diff --git a/Models/FlightDeck/a320.flightdeck.xml b/Models/FlightDeck/a320.flightdeck.xml index db494f12..74a8dcb2 100644 --- a/Models/FlightDeck/a320.flightdeck.xml +++ b/Models/FlightDeck/a320.flightdeck.xml @@ -4323,7 +4323,7 @@ xy-plane number-value %3.0f - it-autoflight/input/spd-kts + it-autoflight/input/kts false led.txf true @@ -4349,7 +4349,7 @@ xy-plane number-value %0.3f - it-autoflight/input/spd-mach + it-autoflight/input/mach false led.txf true diff --git a/Models/Instruments/MCDU/MCDU.nas b/Models/Instruments/MCDU/MCDU.nas index c479e57a..01204d89 100644 --- a/Models/Instruments/MCDU/MCDU.nas +++ b/Models/Instruments/MCDU/MCDU.nas @@ -2531,9 +2531,9 @@ var canvas_MCDU_base = { } else { me["Simple_L1"].setText("SELECTED"); if (getprop("/it-autoflight/input/kts-mach")) { - me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/spd-mach"))); + me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/mach"))); } else { - me["Simple_L4"].setText(sprintf(" %s", int(getprop("/it-autoflight/input/spd-kts")))); + me["Simple_L4"].setText(sprintf(" %s", int(getprop("/it-autoflight/input/kts")))); } me.fontLeft(0, 0, 0, default, 0, 0); } @@ -2685,9 +2685,9 @@ var canvas_MCDU_base = { } else { me["Simple_L1"].setText("SELECTED"); if (getprop("/it-autoflight/input/kts-mach")) { - me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/spd-mach"))); + me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/mach"))); } else { - me["Simple_L4"].setText(sprintf(" %s", int(getprop("/it-autoflight/input/spd-kts")))); + me["Simple_L4"].setText(sprintf(" %s", int(getprop("/it-autoflight/input/kts")))); } me.fontLeft(0, 0, 0, default, 0, 0); } @@ -2846,9 +2846,9 @@ var canvas_MCDU_base = { } else { me["Simple_L1"].setText("SELECTED"); if (getprop("/it-autoflight/input/kts-mach")) { - me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/spd-mach"))); + me["Simple_L4"].setText(sprintf(" %3.3f", getprop("/it-autoflight/input/mach"))); } else { - me["Simple_L4"].setText(sprintf(" %3.0f", getprop("/it-autoflight/input/spd-kts"))); + me["Simple_L4"].setText(sprintf(" %3.0f", getprop("/it-autoflight/input/kts"))); } me.fontLeft(0, 0, 0, default, 0, 0); } diff --git a/Models/Instruments/PFD/PFD.nas b/Models/Instruments/PFD/PFD.nas index be5385fc..dcb90350 100644 --- a/Models/Instruments/PFD/PFD.nas +++ b/Models/Instruments/PFD/PFD.nas @@ -82,8 +82,8 @@ var FMGC_max_spd = props.globals.getNode("/FMGC/internal/maxspeed", 1); var ind_spd_kt = props.globals.getNode("/instrumentation/airspeed-indicator/indicated-speed-kt", 1); var ind_spd_mach = props.globals.getNode("/instrumentation/airspeed-indicator/indicated-mach", 1); var at_mach_mode = props.globals.getNode("/it-autoflight/input/kts-mach", 1); -var at_input_spd_mach = props.globals.getNode("/it-autoflight/input/spd-mach", 1); -var at_input_spd_kts = props.globals.getNode("/it-autoflight/input/spd-kts", 1); +var at_input_spd_mach = props.globals.getNode("/it-autoflight/input/mach", 1); +var at_input_spd_kts = props.globals.getNode("/it-autoflight/input/kts", 1); var fd_roll = props.globals.getNode("/it-autoflight/fd/roll-bar", 1); var fd_pitch = props.globals.getNode("/it-autoflight/fd/pitch-bar", 1); var decision = props.globals.getNode("/instrumentation/mk-viii/inputs/arinc429/decision-height", 1); diff --git a/Nasal/FMGC/FCU.nas b/Nasal/FMGC/FCU.nas index 618893bc..eccfaf09 100644 --- a/Nasal/FMGC/FCU.nas +++ b/Nasal/FMGC/FCU.nas @@ -2,37 +2,37 @@ # Copyright (c) 2020 Josh Davidson (Octal450), Jonathan Redpath (legoboyvdlp) # Nodes -var fd1 = props.globals.getNode("it-autoflight/output/fd1", 1); -var fd2 = props.globals.getNode("it-autoflight/output/fd2", 1); -var ap1 = props.globals.getNode("it-autoflight/output/ap1", 1); -var ap2 = props.globals.getNode("it-autoflight/output/ap2", 1); -var athr = props.globals.getNode("it-autoflight/output/athr", 1); -var fd1Input = props.globals.getNode("it-autoflight/input/fd1", 1); -var fd2Input = props.globals.getNode("it-autoflight/input/fd2", 1); -var ap1Input = props.globals.getNode("it-autoflight/input/ap1", 1); -var ap2Input = props.globals.getNode("it-autoflight/input/ap2", 1); -var athrInput = props.globals.getNode("it-autoflight/input/athr", 1); -var ktsMach = props.globals.getNode("it-autoflight/input/kts-mach", 1); -var iasSet = props.globals.getNode("it-autoflight/input/spd-kts", 1); -var machSet = props.globals.getNode("it-autoflight/input/spd-mach", 1); -var hdgSet = props.globals.getNode("it-autoflight/input/hdg", 1); -var altSet = props.globals.getNode("it-autoflight/input/alt", 1); -var altSetMode = props.globals.getNode("it-autoflight/config/altitude-dial-mode", 1); -var vsSet = props.globals.getNode("it-autoflight/input/vs", 1); -var fpaSet = props.globals.getNode("it-autoflight/input/fpa", 1); -var iasNow = props.globals.getNode("instrumentation/airspeed-indicator/indicated-speed-kt", 1); -var machNow = props.globals.getNode("instrumentation/airspeed-indicator/indicated-mach", 1); -var spdManaged = props.globals.getNode("it-autoflight/input/spd-managed", 1); -var showHDG = props.globals.getNode("it-autoflight/custom/show-hdg", 1); -var trkFpaSW = props.globals.getNode("it-autoflight/custom/trk-fpa", 1); -var latMode = props.globals.getNode("it-autoflight/output/lat", 1); -var vertMode = props.globals.getNode("it-autoflight/output/vert", 1); -var fpaModeInput = props.globals.getNode("it-autoflight/input/fpa", 1); -var latModeInput = props.globals.getNode("it-autoflight/input/lat", 1); -var vertModeInput = props.globals.getNode("it-autoflight/input/vert", 1); -var vsModeInput = props.globals.getNode("it-autoflight/input/vs", 1); -var locArm = props.globals.getNode("it-autoflight/output/loc-armed", 1); -var apprArm = props.globals.getNode("it-autoflight/output/appr-armed", 1); +var fd1 = props.globals.getNode("/it-autoflight/output/fd1", 1); +var fd2 = props.globals.getNode("/it-autoflight/output/fd2", 1); +var ap1 = props.globals.getNode("/it-autoflight/output/ap1", 1); +var ap2 = props.globals.getNode("/it-autoflight/output/ap2", 1); +var athr = props.globals.getNode("/it-autoflight/output/athr", 1); +var fd1Input = props.globals.getNode("/it-autoflight/input/fd1", 1); +var fd2Input = props.globals.getNode("/it-autoflight/input/fd2", 1); +var ap1Input = props.globals.getNode("/it-autoflight/input/ap1", 1); +var ap2Input = props.globals.getNode("/it-autoflight/input/ap2", 1); +var athrInput = props.globals.getNode("/it-autoflight/input/athr", 1); +var ktsMach = props.globals.getNode("/it-autoflight/input/kts-mach", 1); +var iasSet = props.globals.getNode("/it-autoflight/input/kts", 1); +var machSet = props.globals.getNode("/it-autoflight/input/mach", 1); +var hdgSet = props.globals.getNode("/it-autoflight/input/hdg", 1); +var altSet = props.globals.getNode("/it-autoflight/input/alt", 1); +var altSetMode = props.globals.getNode("/it-autoflight/config/altitude-dial-mode", 1); +var