1093 lines
36 KiB
Text
1093 lines
36 KiB
Text
# A3XX FMGC Autopilot
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# Based off IT-AUTOFLIGHT System Controller V4.0.X
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# Copyright (c) 2021 Josh Davidson (Octal450)
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# Initialize all used variables and property nodes
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# Sim
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var Controls = {
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aileron: props.globals.getNode("/controls/flight/aileron", 1),
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aileron2: props.globals.getNode("/controls/flight/aileron[1]", 1),
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elevator: props.globals.getNode("/controls/flight/elevator", 1),
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elevator2: props.globals.getNode("/controls/flight/elevator[1]", 1),
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rudder: props.globals.getNode("/controls/flight/rudder", 1),
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rudder2: props.globals.getNode("/controls/flight/rudder[1]", 1),
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};
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var FPLN = {
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active: props.globals.getNode("/FMGC/flightplan[2]/active", 1),
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activeTemp: 0,
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currentCourse: 0,
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currentWp: props.globals.getNode("/FMGC/flightplan[2]/current-wp", 1),
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currentWpTemp: 0,
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deltaAngle: 0,
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deltaAngleRad: 0,
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distCoeff: 0,
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maxBank: 0,
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maxBankLimit: 0,
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nextCourse: 0,
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R: 0,
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radius: 0,
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turnDist: 0,
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wp0Dist: props.globals.getNode("/FMGC/flightplan[2]/current-leg-dist", 1),
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wpFlyFrom: 0,
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wpFlyTo: 0,
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};
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var Gear = {
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wow0: props.globals.getNode("/gear/gear[0]/wow", 1),
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wow1: props.globals.getNode("/gear/gear[1]/wow", 1),
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wow1Temp: 1,
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wow2: props.globals.getNode("/gear/gear[2]/wow", 1),
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wow2Temp: 1,
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};
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var Misc = {
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elapsedSec: props.globals.getNode("/sim/time/elapsed-sec", 1),
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fbwLaw: props.globals.getNode("/it-fbw/law", 1),
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flapNorm: props.globals.getNode("/surface-positions/flap-pos-norm", 1),
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pfdHeadingScale: props.globals.getNode("/instrumentation/pfd/heading-scale", 1),
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};
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var Position = {
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gearAglFtTemp: 0,
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gearAglFt: props.globals.getNode("/position/gear-agl-ft", 1),
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indicatedAltitudeFt: props.globals.getNode("/instrumentation/altimeter/indicated-altitude-ft", 1),
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indicatedAltitudeFtTemp: 0,
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};
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var Radio = {
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gsDefl: props.globals.getNode("/instrumentation/nav[0]/gs-needle-deflection-norm", 1),
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gsDeflTemp: 0,
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inRange: props.globals.getNode("/instrumentation/nav[0]/in-range", 1),
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locDefl: props.globals.getNode("/instrumentation/nav[0]/heading-needle-deflection-norm", 1),
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locDeflTemp: 0,
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signalQuality: props.globals.getNode("/instrumentation/nav[0]/signal-quality-norm", 1),
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signalQualityTemp: 0,
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};
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var Velocities = {
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airspeedKt: props.globals.getNode("/velocities/airspeed-kt", 1), # Only used for gain scheduling
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groundspeedKt: props.globals.getNode("/velocities/groundspeed-kt", 1),
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groundspeedMps: 0,
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indicatedAirspeedKt: props.globals.getNode("/instrumentation/airspeed-indicator/indicated-speed-kt", 1),
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indicatedMach: props.globals.getNode("/instrumentation/airspeed-indicator/indicated-mach", 1),
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trueAirspeedKt: props.globals.getNode("/instrumentation/airspeed-indicator/true-speed-kt", 1),
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trueAirspeedKtTemp: 0,
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};
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# IT-AUTOFLIGHT
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var Fd = {
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pitchBar: props.globals.initNode("/it-autoflight/fd/pitch-bar", 0, "DOUBLE"),
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rollBar: props.globals.initNode("/it-autoflight/fd/roll-bar", 0, "DOUBLE"),
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};
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var Input = {
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alt: props.globals.initNode("/it-autoflight/input/alt", 10000, "INT"),
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ap1: props.globals.initNode("/it-autoflight/input/ap1", 0, "BOOL"),
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ap2: props.globals.initNode("/it-autoflight/input/ap2", 0, "BOOL"),
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athr: props.globals.initNode("/it-autoflight/input/athr", 0, "BOOL"),
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altDiff: 0,
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bankLimitSw: props.globals.initNode("/it-autoflight/input/bank-limit-sw", 0, "INT"),
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bankLimitSwTemp: 0,
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fd1: props.globals.initNode("/it-autoflight/input/fd1", 1, "BOOL"),
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fd2: props.globals.initNode("/it-autoflight/input/fd2", 1, "BOOL"),
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fpa: props.globals.initNode("/it-autoflight/input/fpa", 0, "DOUBLE"),
