If installing IT-AUTOFLIGHT, please do so properly -- especially, with regards to dialogs, and ensuring the removal of old autopilot nasal.
This commit is contained in:
parent
ab74236b91
commit
c04c12d4ba
5 changed files with 146 additions and 139 deletions
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@ -278,9 +278,8 @@
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<item>
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<label>Autopilot Dialog</label>
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<binding>
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<command>nasal</command>
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<script>var ap_dialog = gui.Dialog.new("sim/gui/dialogs/ap_dialog/dialog", "Aircraft/A350-family/Systems/autopilot-dlg.xml");
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ap_dialog.open();</script>
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<command>dialog-show</command>
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<dialog-name>autopilot</dialog-name>
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</binding>
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</item>
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<item>
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@ -425,6 +424,7 @@
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</jsbsim>
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</fdm>
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<it-autoflight>
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<config>
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<roll>
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@ -459,13 +459,14 @@
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<auto-bank-max-deg>30</auto-bank-max-deg> <!-- Maximum Auto Bank Limit -->
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<autothrottle-max>0.95</autothrottle-max> <!-- Thrust Max Limit Normalized -->
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<autothrottle-min>0.02</autothrottle-min> <!-- Thrust Low Limit Normalized -->
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<custom-fma>0</custom-fma> <!-- Call functions when modes change for a custom FMA to be implemented -->
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<disable-final>0</disable-final> <!-- Disable the Final Controllers, for custom FCS integration -->
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<land-enable>1</land-enable> <!-- Enable/Disable Autoland -->
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<land-flap>0.7</land-flap> <!-- Minimum Flap used for Landing -->
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<land-flap>0.645</land-flap> <!-- Minimum Flap used for Landing -->
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<lat-agl-ft>50</lat-agl-ft> <!-- AGL when LNAV becomes active if armed -->
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<reduc-agl-ft>1500</reduc-agl-ft> <!-- AGL when T/O CLB changes to SPD CLB (FLCH), set to 0 to disable -->
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<retard-enable>1</retard-enable> <!-- AGL to Thrust Retard -->
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<retard-ft>50</retard-ft> <!-- Enable Thrust Retard -->
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<retard-ft>20</retard-ft> <!-- Enable Thrust Retard -->
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<togaspd>160</togaspd> <!-- V2 + 10kts -->
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</settings>
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</it-autoflight>
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@ -539,24 +540,6 @@
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<keyboard include="A350-keyboard.xml">
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</keyboard>
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</input>
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<!-- Autopilot initialization -->
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<autopilot>
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<settings>
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<kts-mach-select type="string">kts</kts-mach-select>
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<max-pitch type="float">6.0</max-pitch>
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<min-pitch type="float">-4.0</min-pitch>
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<bank-angle-limit-deg type="int">35</bank-angle-limit-deg>
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</settings>
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<internal>
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<target-pitch-deg type="float">0.00</target-pitch-deg>
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<max-pitch type="float">6.0</max-pitch>
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<min-pitch type="float">-4.0</min-pitch>
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</internal>
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</autopilot>
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<nasal>
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<A350XWB>
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@ -114,6 +114,7 @@ var Internal = {
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altPredicted: props.globals.initNode("/it-autoflight/internal/altitude-predicted", 0, "DOUBLE"),
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bankLimit: props.globals.initNode("/it-autoflight/internal/bank-limit", 30, "INT"),
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bankLimitAuto: 30,
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bankLimitMax: [30, 5, 10, 15, 20, 25, 30],
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captVs: 0,
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driftAngle: props.globals.initNode("/it-autoflight/internal/drift-angle-deg", 0, "DOUBLE"),
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flchActive: 0,
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@ -159,10 +160,11 @@ var Text = {
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vertTemp: "T/O CLB",
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};
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var Setting = {
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var Settings = {
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autoBankMaxDeg: props.globals.getNode("/it-autoflight/settings/auto-bank-max-deg", 1),
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autolandWithoutAp: props.globals.getNode("/it-autoflight/settings/autoland-without-ap", 1),
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autolandWithoutApTemp: 0,
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customFMA: props.globals.getNode("/it-autoflight/settings/custom-fma", 1),
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disableFinal: props.globals.getNode("/it-autoflight/settings/disable-final", 1),
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latAglFt: props.globals.getNode("/it-autoflight/settings/lat-agl-ft", 1),
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landingFlap: props.globals.getNode("/it-autoflight/settings/land-flap", 1),
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@ -197,29 +199,37 @@ var Gain = {
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};
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var ITAF = {
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init: func() {
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Input.ktsMach.setBoolValue(0);
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init: func(t) { # Not everything should be reset if the reset is type 1
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if (t != 1) {
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Input.alt.setValue(10000);
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Input.bankLimitSW.setValue(0);
