Managed speed: rewrite control loop. Add CLB / DES SPD LIM feature
This commit is contained in:
Jonathan Redpath
parent
efe7d9c977
commit
c202b1e67e
5 changed files with 161 additions and 122 deletions
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@ -5223,6 +5223,12 @@ var canvas_MCDU_base = {
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me.colorRight(myVertRev[i].R1[2],myVertRev[i].R2[2],myVertRev[i].R3[2],myVertRev[i].R4[2],myVertRev[i].R5[2],myVertRev[i].R6[2]);
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}
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if (myVertRev[i] != nil and (myVertRev[i].type == 1 and fmgc.FMGCInternal.desSpdLimSet) or (myVertRev[i].type != 1 and fmgc.FMGCInternal.clbSpdLimSet)) {
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me["Simple_L2"].setFontSize(normal);
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} else {
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me["Simple_L2"].setFontSize(small);
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}
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pageSwitch[i].setBoolValue(1);
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}
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} else if (page == "DEPARTURE") {
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@ -27,8 +27,6 @@ var alt = 0;
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var altitude = 0;
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var flap = 0;
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var flaps = 0;
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var ias = 0;
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var mach = 0;
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var ktsmach = 0;
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var kts_sel = 0;
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var mach_sel = 0;
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@ -82,6 +80,12 @@ var FMGCInternal = {
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phase: 0,
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minspeed: 0,
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maxspeed: 0,
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clbSpdLim: 250,
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desSpdLim: 250,
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clbSpdLimAlt: 10000,
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desSpdLimAlt: 10000,
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clbSpdLimSet: 0,
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desSpdLimSet: 0,
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takeoffState: 0,
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# speeds
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@ -257,9 +261,12 @@ var postInit = func() {
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var FMGCNodes = {
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costIndex: props.globals.initNode("/FMGC/internal/cost-index", 0, "DOUBLE"),
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decel: props.globals.initNode("/FMGC/internal/decel", 0, "BOOL"),
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flexSet: props.globals.initNode("/FMGC/internal/flex-set", 0, "BOOL"),
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flexTemp: props.globals.initNode("/FMGC/internal/flex", 0, "INT"),
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mngSpdAlt: props.globals.getNode("/FMGC/internal/mng-alt-spd"),
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ktsToMachFactor: props.globals.getNode("/FMGC/internal/kts-to-mach-factor"),
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machToKtsFactor: props.globals.getNode("/FMGC/internal/mach-to-kts-factor"),
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mngMachAlt: props.globals.getNode("/FMGC/internal/mng-alt-mach"),
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toFromSet: props.globals.initNode("/FMGC/internal/tofrom-set", 0, "BOOL"),
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toState: props.globals.initNode("/FMGC/internal/to-state", 0, "BOOL"),
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@ -338,11 +345,8 @@ var updateFuel = func {
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final_fuel = 1000 * FMGCInternal.finalFuel;
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zfw = 1000 * FMGCInternal.zfw;
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final_time = final_fuel / (2.0 * ((zfw*zfw*-2e-10) + (zfw*0.0003) + 2.8903)); # x2 for 2 engines