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fpaAbs: props.globals.initNode("/it-autoflight/input/fpa-abs", 0, "DOUBLE"), # Set by property rule
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hdg: props.globals.initNode("/it-autoflight/input/hdg", 0, "INT"),
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hdgCalc: 0,
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kts: props.globals.initNode("/it-autoflight/input/kts", 100, "INT"),
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ktsMach: props.globals.initNode("/it-autoflight/input/kts-mach", 0, "BOOL"),
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lat: props.globals.initNode("/it-autoflight/input/lat", 5, "INT"),
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latTemp: 5,
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mach: props.globals.initNode("/it-autoflight/input/mach", 0.5, "DOUBLE"),
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toga: props.globals.initNode("/it-autoflight/input/toga", 0, "BOOL"),
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trk: props.globals.initNode("/it-autoflight/input/trk", 0, "BOOL"),
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trueCourse: props.globals.initNode("/it-autoflight/input/true-course", 0, "BOOL"),
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vert: props.globals.initNode("/it-autoflight/input/vert", 7, "INT"),
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vertTemp: 7,
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vs: props.globals.initNode("/it-autoflight/input/vs", 0, "INT"),
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vsAbs: props.globals.initNode("/it-autoflight/input/vs-abs", 0, "INT"), # Set by property rule
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};
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var Internal = {
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alt: props.globals.initNode("/it-autoflight/internal/alt", 10000, "INT"),
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altCaptureActive: 0,
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altDiff: 0,
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altTemp: 0,
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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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captVs: 0,
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driftAngle: props.globals.initNode("/it-autoflight/internal/drift-angle-deg", 0, "DOUBLE"),
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driftAngleTemp: 0,
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flchActive: 0,
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fpa: props.globals.initNode("/it-autoflight/internal/fpa", 0, "DOUBLE"),
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hdgErrorDeg: props.globals.initNode("/it-autoflight/internal/heading-error-deg", 0, "DOUBLE"),
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hdgPredicted: props.globals.initNode("/it-autoflight/internal/heading-predicted", 0, "DOUBLE"),
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lnavAdvanceNm: props.globals.initNode("/it-autoflight/internal/lnav-advance-nm", 0, "DOUBLE"),
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minVs: props.globals.initNode("/it-autoflight/internal/min-vs", -500, "INT"),
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maxVs: props.globals.initNode("/it-autoflight/internal/max-vs", 500, "INT"),
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navHeadingErrorDeg: props.globals.initNode("/it-autoflight/internal/nav-heading-error-deg", 0, "DOUBLE"),
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navHeadingErrorDegTemp: 0,
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vs: props.globals.initNode("/it-autoflight/internal/vert-speed-fpm", 0, "DOUBLE"),
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vsTemp: 0,
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};
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var Output = {
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ap1: props.globals.initNode("/it-autoflight/output/ap1", 0, "BOOL"),
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ap1Temp: 0,
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ap2: props.globals.initNode("/it-autoflight/output/ap2", 0, "BOOL"),
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ap2Temp: 0,
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apprArm: props.globals.initNode("/it-autoflight/output/appr-armed", 0, "BOOL"),
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athr: props.globals.initNode("/it-autoflight/output/athr", 0, "BOOL"),
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athrTemp: 0,
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fd1: props.globals.initNode("/it-autoflight/output/fd1", 1, "BOOL"),
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fd1Temp: 0,
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fd2: props.globals.initNode("/it-autoflight/output/fd2", 1, "BOOL"),
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fd2Temp: 0,
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lat: props.globals.initNode("/it-autoflight/output/lat", 5, "INT"),
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latTemp: 5,
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lnavArm: props.globals.initNode("/it-autoflight/output/lnav-armed", 0, "BOOL"),
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locArm: props.globals.initNode("/it-autoflight/output/loc-armed", 0, "BOOL"),
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thrMode: props.globals.initNode("/it-autoflight/output/thr-mode", 2, "INT"),
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vert: props.globals.initNode("/it-autoflight/output/vert", 7, "INT"),
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vertTemp: 7,
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};
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var Text = {
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lat: props.globals.initNode("/it-autoflight/mode/lat", "T/O", "STRING"),
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thr: props.globals.initNode("/it-autoflight/mode/thr", "PITCH", "STRING"),
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vert: props.globals.initNode("/it-autoflight/mode/vert", "T/O CLB", "STRING"),
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vertTemp: "T/O CLB",
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};
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var Settings = {
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reducAglFt: props.globals.initNode("/it-autoflight/settings/accel-agl-ft", 1500, "INT"), # Changable from MCDU, eventually set to 1500 above runway
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};
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var Sound = {
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apOff: props.globals.initNode("/it-autoflight/sound/apoffsound", 0, "BOOL"), # Is this still needed??? -JD
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enableApOff: 0,
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};
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# A3XX Custom
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var Custom = {
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apFdOn: 0,
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hdgTime: props.globals.getNode("/modes/fcu/hdg-time", 1),
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ndTrkSel: [props.globals.getNode("/instrumentation/efis[0]/trk-selected", 1), props.globals.getNode("/instrumentation/efis[1]/trk-selected", 1)],
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showHdg: props.globals.initNode("/it-autoflight/custom/show-hdg", 1, "BOOL"),
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trkFpa: props.globals.initNode("/it-autoflight/custom/trk-fpa", 0, "BOOL"),
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Input: {
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spdManaged: props.globals.getNode("/it-autoflight/input/spd-managed", 1),
