rework fix
This commit is contained in:
parent
69a4678e16
commit
d18b121223
3 changed files with 168 additions and 90 deletions
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@ -84,6 +84,7 @@ var FMGCinit = func {
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FMGCInternal.minspeed = 0;
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FMGCInternal.minspeed = 0;
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FMGCInternal.maxspeed = 338;
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FMGCInternal.maxspeed = 338;
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FMGCInternal.phase = 0; # 0 is Preflight 1 is Takeoff 2 is Climb 3 is Cruise 4 is Descent 5 is Decel/Approach 6 is Go Around 7 is Done
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FMGCInternal.phase = 0; # 0 is Preflight 1 is Takeoff 2 is Climb 3 is Cruise 4 is Descent 5 is Decel/Approach 6 is Go Around 7 is Done
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FMGCNodes.phase.setValue(0);
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FMGCInternal.mngSpd = 157;
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FMGCInternal.mngSpd = 157;
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FMGCInternal.mngSpdCmd = 157;
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FMGCInternal.mngSpdCmd = 157;
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FMGCInternal.mngKtsMach = 0;
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FMGCInternal.mngKtsMach = 0;
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@ -257,6 +258,7 @@ var FMGCNodes = {
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toState: props.globals.initNode("/FMGC/internal/to-state", 0, "BOOL"),
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toState: props.globals.initNode("/FMGC/internal/to-state", 0, "BOOL"),
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v1: props.globals.initNode("/FMGC/internal/v1", 0, "DOUBLE"),
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v1: props.globals.initNode("/FMGC/internal/v1", 0, "DOUBLE"),
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v1set: props.globals.initNode("/FMGC/internal/v1-set", 0, "BOOL"),
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v1set: props.globals.initNode("/FMGC/internal/v1-set", 0, "BOOL"),
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phase: props.globals.initNode("/FMGC/internal/phase", 0, "INT"),
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};
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};
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############
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############
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@ -601,92 +603,15 @@ var radios = maketimer(1, func() {
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adf1();
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adf1();
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});
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});
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var masterFMGC = maketimer(0.2, func {
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var fuelUpdateFMGC = maketimer(0.5, func {
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n1_left = pts.Engines.Engine.n1Actual[0].getValue();
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n1_right = pts.Engines.Engine.n1Actual[1].getValue();
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modelat = Modes.PFD.FMA.rollMode.getValue();
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mode = Modes.PFD.FMA.pitchMode.getValue();
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gs = pts.Velocities.groundspeed.getValue();
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alt = pts.Instrumentation.Altimeter.indicatedFt.getValue();
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# cruiseft = FMGCInternal.crzFt;
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# cruiseft_b = FMGCInternal.crzFt - 200;
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state1 = pts.Systems.Thrust.state[0].getValue();
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state2 = pts.Systems.Thrust.state[1].getValue();
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accel_agl_ft = Setting.reducAglFt.getValue();
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gear0 = pts.Gear.wow[0].getBoolValue();
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altSel = Input.alt.getValue();
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if ((n1_left < 85 or n1_right < 85) and gs < 90 and mode == " " and gear0 and FMGCInternal.phase == 1) { # rejected takeoff
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FMGCInternal.phase = 0;
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systems.PNEU.pressMode.setValue("GN");
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}
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if (gear0 and FMGCInternal.phase == 0 and ((n1_left >= 85 and n1_right >= 85 and mode == "SRS") or gs >= 90)) {
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FMGCInternal.phase = 1;
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systems.PNEU.pressMode.setValue("TO");
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}
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if (FMGCInternal.phase == 1 and ((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
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FMGCInternal.phase = 2;
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systems.PNEU.pressMode.setValue("TO");
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}
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if (FMGCInternal.phase == 2 and (mode == "ALT CRZ" or mode == "ALT CRZ*")) {
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FMGCInternal.phase = 3;
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systems.PNEU.pressMode.setValue("CR");
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}
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if (FMGCInternal.crzFl >= 200) {
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if (FMGCInternal.phase == 3 and (flightPlanController.arrivalDist <= 200 or altSel < 20000)) {
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FMGCInternal.phase = 4;
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systems.PNEU.pressMode.setValue("DE");
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}
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} else {
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if (FMGCInternal.phase == 3 and (flightPlanController.arrivalDist <= 200 or altSel < (FMGCInternal.crzFl * 100))) { # todo - not sure about crzFl condition, investigate what happens!