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if (final_time < 0) {
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final_time = 0;
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} elsif (final_time > 480) {
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final_time = 480;
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}
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final_time = math.clamp(final_time, 0, 480);
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if (num(final_time) >= 60) {
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final_min = int(math.mod(final_time, 60));
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final_hour = int((final_time - final_min) / 60);
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@ -360,11 +364,8 @@ var updateFuel = func {
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}
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zfw = 1000 * FMGCInternal.zfw;
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final_fuel = final_time * 2.0 * ((zfw*zfw*-2e-10) + (zfw*0.0003) + 2.8903); # x2 for 2 engines
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if (final_fuel < 0) {
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final_fuel = 0;
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} elsif (final_fuel > 80000) {
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final_fuel = 80000;
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}
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final_fuel = math.clamp(final_fuel, 0, 80000);
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FMGCInternal.finalFuel = final_fuel / 1000;
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}
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@ -376,11 +377,8 @@ var updateFuel = func {
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alt_fuel = 1000 * num(FMGCInternal.altFuel);
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zfw = 1000 * FMGCInternal.zfw;
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alt_time = alt_fuel / (2.0 * ((zfw*zfw*-2e-10) + (zfw*0.0003) + 2.8903)); # x2 for 2 engines
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if (alt_time < 0) {
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alt_time = 0;
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} elsif (alt_time > 480) {
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alt_time = 480;
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}
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alt_time = math.clamp(alt_time, 0, 480);
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if (num(alt_time) >= 60) {
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alt_min = int(math.mod(alt_time, 60));
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alt_hour = int((alt_time - alt_min) / 60);
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@ -417,21 +415,14 @@ var updateFuel = func {
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#trip_fuel = 4.003e+02 + (dist * -5.399e+01) + (dist * dist * -7.322e-02) + (dist * dist * dist * 1.091e-05) + (dist * dist * dist * dist * 2.962e-10) + (dist * dist * dist * dist * dist * -1.178e-13) + (dist * dist * dist * dist * dist * dist * 6.322e-18) + (crz * 5.387e+01) + (dist * crz * 1.583e+00) + (dist * dist * crz * 7.695e-04) + (dist * dist * dist * crz * -1.057e-07) + (dist * dist * dist * dist * crz * 1.138e-12) + (dist * dist * dist * dist * dist * crz * 1.736e-16) + (crz * crz * -1.171e+00) + (dist * crz * crz * -1.219e-02) + (dist * dist * crz * crz * -2.879e-06) + (dist * dist * dist * crz * crz * 3.115e-10) + (dist * dist * dist * dist * crz * crz * -4.093e-15) + (crz * crz * crz * 9.160e-03) + (dist * crz * crz * crz * 4.311e-05) + (dist * dist * crz * crz * crz * 4.532e-09) + (dist * dist * dist * crz * crz * crz * -2.879e-13) + (crz * crz * crz * crz * -3.338e-05) + (dist * crz * crz * crz * crz * -7.340e-08) + (dist * dist * crz * crz * crz * crz * -2.494e-12) + (crz * crz * crz * crz * crz * 5.849e-08) + (dist * crz * crz * crz * crz * crz * 4.898e-11) + (crz * crz * crz * crz * crz * crz * -3.999e-11);