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},
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Output: {
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fmaPower: props.globals.initNode("/it-autoflight/output/fma-pwr", 0, "BOOL"),
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vsFCU: props.globals.initNode("/it-autoflight/output/vs-fcu-display", "", "STRING"),
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},
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Sound: {
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athrOff: props.globals.initNode("/it-autoflight/sound/athrsound", 0, "BOOL"),
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enableAthrOff: 0,
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},
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ThrLock: props.globals.getNode("/fdm/jsbsim/fadec/thr-locked", 1)
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};
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var ITAF = {
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init: func() {
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Custom.ndTrkSel[0].setBoolValue(0);
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Custom.ndTrkSel[1].setBoolValue(0);
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Custom.trkFpa.setBoolValue(0);
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Input.ktsMach.setBoolValue(0);
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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(1);
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Input.fd2.setBoolValue(1);
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Input.hdg.setValue(360);
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Input.alt.setValue(10000);
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Input.vs.setValue(0);
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Custom.Output.vsFCU.setValue(left(sprintf("%+05.0f",0),3));
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Input.fpa.setValue(0);
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Input.lat.setValue(9);
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Input.vert.setValue(9);
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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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Custom.Input.spdManaged.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(1);
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Output.fd2.setBoolValue(1);
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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.thrMode.setValue(0);
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Output.lat.setValue(9);
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Output.vert.setValue(9);
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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(100);
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Input.mach.setValue(0.5);
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Text.thr.setValue("THRUST");
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updateFma.arm();
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me.updateLatText("");
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me.updateVertText("");
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Custom.showHdg.setBoolValue(1);
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Custom.Output.fmaPower.setBoolValue(1);
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ManagedSPD.stop();
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loopTimer.start();
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slowLoopTimer.start();
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},
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loop: func() {
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Output.latTemp = Output.lat.getValue();
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Output.vertTemp = Output.vert.getValue();
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# VOR/ILS Revision
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if (Output.latTemp == 2 or Output.vertTemp == 2 or Output.vertTemp == 6) {
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me.checkRadioRevision(Output.latTemp, Output.vertTemp);
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}
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Gear.wow1Temp = Gear.wow1.getBoolValue();
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Gear.wow2Temp = Gear.wow2.getBoolValue();
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Output.ap1Temp = Output.ap1.getBoolValue();
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Output.ap2Temp = Output.ap2.getBoolValue();
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Output.latTemp = Output.lat.getValue();
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Output.vertTemp = Output.vert.getValue();
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Text.vertTemp = Text.vert.getValue();
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Position.gearAglFtTemp = Position.gearAglFt.getValue();
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Internal.vsTemp = Internal.vs.getValue();
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Position.indicatedAltitudeFtTemp = Position.indicatedAltitudeFt.getValue();
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# Update VLS / VMAX for autothrust
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FMGCNodes.vmax.setValue(FMGCInternal.maxspeed);
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FMGCNodes.vlsMin.setValue(FMGCInternal.vls_min);
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# LNAV Engagement
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if (Output.lnavArm.getBoolValue()) {
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me.checkLnav(1);
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}
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# VOR/LOC or ILS/LOC Capture
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if (Output.locArm.getBoolValue()) {
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me.checkLoc(1);
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}
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# G/S Capture
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if (Output.apprArm.getBoolValue()) {
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me.checkAppr(1);
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}
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# Autoland Logic
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if (Output.latTemp == 2) {
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if (Position.gearAglFtTemp <= 50) { # ALIGN
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me.setLatMode(4);
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}
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}
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if (Output.vertTemp == 2) {
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if (Position.gearAglFtTemp <= 400 and Position.gearAglFtTemp >= 5) {
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me.updateVertText("LAND");
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if (Position.gearAglFtTemp <= 50) {
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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 (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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# FLCH Engagement
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if (Text.vertTemp == "T/O CLB") {
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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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if (Output.vertTemp != 0) {
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Internal.alt.setValue(Input.alt.getValue());
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}