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Input.hdg.setValue(360);
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Input.ktsMach.setBoolValue(0);
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Input.kts.setValue(250);
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Input.mach.setValue(0.5);
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Input.trk.setBoolValue(0);
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Input.trueCourse.setBoolValue(0);
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Input.useNav2Radio.setBoolValue(0);
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}
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Input.ap1.setBoolValue(0);
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Input.ap2.setBoolValue(0);
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Input.athr.setBoolValue(0);
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Input.fd1.setBoolValue(0);
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Input.fd2.setBoolValue(0);
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Input.hdg.setValue(360);
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Input.alt.setValue(10000);
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if (t != 1) {
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Input.fd1.setBoolValue(0);
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Input.fd2.setBoolValue(0);
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}
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Input.vs.setValue(0);
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Input.fpa.setValue(0);
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Input.lat.setValue(5);
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Input.vert.setValue(7);
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Input.trk.setBoolValue(0);
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Input.trueCourse.setBoolValue(0);
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Input.toga.setBoolValue(0);
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Input.bankLimitSW.setValue(0);
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Input.useNav2Radio.setBoolValue(0);
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Output.ap1.setBoolValue(0);
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Output.ap2.setBoolValue(0);
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Output.athr.setBoolValue(0);
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Output.fd1.setBoolValue(0);
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Output.fd2.setBoolValue(0);
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if (t != 1) {
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Output.fd1.setBoolValue(0);
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Output.fd2.setBoolValue(0);
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}
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Output.hdgInHld.setBoolValue(0);
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Output.lnavArm.setBoolValue(0);
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Output.locArm.setBoolValue(0);
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@ -229,16 +239,15 @@ var ITAF = {
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Output.vert.setValue(7);
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Internal.minVs.setValue(-500);
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Internal.maxVs.setValue(500);
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Internal.bankLimit.setValue(30);
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Internal.bankLimitAuto = 30;
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Internal.alt.setValue(10000);
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Internal.altCaptureActive = 0;
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Input.kts.setValue(250);
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Input.mach.setValue(0.5);
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Text.thr.setValue("PITCH");
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Text.arm.setValue(" ");
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Text.lat.setValue("T/O");
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Text.vert.setValue("T/O CLB");
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if (Settings.customFMA.getBoolValue()) {
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updateFMA.arm();
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}
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me.updateLatText("T/O");
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me.updateVertText("T/O CLB");
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loopTimer.start();
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slowLoopTimer.start();
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},
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@ -247,10 +256,10 @@ var ITAF = {
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Output.vertTemp = Output.vert.getValue();
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Output.ap1Temp = Output.ap1.getBoolValue();
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Output.ap2Temp = Output.ap2.getBoolValue();
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Setting.autolandWithoutApTemp = Setting.autolandWithoutAp.getBoolValue();
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Settings.autolandWithoutApTemp = Settings.autolandWithoutAp.getBoolValue();
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# Kill Autoland if the system should not autoland without AP, and AP is off
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if (Setting.autolandWithoutApTemp) { # Only evaluate the rest if this setting is on
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if (Settings.autolandWithoutApTemp) { # Only evaluate the rest if this setting is on
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if (!Output.ap1Temp and !Output.ap2Temp) {
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if (Output.latTemp == 4) {
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me.activateLOC();
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@ -312,35 +321,35 @@ var ITAF = {
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# Autoland Logic
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if (Output.latTemp == 2) {
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if (Position.gearAglFtTemp <= 150) {
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if (Output.ap1Temp or Output.ap2Temp or Setting.autolandWithoutApTemp) {
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if (Output.ap1Temp or Output.ap2Temp or Settings.autolandWithoutApTemp) {
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me.setLatMode(4);
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}
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}
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}
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if (Output.vertTemp == 2) {
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if (Position.gearAglFtTemp <= 100 and Position.gearAglFtTemp >= 5) {
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if (Output.ap1Temp or Output.ap2Temp or Setting.autolandWithoutApTemp) {
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if (Output.ap1Temp or Output.ap2Temp or Settings.autolandWithoutApTemp) {
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me.setVertMode(6);
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}
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}
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} else if (Output.vertTemp == 6) {
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if (!Output.ap1Temp and !Output.ap2Temp and !Setting.autolandWithoutApTemp) {
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if (!Output.ap1Temp and !Output.ap2Temp and !Settings.autolandWithoutApTemp) {
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me.activateLOC();