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trip_fuel = 4.018e+02 + (dist*3.575e+01) + (dist*dist*-4.260e-02) + (dist*dist*dist*-1.446e-05) + (dist*dist*dist*dist*4.101e-09) + (dist*dist*dist*dist*dist*-6.753e-13) + (dist*dist*dist*dist*dist*dist*5.074e-17) + (crz*-2.573e+01) + (dist*crz*-1.583e-01) + (dist*dist*crz*8.147e-04) + (dist*dist*dist*crz*4.485e-08) + (dist*dist*dist*dist*crz*-7.656e-12) + (dist*dist*dist*dist*dist*crz*4.503e-16) + (crz*crz*4.427e-01) + (dist*crz*crz*-1.137e-03) + (dist*dist*crz*crz*-4.409e-06) + (dist*dist*dist*crz*crz*-3.345e-11) + (dist*dist*dist*dist*crz*crz*4.985e-15) + (crz*crz*crz*-2.471e-03) + (dist*crz*crz*crz*1.223e-05) + (dist*dist*crz*crz*crz*9.660e-09) + (dist*dist*dist*crz*crz*crz*-2.127e-14) + (crz*crz*crz*crz*5.714e-06) + (dist*crz*crz*crz*crz*-3.546e-08) + (dist*dist*crz*crz*crz*crz*-7.536e-12) + (crz*crz*crz*crz*crz*-4.061e-09) + (dist*crz*crz*crz*crz*crz*3.355e-11) + (crz*crz*crz*crz*crz*crz*-1.451e-12);
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if (trip_fuel < 400) {
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trip_fuel = 400;
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} elsif (trip_fuel > 80000) {
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trip_fuel = 80000;
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}
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trip_fuel = math.clamp(trip_fuel, 400, 80000);
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# cruize temp correction
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trip_fuel = trip_fuel + (0.033 * (temp - 15 + (2 * crz / 10)) * flightPlanController.arrivalDist);
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trip_time = 9.095e-02 + (dist*-3.968e-02) + (dist*dist*4.302e-04) + (dist*dist*dist*2.005e-07) + (dist*dist*dist*dist*-6.876e-11) + (dist*dist*dist*dist*dist*1.432e-14) + (dist*dist*dist*dist*dist*dist*-1.177e-18) + (crz*7.348e-01) + (dist*crz*3.310e-03) + (dist*dist*crz*-8.700e-06) + (dist*dist*dist*crz*-4.214e-10) + (dist*dist*dist*dist*crz*5.652e-14) + (dist*dist*dist*dist*dist*crz*-6.379e-18) + (crz*crz*-1.449e-02) + (dist*crz*crz*-7.508e-06) + (dist*dist*crz*crz*4.529e-08) + (dist*dist*dist*crz*crz*3.699e-13) + (dist*dist*dist*dist*crz*crz*8.466e-18) + (crz*crz*crz*1.108e-04) + (dist*crz*crz*crz*-4.126e-08) + (dist*dist*crz*crz*crz*-9.645e-11) + (dist*dist*dist*crz*crz*crz*-1.544e-16) + (crz*crz*crz*crz*-4.123e-07) + (dist*crz*crz*crz*crz*1.831e-10) + (dist*dist*crz*crz*crz*crz*7.438e-14) + (crz*crz*crz*crz*crz*7.546e-10) + (dist*crz*crz*crz*crz*crz*-1.921e-13) + (crz*crz*crz*crz*crz*crz*-5.453e-13);
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if (trip_time < 10) {
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trip_time = 10;
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} elsif (trip_time > 480) {
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trip_time = 480;
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}
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trip_time = math.clamp(trip_time, 10, 480);
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# if (low air conditioning) {
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# trip_fuel = trip_fuel * 0.995;
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#}
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@ -444,11 +435,7 @@ var updateFuel = func {
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zfw = FMGCInternal.zfw;
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landing_weight_correction = 9.951e+00 + (dist*-2.064e+00) + (dist*dist*2.030e-03) + (dist*dist*dist*8.179e-08) + (dist*dist*dist*dist*-3.941e-11) + (dist*dist*dist*dist*dist*2.443e-15) + (crz*2.771e+00) + (dist*crz*3.067e-02) + (dist*dist*crz*-1.861e-05) + (dist*dist*dist*crz*2.516e-10) + (dist*dist*dist*dist*crz*5.452e-14) + (crz*crz*-4.483e-02) + (dist*crz*crz*-1.645e-04) + (dist*dist*crz*crz*5.212e-08) + (dist*dist*dist*crz*crz*-8.721e-13) + (crz*crz*crz*2.609e-04) + (dist*crz*crz*crz*3.898e-07) + (dist*dist*crz*crz*crz*-4.617e-11) + (crz*crz*crz*crz*-6.488e-07) + (dist*crz*crz*crz*crz*-3.390e-10) + (crz*crz*crz*crz*crz*5.835e-10);
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trip_fuel = trip_fuel + (landing_weight_correction * (FMGCInternal.lw * 1000 - 121254.24421) / 2204.622622);
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if (trip_fuel < 400) {
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trip_fuel = 400;
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} elsif (trip_fuel > 80000) {
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trip_fuel = 80000;
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}
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trip_fuel = math.clamp(trip_fuel, 400, 80000);
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FMGCInternal.tripFuel = trip_fuel / 1000;
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if (num(trip_time) >= 60) {
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@ -502,11 +489,8 @@ var updateFuel = func {