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FMGCInternal.phase = 4;
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systems.PNEU.pressMode.setValue("DE");
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}
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}
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if (FMGCInternal.phase == 4) {
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if (getprop("/FMGC/internal/decel")) {
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FMGCInternal.phase = 5;
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}
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else if (altSel == (FMGCInternal.crzFl * 100)) { # back to CRZ state
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FMGCInternal.phase = 3;
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systems.PNEU.pressMode.setValue("CR");
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}
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}
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if (flightPlanController.num[2].getValue() > 0 and getprop("/FMGC/flightplan[2]/active") == 1 and flightPlanController.arrivalDist <= 15 and (modelat == "NAV" or modelat == "LOC" or modelat == "LOC*") and pts.Position.gearAglFt.getValue() < 9500) { #todo decel pseudo waypoint
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setprop("/FMGC/internal/decel", 1);
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} else if (getprop("/FMGC/internal/decel") == 1 and (FMGCInternal.phase == 0 or FMGCInternal.phase == 6)) {
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setprop("/FMGC/internal/decel", 0);
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}
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if ((FMGCInternal.phase == 5) and state1 == "TOGA" and state2 == "TOGA") {
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FMGCInternal.phase = 6;
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systems.PNEU.pressMode.setValue("TO");
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Input.toga.setValue(1);
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}
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if (FMGCInternal.phase == 6 and alt >= accel_agl_ft) { # todo when insert altn or new dest
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FMGCInternal.phase = 2;
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}
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if (getprop("/systems/navigation/adr/computation/overspeed-vfe-spd") != 1024) {
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FMGCInternal.maxspeed = getprop("/systems/navigation/adr/computation/overspeed-vfe-spd") - 4;
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} elsif (pts.Gear.position[0].getValue() != 0 or pts.Gear.position[1].getValue() != 0 or pts.Gear.position[2].getValue() != 0) {
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FMGCInternal.maxspeed = 284;
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} else {
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FMGCInternal.maxspeed = fmgc.FMGCInternal.vmo_mmo;
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}
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############################
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############################
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# fuel
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# fuel
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############################
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############################
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updateFuel();
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updateFuel();
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});
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var windUpdateFMGC = maketimer(1, func {
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############################
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############################
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# wind
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# wind
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############################
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############################
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@ -730,6 +655,142 @@ var masterFMGC = maketimer(0.2, func {
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fmgc.windController.write();
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fmgc.windController.write();
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}
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}
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}
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}
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});
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var prop_n1_left = pts.Engines.Engine.n1Actual[0];
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var prop_n1_right = pts.Engines.Engine.n1Actual[1];
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#var prop_nmodelat = Modes.PFD.FMA.rollMode;
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#var prop_mode = Modes.PFD.FMA.pitchMode;
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var prop_gs = pts.Velocities.groundspeed;
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var prop_alt = pts.Instrumentation.Altimeter.indicatedFt;
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var prop_state1 = pts.Systems.Thrust.state[0];
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var prop_state2 = pts.Systems.Thrust.state[1];
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#var prop_accel_agl_ft = Setting.reducAglFt;
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var prop_gear0 = pts.Gear.wow[0];
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#var prop_altSel = Input.alt;
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var masterFMGC = maketimer(0.2, func {