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Internal.altTemp = Internal.alt.getValue();
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Internal.altDiff = Internal.altTemp - Position.indicatedAltitudeFtTemp;
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if (Output.vertTemp != 0 and Output.vertTemp != 2 and Output.vertTemp != 6 and Output.vertTemp != 9) {
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Internal.captVs = math.clamp(math.round(abs(Internal.vs.getValue()) / 5, 100), 50, 2500); # Capture limits
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Custom.apFdOn = Output.ap1Temp or Output.ap2Temp or Output.fd1.getBoolValue() or Output.fd2.getBoolValue();
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if (abs(Internal.altDiff) <= Internal.captVs and !Gear.wow1Temp and !Gear.wow2Temp and Custom.apFdOn) {
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if (Internal.altTemp >= Position.indicatedAltitudeFtTemp and Internal.vsTemp >= -25) { # Don't capture if we are going the wrong way
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me.setVertMode(3);
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} else if (Internal.altTemp < Position.indicatedAltitudeFtTemp and Internal.vsTemp <= 25) { # Don't capture if we are going the wrong way
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me.setVertMode(3);
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}
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}
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}
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# Altitude Hold Min/Max Reset
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if (Internal.altCaptureActive) {
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if (abs(Internal.altDiff) <= 20 and Text.vert.getValue() != "ALT HLD") {
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me.resetClimbRateLim();
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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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me.updateThrustMode();
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# Custom Stuff Below
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# Heading Sync
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if (!Custom.showHdg.getBoolValue()) {
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Input.hdg.setValue(Misc.pfdHeadingScale.getValue());
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}
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# Preselect Heading
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if (Output.latTemp != 0 and Output.latTemp != 9) { # Modes that always show HDG
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if (Custom.hdgTime.getValue() + 45 >= Misc.elapsedSec.getValue()) {
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Custom.showHdg.setBoolValue(1);
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} else {
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Custom.showHdg.setBoolValue(0);
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}
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}
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# Misc
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if (Output.ap1Temp == 1 or Output.ap2Temp == 1) { # Trip AP off
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if (abs(Controls.aileron.getValue()) >= 0.2 or abs(Controls.elevator.getValue()) >= 0.2 or abs(Controls.rudder.getValue()) >= 0.2 or abs(Controls.aileron2.getValue()) >= 0.2 or abs(Controls.elevator2.getValue()) >= 0.2 or abs(Controls.rudder2.getValue()) >= 0.2) {
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fcu.apOff("hard", 0);
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}
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}
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if ((systems.FADEC.n1Mode[0].getValue() > 0 or systems.FADEC.n1Mode[1].getValue() > 0) and Output.athr.getBoolValue()) {
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fcu.athrOff("hard");
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}
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},
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slowLoop: func() {
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Velocities.trueAirspeedKtTemp = Velocities.trueAirspeedKt.getValue();
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FPLN.activeTemp = FPLN.active.getValue();
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FPLN.currentWpTemp = FPLN.currentWp.getValue();
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# Bank Limit
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if (Velocities.trueAirspeedKtTemp >= 420) {
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Internal.bankLimitAuto = 15;
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} else if (Velocities.trueAirspeedKtTemp >= 340) {
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Internal.bankLimitAuto = 20;
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} else {
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Internal.bankLimitAuto = 30;
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}
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Internal.bankLimit.setValue(Internal.bankLimitAuto);
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# If in LNAV mode and route is not longer active, switch to HDG HLD
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if (Output.lat.getValue() == 1) { # Only evaulate the rest of the condition if we are in LNAV mode
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if (flightPlanController.num[2].getValue() == 0 or !FPLN.active.getBoolValue()) {
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me.setLatMode(3);
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}
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}
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# Waypoint Advance Logic
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if (flightPlanController.num[2].getValue() > 0 and FPLN.activeTemp == 1) {
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if ((FPLN.currentWpTemp + 1) < flightPlanController.num[2].getValue()) {
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Velocities.groundspeedMps = Velocities.groundspeedKt.getValue() * 0.5144444444444;
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FPLN.wpFlyFrom = FPLN.currentWpTemp;
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if (FPLN.wpFlyFrom < 0) {
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FPLN.wpFlyFrom = 0;
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}
|
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FPLN.currentCourse = fmgc.wpCourse[2][FPLN.wpFlyFrom].getValue();
|
|
FPLN.wpFlyTo = FPLN.currentWpTemp + 1;
|
|
FPLN.nextCourse = fmgc.wpCourse[2][FPLN.wpFlyTo].getValue();
|
|
FPLN.maxBankLimit = Internal.bankLimit.getValue();
|
|
|
|
FPLN.deltaAngle = math.abs(geo.normdeg180(FPLN.currentCourse - FPLN.nextCourse));
|
|
FPLN.maxBank = FPLN.deltaAngle * 1.5;
|
|
if (FPLN.maxBank > FPLN.maxBankLimit) {
|
|
FPLN.maxBank = FPLN.maxBankLimit;
|
|
}
|
|
FPLN.radius = (Velocities.groundspeedMps * Velocities.groundspeedMps) / (9.81 * math.tan(FPLN.maxBank / 57.2957795131));
|
|
FPLN.deltaAngleRad = (180 - FPLN.deltaAngle) / 114.5915590262;
|
|
FPLN.R = FPLN.radius / math.sin(FPLN.deltaAngleRad);
|
|
FPLN.distCoeff = FPLN.deltaAngle * -0.011111 + 2;
|
|
if (FPLN.distCoeff < 1) {
|
|
FPLN.distCoeff = 1;
|
|
}
|
|
FPLN.turnDist = math.cos(FPLN.deltaAngleRad) * FPLN.R * FPLN.distCoeff / 1852;
|
|
if (Gear.wow0.getBoolValue() and FPLN.turnDist < 1) {
|
|
FPLN.turnDist = 1;
|
|
}
|
|
Internal.lnavAdvanceNm.setValue(FPLN.turnDist);
|
|
|
|
# Advance logic done by flightplan controller
|
|
if (FPLN.wp0Dist.getValue() <= FPLN.turnDist and !Gear.wow1.getBoolValue()) {
|
|
flightPlanController.autoSequencing();
|
|
}
|
|
|
|