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me.activateGS();
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} else {
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if (Position.gearAglFtTemp <= 50 and Position.gearAglFtTemp >= 5) {
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Text.vert.setValue("FLARE");
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if (Position.gearAglFtTemp <= 50 and Position.gearAglFtTemp >= 5 and Text.vert.getValue() != "FLARE") {
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me.updateVertText("FLARE");
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}
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if (Gear.wow1Temp and Gear.wow2Temp) {
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Text.lat.setValue("RLOU");
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Text.vert.setValue("ROLLOUT");
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if (Gear.wow1Temp and Gear.wow2Temp and Text.vert.getValue() != "ROLLOUT") {
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me.updateLatText("RLOU");
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me.updateVertText("ROLLOUT");
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}
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}
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}
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# FLCH Engagement
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if (Text.vertTemp == "T/O CLB") {
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me.checkFLCH(Setting.reducAglFt.getValue());
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me.checkFLCH(Settings.reducAglFt.getValue());
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}
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# Altitude Capture/Sync Logic
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@ -363,14 +372,14 @@ var ITAF = {
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# Altitude Hold Min/Max Reset
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if (Internal.altCaptureActive) {
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if (abs(Internal.altDiff) <= 25) {
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if (abs(Internal.altDiff) <= 25 and Text.vert.getValue() != "ALT HLD") {
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me.resetClimbRateLim();
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Text.vert.setValue("ALT HLD");
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me.updateVertText("ALT HLD");
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}
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}
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# Thrust Mode Selector
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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) {
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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) {
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Output.thrMode.setValue(1);
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Text.thr.setValue("RETARD");
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if (Gear.wow1Temp or Gear.wow2Temp) { # Disconnect A/THR on either main gear touch
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@ -388,14 +397,14 @@ var ITAF = {
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if (Internal.altTemp >= Position.indicatedAltitudeFtTemp) {
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Output.thrMode.setValue(2);
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Text.thr.setValue("PITCH");
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if (Internal.flchActive) { # Set before mode change to prevent it from overwriting by mistake
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Text.vert.setValue("SPD CLB");
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if (Internal.flchActive and Text.vert.getValue() != "SPD CLB") { # Set before mode change to prevent it from overwriting by mistake
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me.updateVertText("SPD CLB");
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}
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} else {
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Output.thrMode.setValue(1);
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Text.thr.setValue("PITCH");
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if (Internal.flchActive) { # Set before mode change to prevent it from overwriting by mistake
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Text.vert.setValue("SPD DES");
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if (Internal.flchActive and Text.vert.getValue() != "SPD DES") { # Set before mode change to prevent it from overwriting by mistake
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me.updateVertText("SPD DES");
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}
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}
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} else if (Output.vertTemp == 7) {
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@ -421,22 +430,11 @@ var ITAF = {
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} else {
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Internal.bankLimitAuto = 30;
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}
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math.clamp(Internal.bankLimitAuto, 15, Setting.autoBankMaxDeg.getValue()); # Limit to max degree
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if (Input.bankLimitSWTemp == 0) {
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if (Internal.bankLimitAuto > Internal.bankLimitMax[Input.bankLimitSWTemp]) {
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Internal.bankLimit.setValue(Internal.bankLimitMax[Input.bankLimitSWTemp]);
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} else {
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Internal.bankLimit.setValue(Internal.bankLimitAuto);
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} else if (Input.bankLimitSWTemp == 1) {
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Internal.bankLimit.setValue(5);
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} else if (Input.bankLimitSWTemp == 2) {
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Internal.bankLimit.setValue(10);
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} else if (Input.bankLimitSWTemp == 3) {
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Internal.bankLimit.setValue(15);
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} else if (Input.bankLimitSWTemp == 4) {
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Internal.bankLimit.setValue(20);
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} else if (Input.bankLimitSWTemp == 5) {
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Internal.bankLimit.setValue(25);
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} else if (Input.bankLimitSWTemp == 6) {
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Internal.bankLimit.setValue(30);
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}
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# If in LNAV mode and route is not longer active, switch to HDG HLD
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@ -488,11 +486,11 @@ var ITAF = {
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# Reset system once flight complete
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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
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me.init();
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me.init(1);
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}
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# Calculate Roll and Pitch Rate Kp
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if (!Setting.disableFinal.getBoolValue()) {