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FMGCInternal.extraFuel = extra_fuel / 1000;
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lw = 1000 * FMGCInternal.lw;
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extra_time = extra_fuel / (2.0 * ((lw*lw*-2e-10) + (lw*0.0003) + 2.8903)); # x2 for 2 engines
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if (extra_time < 0) {
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extra_time = 0;
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} elsif (extra_time > 480) {
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extra_time = 480;
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}
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extra_time = math.clamp(extra_time, 0, 480);
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if (num(extra_time) >= 60) {
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extra_min = int(math.mod(extra_time, 60));
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extra_hour = int((extra_time - extra_min) / 60);
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@ -631,7 +615,7 @@ var masterFMGC = maketimer(0.2, func {
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}
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}
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} elsif (FMGCInternal.phase == 4) {
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if (getprop("/FMGC/internal/decel")) {
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if (FMGCNodes.decel.getValue()) {
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newphase = 5;
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}
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} elsif (FMGCInternal.phase == 5) {
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@ -648,9 +632,9 @@ var masterFMGC = maketimer(0.2, func {
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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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} elsif (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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FMGCNodes.decel.setValue(1);
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} elsif (FMGCNodes.decel.getValue() and (FMGCInternal.phase == 0 or FMGCInternal.phase == 6)) {
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FMGCNodes.decel.setValue(0);
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}
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@ -955,8 +939,8 @@ var updateAirportRadios = func {
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};
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setlistener(FMGCNodes.phase, updateAirportRadios,0,0);
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setlistener(flightPlanController.changed, updateAirportRadios,0,0);
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setlistener(FMGCNodes.phase, updateAirportRadios, 0, 0);
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setlistener(flightPlanController.changed, updateAirportRadios, 0, 0);
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var reset_FMGC = func {
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FMGCInternal.phase = 0;
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@ -1007,110 +991,76 @@ var reset_FMGC = func {
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#################
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# Managed Speed #
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#################
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var srsSpeedNode = props.globals.getNode("/it-autoflight/settings/togaspd", 1);
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var ktToMach = func(val) { return val * FMGCNodes.ktsToMachFactor.getValue(); }
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var machToKt = func(val) { return val * FMGCNodes.machToKtsFactor.getValue(); }
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var ManagedSPD = maketimer(0.25, func {
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if (FMGCInternal.crzSet and FMGCInternal.costIndexSet) {
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if (Custom.Input.spdManaged.getBoolValue()) {
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altitude = pts.Instrumentation.Altimeter.indicatedFt.getValue();
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mode = Modes.PFD.FMA.pitchMode.getValue();
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ias = pts.Instrumentation.AirspeedIndicator.indicatedSpdKt.getValue();