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n1_left = prop_n1_left.getValue();
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n1_right = prop_n1_right.getValue();
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modelat = Modes.PFD.FMA.rollMode.getValue();
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mode = Modes.PFD.FMA.pitchMode.getValue();
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gs = prop_gs.getValue();
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alt = prop_alt.getValue();
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# cruiseft = FMGCInternal.crzFt;
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# cruiseft_b = FMGCInternal.crzFt - 200;
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state1 = prop_state1.getValue();
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state2 = prop_state2.getValue();
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accel_agl_ft = Setting.reducAglFt.getValue();
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gear0 = prop_gear0.getBoolValue();
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altSel = Input.alt.getValue();
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var phase = FMGCInternal.phase;
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var newphase = phase;
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if (phase == 0) {
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if (gear0 and ((n1_left >= 85 and n1_right >= 85 and mode == "SRS") or gs >= 90)) {
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newphase = 1;
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systems.PNEU.pressMode.setValue("TO");
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}
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}
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else if (phase == 1) {
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if (gear0) {
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if ((n1_left < 85 or n1_right < 85) and gs < 90 and mode == " ") { # rejected takeoff
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newphase = 0;
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systems.PNEU.pressMode.setValue("GN");
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}
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}
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else if (((mode != "SRS" and mode != " ") or alt >= accel_agl_ft)) {
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newphase = 2;
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systems.PNEU.pressMode.setValue("TO");
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}
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}
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else if (phase == 2) {
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if ((mode == "ALT CRZ" or mode == "ALT CRZ*")) {
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newphase = 3;
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systems.PNEU.pressMode.setValue("CR");
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}
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}
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else if (phase == 3) {
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if (FMGCInternal.crzFl >= 200) {
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if ((flightPlanController.arrivalDist <= 200 or altSel < 20000)) {
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newphase = 4;
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systems.PNEU.pressMode.setValue("DE");
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}
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} else {
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if ((flightPlanController.arrivalDist <= 200 or altSel < (FMGCInternal.crzFl * 100))) { # todo - not sure about crzFl condition, investigate what happens!
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newphase = 4;
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systems.PNEU.pressMode.setValue("DE");
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}
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}
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}
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else if (phase == 4) {
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if (getprop("/FMGC/internal/decel")) {
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newphase = 5;
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}
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else if (altSel == (FMGCInternal.crzFl * 100)) { # back to CRZ state
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newphase = 3;
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systems.PNEU.pressMode.setValue("CR");
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}
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}
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else if (phase == 5) {
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if (state1 == "TOGA" and state2 == "TOGA") {
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newphase = 6;
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systems.PNEU.pressMode.setValue("TO");
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Input.toga.setValue(1);
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}
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}
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else if (phase == 6) {
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if (alt >= accel_agl_ft) { # todo when insert altn or new dest
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newphase = 2;
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}
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}
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if (flightPlanController.num[2].getValue() > 0 and getprop("/FMGC/flightplan[2]/active") == 1 and