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if (!Settings.disableFinal.getBoolValue()) {
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Gain.rollKpLowTemp = Gain.rollKpLow.getValue();
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Gain.rollKpHighTemp = Gain.rollKpHigh.getValue();
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Gain.pitchKpLowTemp = Gain.pitchKpLow.getValue();
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@ -558,7 +556,7 @@ var ITAF = {
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},
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apOffFunction: func() {
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if (!Output.ap1.getBoolValue() and !Output.ap2.getBoolValue()) { # Only do if both APs are off
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if (!Setting.disableFinal.getBoolValue()) {
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if (!Settings.disableFinal.getBoolValue()) {
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Controls.aileron.setValue(0);
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Controls.elevator.setValue(0);
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Controls.rudder.setValue(0);
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@ -608,11 +606,11 @@ var ITAF = {
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setLatMode: func(n) {
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Output.vertTemp = Output.vert.getValue();
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if (n == 0) { # HDG SEL
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Output.lnavArm.setBoolValue(0);
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Output.locArm.setBoolValue(0);
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Output.apprArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.updateLocArm(0);
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me.updateApprArm(0);
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Output.lat.setValue(0);
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Text.lat.setValue("HDG");
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me.updateLatText("HDG");
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if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
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me.setVertMode(1);
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} else {
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@ -621,16 +619,16 @@ var ITAF = {
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} else if (n == 1) { # LNAV
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me.checkLNAV(0);
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} else if (n == 2) { # VOR/LOC
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Output.lnavArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.armTextCheck();
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me.checkLOC(0, 0);
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} else if (n == 3) { # HDG HLD
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Output.lnavArm.setBoolValue(0);
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Output.locArm.setBoolValue(0);
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Output.apprArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.updateLocArm(0);
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me.updateApprArm(0);
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me.syncHdg();
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Output.lat.setValue(0);
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Text.lat.setValue("HDG");
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me.updateLatText("HDG");
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Internal.hdgHldValue = Input.hdg.getValue();
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Output.hdgInHld.setBoolValue(1);
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if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
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me.armTextCheck();
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}
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} else if (n == 4) { # ALIGN
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Output.lnavArm.setBoolValue(0);
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Output.locArm.setBoolValue(0);
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Output.apprArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.updateLocArm(0);
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me.updateApprArm(0);
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Output.lat.setValue(4);
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Text.lat.setValue("ALGN");
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me.updateLatText("ALGN");
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me.armTextCheck();
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} else if (n == 5) { # T/O
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Output.lnavArm.setBoolValue(0);
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Output.locArm.setBoolValue(0);
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Output.apprArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.updateLocArm(0);
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me.updateApprArm(0);
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Output.lat.setValue(5);
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Text.lat.setValue("T/O");
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me.updateLatText("T/O");
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me.armTextCheck();
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}
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},
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setLatArm: func(n) {
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if (n == 0) {
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Output.lnavArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.armTextCheck();
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} else if (n == 1) {
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if (FPLN.num.getValue() > 0 and FPLN.active.getBoolValue()) {
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Output.lnavArm.setBoolValue(1);
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me.updateLnavArm(1);
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me.armTextCheck();
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}
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} else if (n == 3) {
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me.syncHdg();
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Output.lnavArm.setBoolValue(0);
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me.updateLnavArm(0);
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me.armTextCheck();
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}
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},
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@ -674,23 +672,23 @@ var ITAF = {
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if (n == 0) { # ALT HLD
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Internal.flchActive = 0;
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Internal.altCaptureActive = 0;
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Output.apprArm.setBoolValue(0);
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me.updateApprArm(0);
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Output.vert.setValue(0);
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me.resetClimbRateLim();
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Text.vert.setValue("ALT HLD");
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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.
|
||||
|
|
|
@ -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();
|
||||
});
|
||||
|
|
|
@ -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>
|
||||
|
|
Loading…
Reference in a new issue