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mach = pts.Instrumentation.AirspeedIndicator.indicatedMach.getValue();
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decel = FMGCNodes.decel.getValue();
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ktsmach = Input.ktsMach.getValue();
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kts_sel = Input.kts.getValue();
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mach_sel = Input.mach.getValue();
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srsSPD = getprop("/it-autoflight/settings/togaspd");
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phase = FMGCInternal.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
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flap = pts.Controls.Flight.flapsPos.getValue();
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decel = getprop("/FMGC/internal/decel");
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mode = Modes.PFD.FMA.pitchMode.getValue();
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srsSPD = srsSpeedNode.getValue();
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mng_alt_spd = math.round(FMGCNodes.mngSpdAlt.getValue(), 1);
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mng_alt_mach = math.round(FMGCNodes.mngMachAlt.getValue(), 0.001);
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if (mach > mng_alt_mach and (FMGCInternal.phase == 2 or FMGCInternal.phase == 3)) {
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# 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
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if (pts.Instrumentation.AirspeedIndicator.indicatedMach.getValue() > mng_alt_mach and (FMGCInternal.phase == 2 or FMGCInternal.phase == 3)) {
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FMGCInternal.machSwitchover = 1;
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} elsif (ias > mng_alt_spd and (FMGCInternal.phase == 4 or FMGCInternal.phase == 5)) {
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} elsif (pts.Instrumentation.AirspeedIndicator.indicatedSpdKt.getValue() > mng_alt_spd and (FMGCInternal.phase == 4 or FMGCInternal.phase == 5)) {
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FMGCInternal.machSwitchover = 0;
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}
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if ((mode == " " or mode == "SRS") and (FMGCInternal.phase == 0 or FMGCInternal.phase == 1)) {
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if (FMGCInternal.mngKtsMach) {
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FMGCInternal.mngKtsMach = 0;
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FMGCInternal.mngSpdCmd = srsSPD;
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} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude <= FMGCInternal.clbSpdLimAlt) {
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# Speed is maximum of greendot / climb speed limit
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FMGCInternal.mngKtsMach = 0;
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FMGCInternal.mngSpdCmd = decel ? FMGCInternal.minspeed : math.clamp(FMGCInternal.clbSpdLim, FMGCInternal.clean, 999);
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} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > (FMGCInternal.clbSpdLimAlt + 20)) {
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FMGCInternal.mngKtsMach = FMGCInternal.machSwitchover ? 1 : 0;
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FMGCInternal.mngSpdCmd = FMGCInternal.machSwitchover ? mng_alt_mach : mng_alt_spd;
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} elsif ((FMGCInternal.phase >= 4 and FMGCInternal.phase <= 6) and altitude > (FMGCInternal.desSpdLimAlt + 20)) {
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if (decel) {
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FMGCInternal.mngKtsMach = 0;
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}
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if (FMGCInternal.mngSpdCmd != srsSPD) {
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FMGCInternal.mngSpdCmd = srsSPD;
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}
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} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude <= 10050) {
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if (FMGCInternal.mngKtsMach) {
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FMGCInternal.mngKtsMach = 0;
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}
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if (FMGCInternal.mngSpdCmd != 250 and !decel) {