vsSet = props.globals.getNode("/it-autoflight/input/vs", 1); +var fpaSet = props.globals.getNode("/it-autoflight/input/fpa", 1); +var iasNow = props.globals.getNode("/instrumentation/airspeed-indicator/indicated-speed-kt", 1); +var machNow = props.globals.getNode("/instrumentation/airspeed-indicator/indicated-mach", 1); +var spdManaged = props.globals.getNode("/it-autoflight/input/spd-managed", 1); +var showHDG = props.globals.getNode("/it-autoflight/custom/show-hdg", 1); +var trkFpaSW = props.globals.getNode("/it-autoflight/custom/trk-fpa", 1); +var latMode = props.globals.getNode("/it-autoflight/output/lat", 1); +var vertMode = props.globals.getNode("/it-autoflight/output/vert", 1); +var fpaModeInput = props.globals.getNode("/it-autoflight/input/fpa", 1); +var latModeInput = props.globals.getNode("/it-autoflight/input/lat", 1); +var vertModeInput = props.globals.getNode("/it-autoflight/input/vert", 1); +var vsModeInput = props.globals.getNode("/it-autoflight/input/vs", 1); +var locArm = props.globals.getNode("/it-autoflight/output/loc-armed", 1); +var apprArm = props.globals.getNode("/it-autoflight/output/appr-armed", 1); var FCUworkingNode = props.globals.initNode("/FMGC/FCU-working", 0, "BOOL"); var FCU = { diff --git a/Nasal/FMGC/FMGC-b.nas b/Nasal/FMGC/FMGC-b.nas index 8b4023af..e172dcfd 100644 --- a/Nasal/FMGC/FMGC-b.nas +++ b/Nasal/FMGC/FMGC-b.nas @@ -14,8 +14,8 @@ var FPLN = { active: props.globals.getNode("/FMGC/flightplan[2]/active", 1), activeTemp: 0, currentCourse: 0, - currentWP: props.globals.getNode("/FMGC/flightplan[2]/current-wp", 1), - currentWPTemp: 0, + currentWp: props.globals.getNode("/FMGC/flightplan[2]/current-wp", 1), + currentWpTemp: 0, deltaAngle: 0, deltaAngleRad: 0, distCoeff: 0, @@ -90,11 +90,11 @@ var Input = { fpaAbs: props.globals.initNode("/it-autoflight/input/fpa-abs", 0, "DOUBLE"), # Set by property rule hdg: props.globals.initNode("/it-autoflight/input/hdg", 0, "INT"), hdgCalc: 0, - ias: props.globals.initNode("/it-autoflight/input/spd-kts", 250, "INT"), + kts: props.globals.initNode("/it-autoflight/input/kts", 100, "INT"), ktsMach: props.globals.initNode("/it-autoflight/input/kts-mach", 0, "BOOL"), lat: props.globals.initNode("/it-autoflight/input/lat", 5, "INT"), latTemp: 5, - mach: props.globals.initNode("/it-autoflight/input/spd-mach", 0.5, "DOUBLE"), + mach: props.globals.initNode("/it-autoflight/input/mach", 0.5, "DOUBLE"), toga: props.globals.initNode("/it-autoflight/input/toga", 0, "BOOL"), trk: props.globals.initNode("/it-autoflight/input/trk", 0, "BOOL"), trueCourse: props.globals.initNode("/it-autoflight/input/true-course", 0, "BOOL"), @@ -112,7 +112,7 @@ var Internal = { altPredicted: props.globals.initNode("/it-autoflight/internal/altitude-predicted", 0, "DOUBLE"), bankLimit: props.globals.initNode("/it-autoflight/internal/bank-limit", 30, "INT"), bankLimitAuto: 30, - captVS: 0, + captVs: 0, driftAngle: props.globals.initNode("/it-autoflight/internal/drift-angle-deg", 0, "DOUBLE"), flchActive: 0, fpa: props.globals.initNode("/it-autoflight/internal/fpa", 0, "DOUBLE"), @@ -120,8 +120,8 @@ var Internal = { hdgErrorDeg: props.globals.initNode("/it-autoflight/internal/heading-error-deg", 0, "DOUBLE"), hdgPredicted: props.globals.initNode("/it-autoflight/internal/heading-predicted", 0, "DOUBLE"), lnavAdvanceNm: props.globals.initNode("/it-autoflight/internal/lnav-advance-nm", 0, "DOUBLE"), - minVS: props.globals.initNode("/it-autoflight/internal/min-vs", -500, "INT"), - maxVS: props.globals.initNode("/it-autoflight/internal/max-vs", 500, "INT"), + minVs: props.globals.initNode("/it-autoflight/internal/min-vs", -500, "INT"), + maxVs: props.globals.initNode("/it-autoflight/internal/max-vs", 500, "INT"), trk: props.globals.initNode("/it-autoflight/internal/track-deg", 0, "DOUBLE"), vs: props.globals.initNode("/it-autoflight/internal/vert-speed-fpm", 0, "DOUBLE"), vsTemp: 0, @@ -220,13 +220,13 @@ var ITAF = { Output.thrMode.setValue(0); Output.lat.setValue(9); Output.vert.setValue(9); - Internal.minVS.setValue(-500); - Internal.maxVS.setValue(500); + Internal.minVs.setValue(-500); + Internal.maxVs.setValue(500); Internal.bankLimit.setValue(30); Internal.bankLimitAuto = 30; Internal.alt.setValue(10000); Internal.altCaptureActive = 0; - Input.ias.setValue(100); + Input.kts.setValue(100); Input.mach.setValue(0.5); Text.thr.setValue("THRUST"); Text.arm.setValue(" "); @@ -309,9 +309,9 @@ var ITAF = { Internal.altDiff = Internal.altTemp - Position.indicatedAltitudeFtTemp; if (Output.vertTemp != 0 and Output.vertTemp != 2 and Output.vertTemp != 6 and Output.vertTemp != 9) { - Internal.captVS = math.clamp(math.round(abs(Internal.vs.getValue()) / 5, 100), 50, 2500); # Capture limits + Internal.captVs = math.clamp(math.round(abs(Internal.vs.getValue()) / 5, 100), 50, 2500); # Capture limits Custom.apFdOn = Output.ap1Temp or Output.ap2Temp or Output.fd1.getBoolValue() or Output.fd2.getBoolValue(); - if (abs(Internal.altDiff) <= Internal.captVS and !Gear.wow1Temp and !Gear.wow2Temp and Custom.apFdOn) { + if (abs(Internal.altDiff) <= Internal.captVs and !Gear.wow1Temp and !Gear.wow2Temp and Custom.apFdOn) { if (Internal.altTemp >= Position.indicatedAltitudeFtTemp and Internal.vsTemp >= -25) { # Don't capture if we are going the wrong way me.setVertMode(3); } else if (Internal.altTemp < Position.indicatedAltitudeFtTemp and Internal.vsTemp <= 25) { # Don't capture if we are going the wrong way @@ -380,7 +380,7 @@ var ITAF = { Input.bankLimitSWTemp = Input.bankLimitSW.getValue(); Velocities.trueAirspeedKtTemp = Velocities.trueAirspeedKt.getValue(); FPLN.activeTemp = FPLN.active.getValue(); - FPLN.currentWPTemp = FPLN.currentWP.getValue(); + FPLN.currentWpTemp = FPLN.currentWp.getValue(); # Bank Limit if (Velocities.trueAirspeedKtTemp >= 420) { @@ -402,14 +402,14 @@ var ITAF = { # Waypoint Advance Logic if (flightPlanController.num[2].getValue() > 0 and FPLN.activeTemp == 1) { - if ((FPLN.currentWPTemp + 1) < flightPlanController.num[2].getValue()) { + if ((FPLN.currentWpTemp + 1) < flightPlanController.num[2].getValue()) { Velocities.groundspeedMps = Velocities.groundspeedKt.getValue() * 0.5144444444444; - FPLN.wpFlyFrom = FPLN.currentWPTemp; + FPLN.wpFlyFrom = FPLN.currentWpTemp; if (FPLN.wpFlyFrom < 0) { FPLN.wpFlyFrom = 0; } FPLN.currentCourse = fmgc.wpCourse[2][FPLN.wpFlyFrom].getValue(); - FPLN.wpFlyTo = FPLN.currentWPTemp + 1; + FPLN.wpFlyTo = FPLN.currentWpTemp + 1; FPLN.nextCourse = fmgc.wpCourse[2][FPLN.wpFlyTo].getValue(); FPLN.maxBankLimit = Internal.bankLimit.getValue(); @@ -436,7 +436,7 @@ var ITAF = { flightPlanController.autoSequencing(); } - #if (FPLN.wp0Dist.getValue() <= FPLN.turnDist and !Gear.wow1.getBoolValue() and fmgc.flightPlanController.flightplans[2].getWP(FPLN.currentWPTemp).fly_type == "flyBy") { + #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(); @@ -569,7 +569,7 @@ var ITAF = { Output.lnavArm.setBoolValue(0); Output.locArm.setBoolValue(0); Output.apprArm.setBoolValue(0); - me.syncHDG(); + me.syncHdg(); Output.lat.setValue(0); Custom.showHdg.setBoolValue(1); Text.lat.setValue("HDG"); @@ -614,7 +614,7 @@ var ITAF = { me.armTextCheck(); } } else if (n == 3) { - me.syncHDG(); + me.syncHdg(); Output.lnavArm.setBoolValue(0); Custom.showHdg.setBoolValue(1); me.armTextCheck(); @@ -629,7 +629,7 @@ var ITAF = { Output.vert.setValue(0); me.resetClimbRateLim(); Text.vert.setValue("ALT HLD"); - me.syncALT(); + me.syncAlt(); me.armTextCheck(); } else if (n == 1) { # V/S if (abs(Input.altDiff) >= 25) { @@ -638,7 +638,7 @@ var ITAF = { Output.apprArm.setBoolValue(0); Output.vert.setValue(1); Text.vert.setValue("V/S"); - me.syncVS(); + me.syncVs(); me.armTextCheck(); } else { Output.apprArm.setBoolValue(0); @@ -682,7 +682,7 @@ var ITAF = { Output.apprArm.setBoolValue(0); Output.vert.setValue(5); Text.vert.setValue("FPA"); - me.syncFPA(); + me.syncFpa(); me.armTextCheck(); } else { Output.apprArm.setBoolValue(0); @@ -807,16 +807,16 @@ var ITAF = { 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); + Internal.maxVs.setValue(math.round(Internal.vsTemp)); + Internal.minVs.setValue(-500); } else { - Internal.maxVS.setValue(500); - Internal.minVS.setValue(math.round(Internal.vsTemp)); + Internal.maxVs.setValue(500); + Internal.minVs.setValue(math.round(Internal.vsTemp)); } }, resetClimbRateLim: func() { - Internal.minVS.setValue(-500); - Internal.maxVS.setValue(500); + Internal.minVs.setValue(-500); + Internal.maxVs.setValue(500); }, takeoffGoAround: func() { Output.vertTemp = Output.vert.getValue(); @@ -825,7 +825,7 @@ var ITAF = { me.setVertMode(7); # Must be before kicking AP off Text.vert.setValue("G/A CLB"); Input.ktsMach.setBoolValue(0); - me.syncIASGA(); + me.syncKtsGa(); if (Gear.wow1.getBoolValue() or Gear.wow2.getBoolValue()) { me.ap1Master(0); me.ap2Master(0); @@ -850,26 +850,26 @@ var ITAF = { Text.arm.setValue(" "); } }, - syncIAS: func() { - Input.ias.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), 100, 350)); + syncKts: func() { + Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), 100, 350)); }, - syncIASGA: func() { # Same as syncIAS, except doesn't go below V2 - Input.ias.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), Custom.FMGC.v2Speed.getValue(), 350)); + syncKtsGa: func() { # Same as syncKts, except doesn't go below V2 + Input.kts.setValue(math.clamp(math.round(Velocities.indicatedAirspeedKt.getValue()), Custom.FMGC.v2Speed.getValue(), 350)); }, syncMach: func() { Input.mach.setValue(math.clamp(math.round(Velocities.indicatedMach.getValue(), 0.001), 0.5, 0.82)); }, - syncHDG: func() { + syncHdg: func() { Input.hdg.setValue(math.round(Internal.hdgPredicted.getValue())); # Switches to track automatically }, - syncALT: func() { + 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)); }, - syncVS: func() { + syncVs: func() { Input.vs.setValue(math.clamp(math.round(Internal.vs.getValue(), 100), -6000, 6000)); }, - syncFPA: func() { + syncFpa: func() { Input.fpa.setValue(math.clamp(math.round(Internal.fpa.getValue(), 0.1), -9.9, 9.9)); }, # Custom Stuff Below @@ -986,7 +986,7 @@ setlistener("/it-autoflight/input/kts-mach", func { if (Input.ktsMach.getBoolValue()) { ITAF.syncMach(); } else { - ITAF.syncIAS(); + ITAF.syncKts(); } }, 0, 0); diff --git a/Nasal/FMGC/FMGC.nas b/Nasal/FMGC/FMGC.nas index fc2f8bf1..03333d76 100644 --- a/Nasal/FMGC/FMGC.nas +++ b/Nasal/FMGC/FMGC.nas @@ -714,7 +714,7 @@ var reset_FMGC = func { setprop("/FMGC/status/phase", 0); fd1 = getprop("/it-autoflight/input/fd1"); fd2 = getprop("/it-autoflight/input/fd2"); - spd = getprop("/it-autoflight/input/spd-kts"); + spd = getprop("/it-autoflight/input/kts"); hdg = getprop("/it-autoflight/input/hdg"); alt = getprop("/it-autoflight/input/alt"); ITAF.init(); @@ -726,7 +726,7 @@ var reset_FMGC = func { mcdu.MCDU_reset(1); setprop("it-autoflight/input/fd1", fd1); setprop("it-autoflight/input/fd2", fd2); - setprop("it-autoflight/input/spd-kts", spd); + setprop("it-autoflight/input/kts", spd); setprop("it-autoflight/input/hdg", hdg); setprop("it-autoflight/input/alt", alt); setprop("systems/pressurization/mode", "GN"); @@ -868,8 +868,8 @@ var ManagedSPD = maketimer(0.25, func { mngktsmach = getprop("/FMGC/internal/mng-kts-mach"); mng_spd = getprop("/FMGC/internal/mng-spd"); mng_spd_cmd = getprop("/FMGC/internal/mng-spd-cmd"); - kts_sel = getprop("/it-autoflight/input/spd-kts"); - mach_sel = getprop("/it-autoflight/input/spd-mach"); + kts_sel = getprop("/it-autoflight/input/kts"); + mach_sel = getprop("/it-autoflight/input/mach"); srsSPD = getprop("/it-autoflight/settings/togaspd"); phase = getprop("/FMGC/status/phase"); # 0 is Preflight 1 is Takeoff 2 is Climb 3 is Cruise 4 is Descent 5 is Decel/Approach 6 is Go Around 7 is Done flap = getprop("/controls/flight/flaps-pos"); @@ -973,9 +973,9 @@ var ManagedSPD = maketimer(0.25, func { mng_spd = getprop("/FMGC/internal/mng-spd"); if (kts_sel != mng_spd and !ktsmach) { - setprop("it-autoflight/input/spd-kts", mng_spd); + setprop("it-autoflight/input/kts", mng_spd); } else if (mach_sel != mng_spd and ktsmach) { - setprop("it-autoflight/input/spd-mach", mng_spd); + setprop("it-autoflight/input/mach", mng_spd); } } else { ManagedSPD.stop(); diff --git a/Systems/fmgc-drivers.xml b/Systems/fmgc-drivers.xml index 93f49320..e8836c46 100644 --- a/Systems/fmgc-drivers.xml +++ b/Systems/fmgc-drivers.xml @@ -100,7 +100,7 @@ 0 - /it-autoflight/input/spd-kts + /it-autoflight/input/kts @@ -115,7 +115,7 @@ /instrumentation/airspeed-indicator/indicated-speed-kt /instrumentation/airspeed-indicator/indicated-mach - /it-autoflight/input/spd-mach + /it-autoflight/input/mach @@ -142,7 +142,7 @@ - /it-autoflight/input/spd-kts + /it-autoflight/input/kts /it-autoflight/internal/flch-kts @@ -198,7 +198,7 @@ noise-spike true output - /it-autoflight/input/spd-mach + /it-autoflight/input/mach /it-autoflight/internal/flch-mach @@ -270,7 +270,7 @@ - /it-autoflight/input/spd-kts + /it-autoflight/input/kts @@ -301,7 +301,7 @@ - /it-autoflight/input/spd-mach + /it-autoflight/input/mach diff --git a/Systems/fmgc-thrust.xml b/Systems/fmgc-thrust.xml index cc4e6484..6d7018fc 100644 --- a/Systems/fmgc-thrust.xml +++ b/Systems/fmgc-thrust.xml @@ -11,7 +11,7 @@ noise-spike true output - /it-autoflight/input/spd-kts + /it-autoflight/input/kts /it-autoflight/internal/athr-kts @@ -69,7 +69,7 @@ noise-spike true output - /it-autoflight/input/spd-mach + /it-autoflight/input/mach /it-autoflight/internal/athr-mach diff --git a/gui/dialogs/a3xx-autoflight-dlg.xml b/gui/dialogs/a3xx-autoflight-dlg.xml index fa5cc801..c9002aa0 100644 --- a/gui/dialogs/a3xx-autoflight-dlg.xml +++ b/gui/dialogs/a3xx-autoflight-dlg.xml @@ -403,7 +403,7 @@ 0 3 50 - /it-autoflight/input/spd-kts + /it-autoflight/input/kts true @@ -529,7 +529,7 @@ 0 3 50 - /it-autoflight/input/spd-mach + /it-autoflight/input/mach true