#if (FPLN.wp0Dist.getValue() <= FPLN.turnDist and !Gear.wow1.getBoolValue() and fmgc.flightPlanController.flightplans[2].getWP(FPLN.currentWpTemp).fly_type == "flyBy") {
|
|
# flightPlanController.autoSequencing();
|
|
#} elsif (FPLN.wp0Dist.getValue() <= 0.1) {
|
|
# flightPlanController.autoSequencing();
|
|
#}
|
|
}
|
|
}
|
|
},
|
|
ap1Master: func(s) {
|
|
if (s == 1) {
|
|
if (Output.vert.getValue() != 6 and !Gear.wow1.getBoolValue() and !Gear.wow2.getBoolValue() and systems.ELEC.Bus.acEss.getValue() >= 110 and fbw.FBW.apOff == 0 and Position.gearAglFt.getValue() >= 100) {
|
|
me.revertBasicMode();
|
|
Output.ap1.setBoolValue(1);
|
|
Output.latTemp = Output.lat.getValue();
|
|
if (Output.ap2.getBoolValue() and !Output.apprArm.getBoolValue() and Output.latTemp != 2 and Output.latTemp != 4) {
|
|
me.ap2Master(0);
|
|
}
|
|
Sound.enableApOff = 1;
|
|
Sound.apOff.setBoolValue(0);
|
|
}
|
|
} else {
|
|
Output.ap1.setBoolValue(0);
|
|
me.apOffFunction();
|
|
}
|
|
Output.ap1Temp = Output.ap1.getBoolValue();
|
|
if (Input.ap1.getBoolValue() != Output.ap1Temp) {
|
|
Input.ap1.setBoolValue(Output.ap1Temp);
|
|
}
|
|
},
|
|
ap2Master: func(s) {
|
|
if (s == 1) {
|
|
if (Output.vert.getValue() != 6 and !Gear.wow1.getBoolValue() and !Gear.wow2.getBoolValue() and systems.ELEC.Bus.acEss.getValue() >= 110 and fbw.FBW.apOff == 0 and Position.gearAglFt.getValue() >= 100) {
|
|
me.revertBasicMode();
|
|
Output.ap2.setBoolValue(1);
|
|
Output.latTemp = Output.lat.getValue();
|
|
if (Output.ap1.getBoolValue() and !Output.apprArm.getBoolValue() and Output.latTemp != 2 and Output.latTemp != 4) {
|
|
me.ap1Master(0);
|
|
}
|
|
Sound.enableApOff = 1;
|
|
Sound.apOff.setBoolValue(0);
|
|
}
|
|
} else {
|
|
Output.ap2.setBoolValue(0);
|
|
me.apOffFunction();
|
|
}
|
|
Output.ap2Temp = Output.ap2.getBoolValue();
|
|
if (Input.ap2.getBoolValue() != Output.ap2Temp) {
|
|
Input.ap2.setBoolValue(Output.ap2Temp);
|
|
}
|
|
},
|
|
apOffFunction: func() {
|
|
if (!Output.ap1.getBoolValue() and !Output.ap2.getBoolValue()) { # Only do if both APs are off
|
|
me.updateFma();
|
|
if (Sound.enableApOff) {
|
|
Sound.apOff.setBoolValue(1);
|
|
Sound.enableApOff = 0;
|
|
}
|
|
}
|
|
},
|
|
athrMaster: func(s) {
|
|
if (s == 1) {
|
|
if (systems.ELEC.Bus.acEss.getValue() >= 110 and !pts.FMGC.CasCompare.casRejectAll.getBoolValue() and fbw.FBW.apOff == 0 and systems.FADEC.n1Mode[0].getValue() == 0 and systems.FADEC.n1Mode[1].getValue() == 0) {
|
|
Output.athr.setBoolValue(1);
|
|
Custom.ThrLock.setValue(0);
|
|
Custom.Sound.enableAthrOff = 1;
|
|
Custom.Sound.athrOff.setBoolValue(0);
|
|
}
|
|
} else {
|
|
Output.athr.setBoolValue(0);
|
|
if (Custom.Sound.enableAthrOff) {
|
|
Custom.Sound.athrOff.setBoolValue(1);
|
|
Custom.Sound.enableAthrOff = 0;
|
|
}
|
|
}
|
|
Output.athrTemp = Output.athr.getBoolValue();
|
|
if (Input.athr.getBoolValue() != Output.athrTemp) {
|
|
Input.athr.setBoolValue(Output.athrTemp);
|
|
}
|
|
},
|
|
fd1Master: func(s) {
|
|
if (s == 1) {
|
|
Output.fd1.setBoolValue(1);
|
|
me.updateFma();
|
|
} else {
|
|
Output.fd1.setBoolValue(0);
|
|
if (!Output.fd2.getBoolValue()) {
|
|
me.updateFma();
|
|
}
|
|
}
|
|
Output.fd1Temp = Output.fd1.getBoolValue();
|
|
if (Input.fd1.getBoolValue() != Output.fd1Temp) {
|
|
Input.fd1.setBoolValue(Output.fd1Temp);
|
|
}
|
|
},
|
|
fd2Master: func(s) {
|
|
if (s == 1) {
|
|
Output.fd2.setBoolValue(1);
|
|
me.updateFma();
|
|
} else {
|
|
Output.fd2.setBoolValue(0);
|
|
if (!Output.fd1.getBoolValue()) {
|
|
me.updateFma();
|
|
}
|
|
}
|
|
Output.fd2Temp = Output.fd2.getBoolValue();
|
|
if (Input.fd2.getBoolValue() != Output.fd2Temp) {
|
|
Input.fd2.setBoolValue(Output.fd2Temp);
|
|
}
|
|
},
|
|
setLatMode: func(n) {
|
|
Output.vertTemp = Output.vert.getValue();
|
|
if (n == 0) { # HDG SEL
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(0);
|
|
me.updateApprArm(0);
|
|
Output.lat.setValue(0);
|
|
Custom.showHdg.setBoolValue(1);
|
|
me.updateLatText("HDG");
|
|
if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
|
|
me.setVertMode(1);
|
|
}
|
|
} else if (n == 1) { # LNAV
|
|
me.updateLocArm(0);
|
|
me.updateApprArm(0);
|
|
me.checkLnav(0);
|
|
} else if (n == 2) { # VOR/LOC
|
|
me.updateLnavArm(0);
|
|
me.checkLoc(0);
|
|
} else if (n == 3) { # HDG HLD
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(0);
|
|
me.updateApprArm(0);
|
|
me.syncHdg();
|
|
Output.lat.setValue(0);
|
|
Custom.showHdg.setBoolValue(1);
|
|
me.updateLatText("HDG");
|
|
if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
|
|
me.setVertMode(1);
|
|
}
|
|
} else if (n == 4) { # ALIGN
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(0);
|
|
me.updateApprArm(0);
|
|
Output.lat.setValue(4);
|
|
Custom.showHdg.setBoolValue(0);
|
|
me.updateLatText("ALGN");
|
|
} else if (n == 5) { # RWY
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(0);
|
|
me.updateApprArm(0);
|
|
Output.lat.setValue(5);
|
|
Custom.showHdg.setBoolValue(0);
|
|
me.updateLatText("T/O");
|
|
} else if (n == 9) { # NONE
|
|
me.updateLocArm(0);
|
|
Output.lat.setValue(9);
|
|
Custom.showHdg.setBoolValue(1);
|
|
me.updateLatText("");
|
|
}
|
|
},
|
|
setLatArm: func(n) {
|
|
if (n == 0) {
|
|
me.updateLnavArm(0);
|
|
Custom.showHdg.setBoolValue(1);
|
|
} else if (n == 1) {
|
|
if (flightPlanController.num[2].getValue() > 0 and FPLN.active.getBoolValue()) {
|
|
me.updateLnavArm(1);
|
|
Custom.showHdg.setBoolValue(0);
|
|
}
|
|
} else if (n == 3) {
|
|
me.syncHdg();
|
|
me.updateLnavArm(0);
|
|
Custom.showHdg.setBoolValue(1);
|
|
}
|
|
},
|
|
setVertMode: func(n) {
|
|
Input.altDiff = Input.alt.getValue() - Position.indicatedAltitudeFt.getValue();
|
|
if (n == 0) { # ALT HLD
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(0);
|
|
me.resetClimbRateLim();
|
|
me.updateVertText("ALT HLD");
|
|
me.syncAlt();
|
|
me.updateThrustMode();
|
|
} else if (n == 1) { # V/S
|
|
if (abs(Input.altDiff) >= 25) {
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(1);
|
|
me.updateVertText("V/S");
|
|
me.syncVs();
|
|
me.updateThrustMode();
|
|
} else {
|
|
me.updateApprArm(0);
|
|
}
|
|
} else if (n == 2) { # G/S
|
|
me.updateLnavArm(0);
|
|
me.checkLoc(0);
|
|
me.checkAppr(0);
|
|
} else if (n == 3) { # ALT CAP
|
|
Internal.flchActive = 0;
|
|
Output.vert.setValue(0);
|
|
me.setClimbRateLim();
|
|
Internal.altCaptureActive = 1;
|
|
me.updateVertText("ALT CAP");
|
|
me.updateThrustMode();
|
|
} else if (n == 4) { # FLCH
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(1);
|
|
Internal.alt.setValue(Input.alt.getValue());
|
|
Internal.altDiff = Internal.alt.getValue() - Position.indicatedAltitudeFt.getValue();
|
|
if (abs(Internal.altDiff) >= 250) { # SPD CLB or SPD DES
|
|
Internal.altCaptureActive = 0;
|
|
Output.vert.setValue(4);
|
|
Internal.flchActive = 1;
|
|
Internal.alt.setValue(Input.alt.getValue());
|
|
me.updateThrustMode();
|
|
} else { # ALT CAP
|
|
Internal.flchActive = 0;
|
|
Internal.alt.setValue(Input.alt.getValue());
|
|
Internal.altCaptureActive = 1;
|
|
Output.vert.setValue(0);
|
|
me.updateVertText("ALT CAP");
|
|
me.updateThrustMode();
|
|
}
|
|
} else if (n == 5) { # FPA
|
|
if (abs(Input.altDiff) >= 25) {
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(5);
|
|
me.updateVertText("FPA");
|
|
me.syncFpa();
|
|
me.updateThrustMode();
|
|
} else {
|
|
me.updateApprArm(0);
|
|
}
|
|
} else if (n == 6) { # FLARE/ROLLOUT
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(6);
|
|
me.updateVertText("FLARE");
|
|
me.updateThrustMode();
|
|
} else if (n == 7) { # T/O CLB or G/A CLB, text is set by TOGA selector
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(7);
|
|
me.updateThrustMode();
|
|
} else if (n == 9) { # NONE
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(9);
|
|
me.updateVertText("");
|
|
me.updateThrustMode();
|
|
}
|
|
},
|
|
updateThrustMode: func() {
|
|
Output.vertTemp = Output.vert.getValue();
|
|
if (Output.athr.getBoolValue() and Output.vertTemp != 7 and (Output.ap1.getBoolValue() or Output.ap2.getBoolValue()) and Position.gearAglFt.getValue() <= 30 and (Output.vertTemp == 2 or Output.vertTemp == 6)) {