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flightPlanController.arrivalDist <= 15 and (modelat == "NAV" or modelat == "LOC" or modelat == "LOC*") and pts.Position.gearAglFt.getValue() < 9500) { #todo decel pseudo waypoint
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setprop("/FMGC/internal/decel", 1);
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} else if (getprop("/FMGC/internal/decel") == 1 and (phase == 0 or phase == 6)) {
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setprop("/FMGC/internal/decel", 0);
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}
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if (getprop("/systems/navigation/adr/computation/overspeed-vfe-spd") != 1024) {
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FMGCInternal.maxspeed = getprop("/systems/navigation/adr/computation/overspeed-vfe-spd") - 4;
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} elsif (pts.Gear.position[0].getValue() != 0 or pts.Gear.position[1].getValue() != 0 or pts.Gear.position[2].getValue() != 0) {
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FMGCInternal.maxspeed = 284;
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} else {
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FMGCInternal.maxspeed = fmgc.FMGCInternal.vmo_mmo;
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}
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if (newphase != phase) { # phase changed
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FMGCInternal.phase = newphase;
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FMGCNodes.phase.setValue(newphase);
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}
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############################
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############################
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# calculate speeds
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# calculate speeds
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@ -771,7 +832,7 @@ var masterFMGC = maketimer(0.2, func {
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}
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}
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# predicted takeoff speeds
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# predicted takeoff speeds
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if (FMGCInternal.phase == 1) {
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if (phase == 1) {
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FMGCInternal.clean_to = FMGCInternal.clean;
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FMGCInternal.clean_to = FMGCInternal.clean;
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FMGCInternal.vs1g_clean_to = FMGCInternal.vs1g_clean;
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FMGCInternal.vs1g_clean_to = FMGCInternal.vs1g_clean;
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FMGCInternal.vs1g_conf_2_to = FMGCInternal.vs1g_conf_2;
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FMGCInternal.vs1g_conf_2_to = FMGCInternal.vs1g_conf_2;
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@ -793,7 +854,7 @@ var masterFMGC = maketimer(0.2, func {
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}
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}
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# predicted approach (temp go-around) speeds
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# predicted approach (temp go-around) speeds
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if (FMGCInternal.phase == 5 or FMGCInternal.phase == 6) {
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if (phase == 5 or phase == 6) {
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FMGCInternal.clean_appr = FMGCInternal.clean;
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FMGCInternal.clean_appr = FMGCInternal.clean;
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FMGCInternal.vs1g_clean_appr = FMGCInternal.vs1g_clean;
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FMGCInternal.vs1g_clean_appr = FMGCInternal.vs1g_clean;
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FMGCInternal.vs1g_conf_2_appr = FMGCInternal.vs1g_conf_2;
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FMGCInternal.vs1g_conf_2_appr = FMGCInternal.vs1g_conf_2;
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@ -914,7 +975,8 @@ var masterFMGC = maketimer(0.2, func {
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}
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}
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}
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}
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if (gear0 and pts.Controls.Flight.flapsPos.getValue() < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
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#if (gear0 and pts.Controls.Flight.flapsPos.getValue() < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
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if (gear0 and flap < 5 and (state1 == "MCT" or state1 == "MAN THR" or state1 == "TOGA") and (state2 == "MCT" or state2 == "MAN THR" or state2 == "TOGA")) {
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if (!FMGCInternal.takeoffState) {
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if (!FMGCInternal.takeoffState) {
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fmgc.FMGCNodes.toState.setValue(1);
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fmgc.FMGCNodes.toState.setValue(1);
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}
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}
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#handle radios, runways, v1/vr/v2
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#handle radios, runways, v1/vr/v2
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############################
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############################
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});
