.checkLOC(0, 0);
} else if (n == 3) { # HDG HLD
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
Output.apprArm.setBoolValue(0);
me.updateLnavArm(0);
me.updateLocArm(0);
me.updateApprArm(0);
me.syncHdg();
Output.lat.setValue(0);
Text.lat.setValue("HDG");
me.updateLatText("HDG");
Internal.hdgHldValue = Input.hdg.getValue();
Output.hdgInHld.setBoolValue(1);
if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
@ -639,33 +637,33 @@ var ITAF = {
me.armTextCheck();
}
} else if (n == 4) { # ALIGN
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
Output.apprArm.setBoolValue(0);
me.updateLnavArm(0);
me.updateLocArm(0);
me.updateApprArm(0);
Output.lat.setValue(4);
Text.lat.setValue("ALGN");
me.updateLatText("ALGN");
me.armTextCheck();
} else if (n == 5) { # T/O
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
Output.apprArm.setBoolValue(0);
me.updateLnavArm(0);
me.updateLocArm(0);
me.updateApprArm(0);
Output.lat.setValue(5);
Text.lat.setValue("T/O");
me.updateLatText("T/O");
me.armTextCheck();
}
},
setLatArm: func(n) {
if (n == 0) {
Output.lnavArm.setBoolValue(0);
me.updateLnavArm(0);
me.armTextCheck();
} else if (n == 1) {
if (FPLN.num.getValue() > 0 and FPLN.active.getBoolValue()) {
Output.lnavArm.setBoolValue(1);
me.updateLnavArm(1);
me.armTextCheck();
}
} else if (n == 3) {
me.syncHdg();
Output.lnavArm.setBoolValue(0);
me.updateLnavArm(0);
me.armTextCheck();
}
},
@ -674,23 +672,23 @@ var ITAF = {
if (n == 0) { # ALT HLD
Internal.flchActive = 0;
Internal.altCaptureActive = 0;
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
Output.vert.setValue(0);
me.resetClimbRateLim();
Text.vert.setValue("ALT HLD");
me.updateVertText("ALT HLD");
me.syncAlt();
me.armTextCheck();
} else if (n == 1) { # V/S
if (abs(Input.altDiff) >= 25) {
Internal.flchActive = 0;
Internal.altCaptureActive = 0;
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
Output.vert.setValue(1);
Text.vert.setValue("V/S");
me.updateVertText("V/S");
me.syncVs();
me.armTextCheck();
} else {
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
me.armTextCheck();
}
} else if (n == 2) { # G/S
@ -701,14 +699,14 @@ var ITAF = {
Output.vert.setValue(0);
me.setClimbRateLim();
Internal.altCaptureActive = 1;
Text.vert.setValue("ALT CAP");
me.updateVertText("ALT CAP");
} else if (n == 4) { # FLCH
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
if (abs(Input.altDiff) >= 125) { # SPD CLB or SPD DES
if (Input.alt.getValue() >= Position.indicatedAltitudeFt.getValue()) { # Usually set Thrust Mode Selector, but we do it now due to timer lag
Text.vert.setValue("SPD CLB");
me.updateVertText("SPD CLB");
} else {
Text.vert.setValue("SPD DES");
me.updateVertText("SPD DES");
}
Internal.altCaptureActive = 0;
Output.vert.setValue(4);
@ -718,44 +716,44 @@ var ITAF = {
Internal.alt.setValue(Input.alt.getValue());
Internal.altCaptureActive = 1;
Output.vert.setValue(0);
Text.vert.setValue("ALT CAP");
me.updateVertText("ALT CAP");
}
me.armTextCheck();
} else if (n == 5) { # FPA
if (abs(Input.altDiff) >= 25) {
Internal.flchActive = 0;
Internal.altCaptureActive = 0;
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
Output.vert.setValue(5);
Text.vert.setValue("FPA");
me.updateVertText("FPA");
me.syncFpa();
me.armTextCheck();
} else {
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
me.armTextCheck();
}
} else if (n == 6) { # FLARE/ROLLOUT
Internal.flchActive = 0;
Internal.altCaptureActive = 0;
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
Output.vert.setValue(6);
Text.vert.setValue("G/S");
me.updateVertText("G/S");
me.armTextCheck();
} else if (n == 7) { # T/O CLB or G/A CLB, text is set by TOGA selector
Internal.flchActive = 0;
Internal.altCaptureActive = 0;
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
Output.vert.setValue(7);
me.armTextCheck();
}
},
activateLNAV: func() {
if (Output.lat.getValue() != 1) {
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
Output.apprArm.setBoolValue(0);
me.updateLnavArm(0);
me.updateLocArm(0);
me.updateApprArm(0);
Output.lat.setValue(1);
Text.lat.setValue("LNAV");
me.updateLatText("LNAV");
if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
me.setVertMode(1);
} else {
@ -765,10 +763,10 @@ var ITAF = {
},
activateLOC: func() {
if (Output.lat.getValue() != 2) {
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(0);
me.updateLnavArm(0);
me.updateLocArm(0);
Output.lat.setValue(2);
Text.lat.setValue("LOC");
me.updateLatText("LOC");
me.armTextCheck();
}
},
@ -776,17 +774,17 @@ var ITAF = {
if (Output.vert.getValue() != 2) {
Internal.flchActive = 0;
Internal.altCaptureActive = 0;
Output.apprArm.setBoolValue(0);
me.updateApprArm(0);
Output.vert.setValue(2);
Text.vert.setValue("G/S");
me.updateVertText("G/S");
me.armTextCheck();
}
},
checkLNAV: func(t) {
if (FPLN.num.getValue() > 0 and FPLN.active.getBoolValue() and Position.gearAglFt.getValue() >= Setting.latAglFt.getValue()) {
if (FPLN.num.getValue() > 0 and FPLN.active.getBoolValue() and Position.gearAglFt.getValue() >= Settings.latAglFt.getValue()) {
me.activateLNAV();
} else if (FPLN.active.getBoolValue() and Output.lat.getValue() != 1 and t != 1) {
Output.lnavArm.setBoolValue(1);
me.updateLnavArm(1);
me.armTextCheck();
}
},
@ -804,8 +802,8 @@ var ITAF = {
me.activateLOC();
} else if (t != 1) { # Do not do this if loop calls it
if (Output.lat.getValue() != 2) {
Output.lnavArm.setBoolValue(0);
Output.locArm.setBoolValue(1);
me.updateLnavArm(0);
me.updateLocArm(1);
if (a != 1) { # Don't call this if arming with G/S
me.armTextCheck();
}
@ -823,7 +821,7 @@ var ITAF = {
me.activateGS();
} else if (t != 1) { # Do not do this if loop calls it
if (Output.vert.getValue() != 2) {
Output.apprArm.setBoolValue(1);
me.updateApprArm(1);
}
me.armTextCheck();
}
@ -864,7 +862,7 @@ var ITAF = {
if ((Output.vertTemp == 2 or Output.vertTemp == 6) and Velocities.indicatedAirspeedKt.getValue() >= 80) {
me.setLatMode(3);
me.setVertMode(7); # Must be before kicking AP off
Text.vert.setValue("G/A CLB");
me.updateVertText("G/A CLB");
Input.ktsMach.setBoolValue(0);
me.syncKtsGa();
if (Gear.wow1.getBoolValue() or Gear.wow2.getBoolValue()) {
@ -877,7 +875,7 @@ var ITAF = {
me.setLatMode(5);
}
me.setVertMode(7);
Text.vert.setValue("T/O CLB");
me.updateVertText("T/O CLB");
}
},
armTextCheck: func() {
@ -895,7 +893,7 @@ var ITAF = {
Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), 100, 350));
},
syncKtsGa: func() { # Same as syncKts, except doesn't go below TogaSpd
Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), Setting.togaSpd.getValue(), 350));
Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), Settings.togaSpd.getValue(), 350));
},
syncMach: func() {
Input.mach.setValue(math.clamp(math.round(Velocities.indicatedMach.getValue(), 0.001), 0.5, 0.9));
@ -913,6 +911,37 @@ var ITAF = {
syncFpa: func() {
Input.fpa.setValue(math.clamp(math.round(Internal.fpa.getValue(), 0.1), -9.9, 9.9));
},
# Allows custom FMA behavior if desired
updateLatText: func(t) {
Text.lat.setValue(t);
if (Settings.customFMA.getBoolValue()) {
updateFMA.lat();
}
},
updateVertText: func(t) {
Text.vert.setValue(t);
if (Settings.customFMA.getBoolValue()) {
updateFMA.vert();
}
},
updateLnavArm: func(n) {
Output.lnavArm.setBoolValue(n);
if (Settings.customFMA.getBoolValue()) {
updateFMA.arm();
}
},
updateLocArm: func(n) {
Output.locArm.setBoolValue(n);
if (Settings.customFMA.getBoolValue()) {
updateFMA.arm();
}
},
updateApprArm: func(n) {
Output.apprArm.setBoolValue(n);
if (Settings.customFMA.getBoolValue()) {
updateFMA.arm();
}
},
};
setlistener("/it-autoflight/input/ap1", func {
@ -1006,7 +1035,7 @@ setlistener("/it-autoflight/input/trk", func {
}, 0, 0);
setlistener("/sim/signals/fdm-initialized", func {
ITAF.init();
ITAF.init(0);
});
# For Canvas Nav Display.