|
|
# Manual says 40 feet - but video reference shows 30!
|
|
Output.thrMode.setValue(1);
|
|
Text.thr.setValue("RETARD");
|
|
} else if (Output.vertTemp == 4) {
|
|
if (Internal.alt.getValue() >= Position.indicatedAltitudeFt.getValue()) {
|
|
Output.thrMode.setValue(2);
|
|
Text.thr.setValue("PITCH");
|
|
if (Internal.flchActive and Text.vert.getValue() != "SPD CLB") {
|
|
me.updateVertText("SPD CLB");
|
|
}
|
|
} else {
|
|
Output.thrMode.setValue(1);
|
|
Text.thr.setValue("PITCH");
|
|
if (Internal.flchActive and Text.vert.getValue() != "SPD DES") {
|
|
me.updateVertText("SPD DES");
|
|
}
|
|
}
|
|
} else if (Output.vertTemp == 7) {
|
|
Output.thrMode.setValue(2);
|
|
Text.thr.setValue("PITCH");
|
|
} else {
|
|
Output.thrMode.setValue(0);
|
|
Text.thr.setValue("THRUST");
|
|
}
|
|
},
|
|
activateLnav: func() {
|
|
if (Output.lat.getValue() != 1) {
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(0);
|
|
me.updateApprArm(0);
|
|
Output.lat.setValue(1);
|
|
Custom.showHdg.setBoolValue(0);
|
|
me.updateLatText("LNAV");
|
|
if (Output.vertTemp == 2 or Output.vertTemp == 6) { # Also cancel G/S or FLARE if active
|
|
me.setVertMode(1);
|
|
}
|
|
}
|
|
},
|
|
activateLoc: func() {
|
|
if (Output.lat.getValue() != 2) {
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(0);
|
|
Output.lat.setValue(2);
|
|
Custom.showHdg.setBoolValue(0);
|
|
me.updateLatText("LOC");
|
|
}
|
|
},
|
|
activateGs: func() {
|
|
if (Output.vert.getValue() != 2) {
|
|
Internal.flchActive = 0;
|
|
Internal.altCaptureActive = 0;
|
|
me.updateApprArm(0);
|
|
Output.vert.setValue(2);
|
|
me.updateVertText("G/S");
|
|
me.updateThrustMode();
|
|
}
|
|
},
|
|
checkLnav: func(t) {
|
|
FPLN.activeTemp = FPLN.active.getBoolValue();
|
|
if (flightPlanController.num[2].getValue() > 0 and FPLN.activeTemp and Position.gearAglFt.getValue() >= 30) {
|
|
me.activateLnav();
|
|
} else if (FPLN.activeTemp and Output.lat.getValue() != 1 and t != 1) {
|
|
me.updateLnavArm(1);
|
|
}
|
|
},
|
|
checkFlch: func(a) {
|
|
if (Position.indicatedAltitudeFt.getValue() >= a and a != 0 and !Gear.wow1.getBoolValue() and !Gear.wow2.getBoolValue()) {
|
|
me.setVertMode(4);
|
|
}
|
|
},
|
|
checkLoc: func(t) {
|
|
if (Radio.inRange.getBoolValue()) { # # Only evaulate the rest of the condition unless we are in range
|
|
Internal.navHeadingErrorDegTemp = Internal.navHeadingErrorDeg.getValue();
|
|
Radio.locDeflTemp = Radio.locDefl.getValue();
|
|
Radio.signalQualityTemp = Radio.signalQuality.getValue();
|
|
if (abs(Radio.locDeflTemp) <= 0.95 and Radio.locDeflTemp != 0 and Radio.signalQualityTemp >= 0.99) {
|
|
if (Radio.locDeflTemp >= 0 and Internal.navHeadingErrorDegTemp <= 0) {
|
|
me.activateLoc();
|
|
} else if (Radio.locDeflTemp < 0 and Internal.navHeadingErrorDegTemp >= 0) {
|
|
me.activateLoc();
|
|
}
|
|
|
|
if (t != 1) { # Do not do this if loop calls it
|
|
if (Output.lat.getValue() != 2) {
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(1);
|
|
}
|
|
}
|
|
} else if (t != 1) { # Do not do this if loop calls it
|
|
if (Output.lat.getValue() != 2) {
|
|
me.updateLnavArm(0);
|
|
me.updateLocArm(1);
|
|
}
|
|
}
|
|
} else {
|
|
Radio.signalQuality.setValue(0); # Prevent bad behavior due to FG not updating it when not in range
|
|
me.updateLocArm(0);
|
|
}
|
|
},
|
|
checkAppr: func(t) {
|
|
if (Radio.inRange.getBoolValue()) { # # Only evaulate the rest of the condition unless we are in range
|
|
Radio.gsDeflTemp = Radio.gsDefl.getValue();
|
|
if (abs(Radio.gsDeflTemp) <= 0.2 and Radio.gsDeflTemp != 0 and Output.lat.getValue() == 2) { # Only capture if LOC is active
|
|
me.activateGs();
|
|
} else if (t != 1) { # Do not do this if loop calls it
|
|
if (Output.vert.getValue() != 2) {
|
|
me.updateApprArm(1);
|
|
}
|
|
}
|
|
} else {
|
|
Radio.signalQuality.setValue(0); # Prevent bad behavior due to FG not updating it when not in range
|
|
me.updateApprArm(0);
|
|
}
|
|
},
|
|
checkRadioRevision: func(l, v) { # Revert mode if signal lost
|
|
if (!Radio.inRange.getBoolValue()) {
|
|
if (l == 4 or v == 6) {
|
|
me.ap1Master(0);
|
|
me.ap2Master(0);
|
|
me.setLatMode(3);
|
|
me.setVertMode(1);
|
|
} else {
|
|
me.setLatMode(3); # Also cancels G/S if active
|
|
}
|
|
}
|
|
},
|
|
setClimbRateLim: func() {
|
|
Internal.vsTemp = Internal.vs.getValue();
|
|
if (Internal.alt.getValue() >= Position.indicatedAltitudeFt.getValue()) {
|
|
Internal.maxVs.setValue(math.round(Internal.vsTemp));
|
|