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FMGCInternal.mngSpdCmd = 250;
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} elsif (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
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FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
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}
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} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and !FMGCInternal.machSwitchover) {
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if (FMGCInternal.mngKtsMach) {
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FMGCInternal.mngKtsMach = 0;
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}
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if (FMGCInternal.mngSpdCmd != mng_alt_spd) {
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FMGCInternal.mngSpdCmd = mng_alt_spd;
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}
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} elsif ((FMGCInternal.phase == 2 or FMGCInternal.phase == 3) and altitude > 10070 and FMGCInternal.machSwitchover) {
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if (!FMGCInternal.mngKtsMach) {
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FMGCInternal.mngKtsMach = 1;
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}
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if (FMGCInternal.mngSpdCmd != mng_alt_mach) {
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FMGCInternal.mngSpdCmd = mng_alt_mach;
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}
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} elsif (FMGCInternal.phase == 4 and altitude > 11000 and !FMGCInternal.machSwitchover) {
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if (FMGCInternal.mngKtsMach) {
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FMGCInternal.mngKtsMach = 0;
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}
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if (FMGCInternal.mngSpdCmd != mng_alt_spd) {
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FMGCInternal.mngSpdCmd = mng_alt_spd;
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}
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} elsif (FMGCInternal.phase == 4 and altitude > 11000 and FMGCInternal.machSwitchover) {
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if (!FMGCInternal.mngKtsMach) {
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FMGCInternal.mngKtsMach = 1;
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}
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if (FMGCInternal.mngSpdCmd != mng_alt_mach) {
|
||||
FMGCInternal.mngSpdCmd = mng_alt_mach;
|
||||
}
|
||||
} elsif ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude > 11000 and !FMGCInternal.machSwitchover) {
|
||||
if (FMGCInternal.mngKtsMach) {
|
||||
FMGCInternal.mngKtsMach = 0;
|
||||
}
|
||||
if (FMGCInternal.mngSpdCmd != mng_alt_spd and !decel) {
|
||||
FMGCInternal.mngSpdCmd = mng_alt_spd;
|
||||
} elsif (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
|
||||
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
|
||||
}
|
||||
} elsif ((FMGCInternal.phase == 4 or FMGCInternal.phase == 5 or FMGCInternal.phase == 6) and altitude <= 10980) {
|
||||
if (FMGCInternal.mngKtsMach) {
|
||||
FMGCInternal.mngKtsMach = 0;
|
||||
}
|
||||
if (FMGCInternal.mngSpdCmd != 250 and !decel) {
|
||||
FMGCInternal.mngSpdCmd = 250;
|
||||
} elsif (FMGCInternal.mngSpdCmd != FMGCInternal.minspeed and decel) {
|
||||
FMGCInternal.mngSpdCmd = FMGCInternal.minspeed;
|
||||
} else {
|
||||
FMGCInternal.mngKtsMach = FMGCInternal.machSwitchover ? 1 : 0;
|
||||
FMGCInternal.mngSpdCmd = FMGCInternal.machSwitchover ? mng_alt_mach : mng_alt_spd;
|
||||
}
|
||||
} elsif ((FMGCInternal.phase >= 4 and FMGCInternal.phase <= 6) and altitude <= FMGCInternal.desSpdLimAlt) {
|
||||
FMGCInternal.mngKtsMach = 0;
|
||||
# Speed is maximum of greendot / descent speed limit
|
||||
FMGCInternal.mngSpdCmd = decel ? FMGCInternal.minspeed : math.clamp(FMGCInternal.desSpdLim, FMGCInternal.clean, 999);
|
||||
}
|
||||
|
||||
if (FMGCInternal.mngSpdCmd > FMGCInternal.maxspeed - 5) {
|
||||
FMGCInternal.mngSpd = (FMGCInternal.maxspeed - 5);
|
||||
# Clamp to minspeed, maxspeed
|
||||
if (FMGCInternal.phase >= 2) {
|
||||
if (!FMGCInternal.mngKtsMach) {
|
||||
FMGCInternal.mngSpd = math.clamp(FMGCInternal.mngSpdCmd, FMGCInternal.minspeed, FMGCInternal.maxspeed);
|
||||
} else {
|
||||