7
Nasal/system.nas
View file

@ -20,10 +20,5 @@ setlistener("controls/gear/gear-down", func
});
setlistener("/sim/signals/fdm-initialized", func {
itaf.ap_init();
var autopilot = gui.Dialog.new("sim/gui/dialogs/autopilot/dialog", "Aircraft/A350-family/Systems/autopilot-dlg.xml");
setprop("/it-autoflight/settings/retard-enable", 1); # Enable or disable automatic autothrottle retard.
setprop("/it-autoflight/settings/retard-ft", 20); # Add this to change the retard altitude, default is 50ft AGL.
setprop("/it-autoflight/settings/land-flap", 0.645); # Define the landing flaps here. This is needed for autoland, and retard.
setprop("/it-autoflight/settings/land-enable", 0); # Enable or disable automatic landing.
itaf.ITAF.init();
});

4
Systems/it-autoflight.xml
View file

@ -1476,7 +1476,7 @@
<property>/orientation/pitch-deg</property>
<value>5</value>
</dif>
<value>-10</value>
<value>-15</value>
</max>
</expression>
</u_min>
@ -1502,7 +1502,7 @@
<property>/orientation/pitch-deg</property>
<value>5</value>
</sum>
<value>25</value>
<value>30</value>
</min>
</expression>
</u_max>

0
Systems/autopilot-dlg.xml → gui/dialogs/it-autoflight-dlg.xml
View file