Internal.minVs.setValue(-500);
|
|
} else {
|
|
Internal.maxVs.setValue(500);
|
|
Internal.minVs.setValue(math.round(Internal.vsTemp));
|
|
}
|
|
},
|
|
resetClimbRateLim: func() {
|
|
Internal.minVs.setValue(-500);
|
|
Internal.maxVs.setValue(500);
|
|
},
|
|
takeoffGoAround: func() {
|
|
Output.vertTemp = Output.vert.getValue();
|
|
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
|
|
me.updateVertText("G/A CLB");
|
|
me.syncKtsGa();
|
|
if (Gear.wow1.getBoolValue() or Gear.wow2.getBoolValue()) {
|
|
me.ap1Master(0);
|
|
me.ap2Master(0);
|
|
}
|
|
} else if (Gear.wow1Temp or Gear.wow2Temp) {
|
|
me.athrMaster(1);
|
|
if (Output.lat.getValue() != 5) { # Don't accidently disarm LNAV
|
|
me.setLatMode(5);
|
|
}
|
|
me.setVertMode(7);
|
|
me.updateVertText("T/O CLB");
|
|
}
|
|
},
|
|
syncKts: func() {
|
|
Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), 100, 399));
|
|
},
|
|
syncKtsGa: func() { # Same as syncKts, except doesn't go below V2
|
|
Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), FMGCInternal.v2, 399));
|
|
},
|
|
syncMach: func() {
|
|
Input.mach.setValue(math.clamp(math.round(Velocities.indicatedMach.getValue(), 0.001), 0.1, 0.99));
|
|
},
|
|
syncHdg: func() {
|
|
Input.hdg.setValue(math.round(Internal.hdgPredicted.getValue())); # Switches to track automatically
|
|
},
|
|
syncAlt: func() {
|
|
Input.alt.setValue(math.clamp(math.round(Internal.altPredicted.getValue(), 100), 0, 50000));
|
|
Internal.alt.setValue(math.clamp(math.round(Internal.altPredicted.getValue(), 100), 0, 50000));
|
|
},
|
|
tempVS: 0,
|
|
syncVs: func() {
|
|
me.tempVS = math.clamp(math.round(Internal.vs.getValue(), 100), -6000, 6000);
|
|
Input.vs.setValue(me.tempVS);
|
|
fmgc.Custom.Output.vsFCU.setValue(left(sprintf("%+05.0f",me.tempVS),3));
|
|
},
|
|
syncFpa: func() {
|
|
Input.fpa.setValue(math.clamp(math.round(Internal.fpa.getValue(), 0.1), -9.9, 9.9));
|
|
},
|
|
# Custom Stuff Below
|
|
updateFma: func() {
|
|
if (!Output.ap1.getBoolValue() and !Output.ap2.getBoolValue() and !Output.fd1.getBoolValue() and !Output.fd2.getBoolValue()) {
|
|
me.setLatMode(9);
|
|
me.setVertMode(9);
|
|
me.setLatArm(0);
|
|
Custom.Output.fmaPower.setBoolValue(0);
|
|
} else {
|
|
Custom.Output.fmaPower.setBoolValue(1);
|
|
me.revertBasicMode();
|
|
}
|
|
},
|
|
revertBasicMode: func() {
|
|
if (!Gear.wow1.getBoolValue() and !Gear.wow2.getBoolValue()) { # Don't do this on ground
|
|
if (Output.lat.getValue() == 9) {
|
|
me.setLatMode(3);
|
|
}
|
|
if (Output.vert.getValue() == 9) {
|
|
if (Custom.trkFpa.getBoolValue()) {
|
|
me.setVertMode(5);
|
|
} else {
|
|
me.setVertMode(1);
|
|
}
|
|
}
|
|
}
|
|
},
|
|
disarmLoc: func() {
|
|
me.updateLocArm(0);
|
|
},
|
|
disarmAppr: func() {
|
|
me.updateApprArm(0);
|
|
},
|
|
toggleTrkFpa: func() {
|
|
if (Custom.trkFpa.getBoolValue()) {
|
|
me.trkFpaOff();
|
|
} else {
|
|
me.trkFpaOn();
|
|
}
|
|
},
|
|
trkFpaOn: func() {
|
|
Custom.trkFpa.setBoolValue(1);
|
|
if (Output.vert.getValue() == 1) {
|
|
Input.vert.setValue(5); # This way we only do this if all conditions are true
|
|
}
|
|
Input.trk.setBoolValue(1);
|
|
Custom.ndTrkSel[0].setBoolValue(1);
|
|
Custom.ndTrkSel[1].setBoolValue(1);
|
|
Input.hdgCalc = Input.hdg.getValue() + math.round(Internal.driftAngle.getValue());
|
|
if (Input.hdgCalc > 360) { # It's rounded, so this is ok. Otherwise do >= 360.5
|
|
Input.hdgCalc = Input.hdgCalc - 360;
|
|
} else if (Input.hdgCalc < 1) { # It's rounded, so this is ok. Otherwise do < 0.5
|
|
Input.hdgCalc = Input.hdgCalc + 360;
|
|
}
|
|
Input.hdg.setValue(Input.hdgCalc);
|
|
},
|
|
trkFpaOff: func() {
|
|
Custom.trkFpa.setBoolValue(0);
|
|
if (Output.vert.getValue() == 5) {
|
|
Input.vert.setValue(1); # This way we only do this if all conditions are true
|
|
}
|
|
Input.trk.setBoolValue(0);
|
|
Custom.ndTrkSel[0].setBoolValue(0);
|
|
Custom.ndTrkSel[1].setBoolValue(0);
|
|
Input.hdgCalc = Input.hdg.getValue() - math.round(Internal.driftAngle.getValue());
|
|
if (Input.hdgCalc > 360) { # It's rounded, so this is ok. Otherwise do >= 360.5
|
|
Input.hdgCalc = Input.hdgCalc - 360;
|
|
} else if (Input.hdgCalc < 1) { # It's rounded, so this is ok. Otherwise do < 0.5
|
|
Input.hdgCalc = Input.hdgCalc + 360;
|
|
}
|
|
Input.hdg.setValue(Input.hdgCalc);
|
|
},
|
|
updateLatText: func(t) {
|
|
Text.lat.setValue(t);
|
|
updateFma.lat();
|
|
},
|
|
updateVertText: func(t) {
|
|
Text.vert.setValue(t);
|
|
updateFma.vert();