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var updateAirportRadios = func {
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var phase = FMGCInternal.phase;
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departure_rwy = fmgc.flightPlanController.flightplans[2].departure_runway;
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departure_rwy = fmgc.flightPlanController.flightplans[2].departure_runway;
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destination_rwy = fmgc.flightPlanController.flightplans[2].destination_runway;
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destination_rwy = fmgc.flightPlanController.flightplans[2].destination_runway;
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if (destination_rwy != nil and FMGCInternal.phase >= 2) {
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if (destination_rwy != nil and phase >= 2) {
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var airport = airportinfo(FMGCInternal.arrApt);
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var airport = airportinfo(FMGCInternal.arrApt);
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setprop("/FMGC/internal/ldg-elev", airport.elevation * M2FT); # eventually should be runway elevation
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setprop("/FMGC/internal/ldg-elev", airport.elevation * M2FT); # eventually should be runway elevation
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magnetic_hdg = geo.normdeg(destination_rwy.heading - getprop("/environment/magnetic-variation-deg"));
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magnetic_hdg = geo.normdeg(destination_rwy.heading - getprop("/environment/magnetic-variation-deg"));
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@ -947,7 +1015,7 @@ var masterFMGC = maketimer(0.2, func {
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} else if (!getprop("/FMGC/internal/ils1crs-set")) {
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} else if (!getprop("/FMGC/internal/ils1crs-set")) {
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setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
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setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
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}
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}
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} else if (departure_rwy != nil and FMGCInternal.phase <= 1) {
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} else if (departure_rwy != nil and phase <= 1) {
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magnetic_hdg = geo.normdeg(departure_rwy.heading - getprop("/environment/magnetic-variation-deg"));
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magnetic_hdg = geo.normdeg(departure_rwy.heading - getprop("/environment/magnetic-variation-deg"));
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runway_ils = departure_rwy.ils_frequency_mhz;
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runway_ils = departure_rwy.ils_frequency_mhz;
|
||||||
if (runway_ils != nil and !getprop("/FMGC/internal/ils1freq-set") and !getprop("/FMGC/internal/ils1crs-set")) {
|
if (runway_ils != nil and !getprop("/FMGC/internal/ils1freq-set") and !getprop("/FMGC/internal/ils1crs-set")) {
|
||||||
|
@ -961,10 +1029,15 @@ var masterFMGC = maketimer(0.2, func {
|
||||||
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
|
setprop("instrumentation/nav[0]/radials/selected-deg", magnetic_hdg);
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
});
|
|
||||||
|
};
|
||||||
|
|
||||||
|
setlistener(FMGCNodes.phase, updateAirportRadios);
|
||||||
|
setlistener(flightPlanController.changed, updateAirportRadios);
|
||||||
|
|
||||||
var reset_FMGC = func {
|
var reset_FMGC = func {
|
||||||
FMGCInternal.phase = 0;
|
FMGCInternal.phase = 0;
|
||||||
|
FMGCNodes.phase.serValue(0);
|
||||||
fd1 = Input.fd1.getValue();
|
fd1 = Input.fd1.getValue();
|
||||||
fd2 = Input.fd2.getValue();
|
fd2 = Input.fd2.getValue();
|
||||||
spd = Input.kts.getValue();
|
spd = Input.kts.getValue();
|
||||||
|
|
|
@ -32,6 +32,8 @@ var flightPlanController = {
|
||||||
|
|
||||||
# These flags are only for the main flgiht-plan
|
# These flags are only for the main flgiht-plan
|
||||||
active: props.globals.initNode("/FMGC/flightplan[2]/active", 0, "BOOL"),
|
active: props.globals.initNode("/FMGC/flightplan[2]/active", 0, "BOOL"),
|
||||||
|
|
||||||
|
changed: props.globals.initNode("/FMGC/flightplan[2]/changed", 0, "BOOL"),
|
||||||
|
|
||||||
currentToWpt: nil, # container for the current TO waypoint ghost
|
currentToWpt: nil, # container for the current TO waypoint ghost
|
||||||
currentToWptIndex: props.globals.initNode("/FMGC/flightplan[2]/current-wp", 0, "INT"),
|
currentToWptIndex: props.globals.initNode("/FMGC/flightplan[2]/current-wp", 0, "INT"),
|
||||||
|
@ -765,6 +767,9 @@ var flightPlanController = {
|
||||||
fmgc.FMGCInternal.fuelCalculating = 1;
|
fmgc.FMGCInternal.fuelCalculating = 1;
|
||||||
fmgc.fuelCalculating.setValue(1);
|
fmgc.fuelCalculating.setValue(1);
|
||||||
}
|
}
|
||||||
|
|
||||||
|
if (n == 2) flightPlanController.changed.setBoolValue(1);
|
||||||
|
|
||||||
canvas_nd.A3XXRouteDriver.triggerSignal("fp-added");
|
canvas_nd.A3XXRouteDriver.triggerSignal("fp-added");
|
||||||
},
|
},
|
||||||
|
|
||||||
|
|
|
@ -250,8 +250,8 @@ setlistener("/instrumentation/mk-viii/inputs/discretes/ta-tcf-inhibit", func{
|
||||||
|
|
||||||
# Replay
|
# Replay
|
||||||
var replayState = props.globals.getNode("/sim/replay/replay-state");
|
var replayState = props.globals.getNode("/sim/replay/replay-state");
|
||||||
setlistener("/sim/replay/replay-state", func() {
|
setlistener(replayState, func(v) {
|
||||||
if (replayState.getBoolValue()) {
|
if (v.getBoolValue()) {
|
||||||
} else {
|
} else {
|
||||||
acconfig.colddark();
|
acconfig.colddark();
|
||||||
gui.popupTip("Replay Ended: Setting Cold and Dark state...");
|
gui.popupTip("Replay Ended: Setting Cold and Dark state...");
|
||||||
|
|
Loading…
Add table
Reference in a new issue