|
|
},
|
|
updateLnavArm: func(n) {
|
|
Output.lnavArm.setBoolValue(n);
|
|
updateFma.arm();
|
|
},
|
|
updateLocArm: func(n) {
|
|
Output.locArm.setBoolValue(n);
|
|
updateFma.arm();
|
|
},
|
|
updateApprArm: func(n) {
|
|
Output.apprArm.setBoolValue(n);
|
|
updateFma.arm();
|
|
},
|
|
};
|
|
|
|
setlistener("/it-autoflight/input/ap1", func() {
|
|
Input.ap1Temp = Input.ap1.getBoolValue();
|
|
if (Input.ap1Temp != Output.ap1.getBoolValue()) {
|
|
ITAF.ap1Master(Input.ap1Temp);
|
|
}
|
|
});
|
|
|
|
setlistener("/it-autoflight/input/ap2", func() {
|
|
Input.ap2Temp = Input.ap2.getBoolValue();
|
|
if (Input.ap2Temp != Output.ap2.getBoolValue()) {
|
|
ITAF.ap2Master(Input.ap2Temp);
|
|
}
|
|
});
|
|
|
|
setlistener("/it-autoflight/input/athr", func() {
|
|
Input.athrTemp = Input.athr.getBoolValue();
|
|
if (Input.athrTemp != Output.athr.getBoolValue()) {
|
|
ITAF.athrMaster(Input.athrTemp);
|
|
}
|
|
});
|
|
|
|
setlistener("/it-autoflight/input/fd1", func() {
|
|
Input.fd1Temp = Input.fd1.getBoolValue();
|
|
if (Input.fd1Temp != Output.fd1.getBoolValue()) {
|
|
ITAF.fd1Master(Input.fd1Temp);
|
|
}
|
|
});
|
|
|
|
setlistener("/it-autoflight/input/fd2", func() {
|
|
Input.fd2Temp = Input.fd2.getBoolValue();
|
|
if (Input.fd2Temp != Output.fd2.getBoolValue()) {
|
|
ITAF.fd2Master(Input.fd2Temp);
|
|
}
|
|
});
|
|
|
|
|
|
setlistener("/it-autoflight/input/kts-mach", func() {
|
|
if (Output.vert.getValue() == 7) { # Mach is not allowed in Mode 7, and don't sync
|
|
if (Input.ktsMach.getBoolValue()) {
|
|
Input.ktsMach.setBoolValue(0);
|
|
}
|
|
} else {
|
|
if (Input.ktsMach.getBoolValue()) {
|
|
ITAF.syncMach();
|
|
} else {
|
|
ITAF.syncKts();
|
|
}
|
|
}
|
|
}, 0, 0);
|
|
|
|
setlistener("/it-autoflight/input/toga", func() {
|
|
if (Input.toga.getBoolValue()) {
|
|
ITAF.takeoffGoAround();
|
|
Input.toga.setBoolValue(0);
|
|
}
|
|
});
|
|
|
|
setlistener("/it-autoflight/input/lat", func() {
|
|
Input.latTemp = Input.lat.getValue();
|
|
Output.ap1Temp = Output.ap1.getBoolValue();
|
|
Output.ap2Temp = Output.ap2.getBoolValue();
|
|
Output.fd1Temp = Output.fd1.getBoolValue();
|
|
Output.fd2Temp = Output.fd2.getBoolValue();
|
|
|
|
if (!Gear.wow1.getBoolValue() and !Gear.wow2.getBoolValue()) {
|
|
if (Output.ap1Temp or Output.ap2Temp or Output.fd1Temp or Output.fd2Temp) {
|
|
ITAF.setLatMode(Input.latTemp);
|
|
} else {
|
|
ITAF.setLatMode(9);
|
|
}
|
|
} else {
|
|
if (Output.ap1Temp or Output.ap2Temp or Output.fd1Temp or Output.fd2Temp) {
|
|
ITAF.setLatArm(Input.latTemp);
|
|
} else {
|
|
ITAF.setLatArm(0);
|
|
}
|
|
}
|
|
});
|
|
|
|
setlistener("/it-autoflight/input/vert", func() {
|
|
if (!Gear.wow1.getBoolValue() and !Gear.wow2.getBoolValue() and (Output.ap1.getBoolValue() or Output.ap2.getBoolValue() or Output.fd1.getBoolValue() or Output.fd2.getBoolValue())) {
|
|
ITAF.setVertMode(Input.vert.getValue());
|
|
} else {
|
|
ITAF.setVertMode(9);
|
|
}
|
|
});
|
|
|
|
# Mode Reversions
|
|
setlistener(pts.Systems.Navigation.ADR.Output.overspeed, func(v) {
|
|
if (v.getBoolValue() and !Output.ap1.getBoolValue() and !Output.ap2.getBoolValue() and Output.athr.getBoolValue() and Modes.PFD.FMA.pitchMode.getValue() == "OP CLB" and Modes.PFD.FMA.throttle.getValue() == "THR CLB") {
|
|
Input.fd1.setValue(0);
|
|
Input.fd2.setValue(0);
|
|
ecam.aural[5].setBoolValue(0);
|
|
settimer(func() {
|
|
ecam.aural[5].setBoolValue(1);
|
|
}, 0.15);
|
|
}
|
|
}, 0, 0);
|
|
|
|
setlistener(pts.Systems.Navigation.ADR.Output.underspeed, func(v) {
|
|
if (v.getBoolValue() and !Output.ap1.getBoolValue() and !Output.ap2.getBoolValue() and Output.athr.getBoolValue() and Modes.PFD.FMA.pitchMode.getValue() == "OP DES" and Modes.PFD.FMA.throttle.getValue() == "THR IDLE") {
|
|
Input.fd1.setValue(0);
|
|
Input.fd2.setValue(0);
|
|
ecam.aural[5].setBoolValue(0);
|
|
settimer(func() {
|
|
ecam.aural[5].setBoolValue(1);
|
|
}, 0.15);
|
|
}
|
|
}, 0, 0);
|
|
|
|
|
|
setlistener("/sim/signals/fdm-initialized", func {
|
|
ITAF.init();
|
|
});
|
|
|
|
# For Canvas Nav Display.
|
|
setlistener("/it-autoflight/input/hdg", func() {
|
|
pts.Autopilot.Settings.headingBugDeg.setValue(Input.hdg.getValue());
|
|
}, 0, 0);
|
|
|
|
setlistener("/it-autoflight/internal/alt", func() {
|
|
pts.Autopilot.Settings.targetAltitudeFt.setValue(Internal.alt.getValue());
|
|
}, 0, 0);
|
|
|
|
var loopTimer = maketimer(0.1, ITAF, ITAF.loop);
|
|
var slowLoopTimer = maketimer(1, ITAF, ITAF.slowLoop);
|