FMGCInternal.mngSpd = math.clamp(FMGCInternal.mngSpdCmd, ktToMach(FMGCInternal.minspeed), ktToMach(FMGCInternal.maxspeed));
|
||||
}
|
||||
} else {
|
||||
FMGCInternal.mngSpd = FMGCInternal.mngSpdCmd;
|
||||
}
|
||||
|
||||
# Update value of ktsMach
|
||||
if (ktsmach and !FMGCInternal.mngKtsMach) {
|
||||
Input.ktsMach.setValue(0);
|
||||
} elsif (!ktsmach and FMGCInternal.mngKtsMach) {
|
||||
Input.ktsMach.setValue(1);
|
||||
}
|
||||
|
||||
if (kts_sel != FMGCInternal.mngSpd and !ktsmach) {
|
||||
# Set target speed
|
||||
if (Input.kts.getValue() != FMGCInternal.mngSpd and !ktsmach) {
|
||||
Input.kts.setValue(FMGCInternal.mngSpd);
|
||||
} elsif (mach_sel != FMGCInternal.mngSpd and ktsmach) {
|
||||
} elsif (Input.mach.getValue() != FMGCInternal.mngSpd and ktsmach) {
|
||||
Input.mach.setValue(FMGCInternal.mngSpd);
|
||||
}
|
||||
} else {
|
||||
|
|
|
|||
|
|
@ -15,7 +15,7 @@ var MCDU_init = func(i) {
|
|||
var MCDU_reset = func(i) {
|
||||
setprop("/MCDU[" ~ i ~ "]/active", 0);
|
||||
setprop("/MCDU[" ~ i ~ "]/atsu-active", 0);
|
||||
setprop("it-autoflight/settings/togaspd", 157); #aka v2 clone
|
||||
setprop("/it-autoflight/settings/togaspd", 157); #aka v2 clone
|
||||
setprop("/MCDU[" ~ i ~ "]/last-fmgc-page", "STATUS");
|
||||
setprop("/MCDU[" ~ i ~ "]/last-atsu-page", "ATSUDLINK");
|
||||
setprop("/MCDU[" ~ i ~ "]/active-system","");
|
||||
|
|
@ -496,6 +496,8 @@ var lskbutton = func(btn, i) {
|
|||
mcdu_scratchpad.scratchpads[i].empty();
|
||||
}
|
||||
}
|
||||
} else if (page == "VERTREV") {
|
||||
canvas_mcdu.myVertRev[i].pushButtonLeft(2);
|
||||
} else if (page == "MCDUTEXT") {
|
||||
atsu.freeTexts[i].selection = 1;
|
||||
atsu.freeTexts[i].changed = 1;
|
||||
|
|
|
|||
|
|
@ -1,4 +1,5 @@
|
|||
var scratchpadStore = nil;
|
||||
var scratchpadSplit = nil;
|
||||
|
||||
var vertRev = {
|
||||
title: [nil, nil, nil],
|
||||
|
|
@ -77,7 +78,7 @@ var vertRev = {
|
|||
me.title = ["VERT REV", " AT ", "PPOS"];
|
||||
me.L1 = ["", " EFOB ---.-", "wht"];
|
||||
me.R1 = ["", "EXTRA ---.- ", "wht"];
|
||||
me.L2 = ["250/10000", " CLB SPD LIM", "mag"];
|
||||
me.L2 = [fmgc.FMGCInternal.clbSpdLim ~ "/" ~ fmgc.FMGCInternal.clbSpdLimAlt, " CLB SPD LIM", "mag"];
|
||||
me.L4 = [" CONSTANT MACH", nil, "wht"];
|
||||
me.L5 = [" WIND DATA", nil, "wht"];
|
||||
me.L6 = [" RETURN", nil, "wht"];
|
||||
|
|
@ -90,7 +91,7 @@ var vertRev = {
|
|||
me.fontMatrix = [[0, 0, 1, 0, 0, 0], [0, 0, 1, 0, 0, 0]];
|
||||
me.L1 = ["", " EFOB ---.-", "wht"];
|
||||
me.R1 = ["", "EXTRA ---.- ", "wht"];
|
||||
me.L2 = ["250/10000", " CLB SPD LIM", "mag"];
|
||||
me.L2 = [fmgc.FMGCInternal.clbSpdLim ~ "/" ~ fmgc.FMGCInternal.clbSpdLimAlt, " CLB SPD LIM", "mag"];
|
||||
me.speed = me.getSpd();
|
||||
if (me.speed[0] == nil) {
|
||||
me.L3 = [" [ ]", " SPD CSTR", "blu"];
|
||||
|
|
@ -130,7 +131,7 @@ var vertRev = {
|
|||
}
|
||||
me.L1 = ["", " EFOB ---.-", "wht"];
|
||||
me.R1 = ["", "EXTRA ---.- ", "wht"];
|
||||
me.L2 = ["250/10000", " CLB SPD LIM", "mag"];
|
||||
me.L2 = [fmgc.FMGCInternal.clbSpdLim ~ "/" ~ fmgc.FMGCInternal.clbSpdLimAlt, " CLB SPD LIM", "mag"];
|
||||
me.L4 = [" CONSTANT MACH", nil, "wht"];
|
||||
me.L5 = [" WIND DATA", nil, "wht"];
|
||||
me.L6 = [" RETURN", nil, "wht"];
|
||||
|
|
@ -146,7 +147,7 @@ var vertRev = {
|
|||
}
|
||||
me.L1 = ["", " EFOB ---.-", "wht"];
|
||||
me.R1 = ["", "EXTRA ---.- ", "wht"];
|
||||
me.L2 = ["250/10000", " DES SPD LIM", "mag"];
|
||||
me.L2 = [fmgc.FMGCInternal.desSpdLim ~ "/" ~ fmgc.FMGCInternal.desSpdLimAlt, " DES SPD LIM", "mag"];
|
||||
me.L4 = [" CONSTANT MACH", nil, "wht"];
|
||||
me.L5 = [" WIND DATA", nil, "wht"];
|
||||
me.L6 = [" RETURN", nil, "wht"];
|
||||
|
|
@ -180,7 +181,65 @@ var vertRev = {
|
|||
},
|
||||
pushButtonLeft: func(index) {
|
||||
scratchpadStore = mcdu_scratchpad.scratchpads[me.computer].scratchpad;
|
||||
if (index == 3 and me.type == 2) {
|
||||
if (index == 2) {
|
||||
if (scratchpadStore == "CLR") {
|
||||
if (me.type == 1) {
|
||||
fmgc.FMGCInternal.desSpdLim = 250;
|
||||
fmgc.FMGCInternal.desSpdLimAlt = 10000;
|
||||
fmgc.FMGCInternal.desSpdLimSet = 0;
|
||||
} else {
|
||||
fmgc.FMGCInternal.clbSpdLim = 250;
|
||||
fmgc.FMGCInternal.clbSpdLimAlt = 10000;
|
||||
fmgc.FMGCInternal.clbSpdLimSet = 0;
|
||||
}
|
||||
mcdu_scratchpad.scratchpads[me.computer].empty();
|
||||
me._setupPageWithData();
|
||||
canvas_mcdu.pageSwitch[me.computer].setBoolValue(0);
|
||||
} elsif (find("/", scratchpadStore) != -1) {
|
||||
scratchpadSplit = split("/", scratchpadStore);
|
||||
if (size(scratchpadSplit[0]) == 3 and num(scratchpadSplit[0]) != nil and size(scratchpadSplit[1]) >= 3 and size(scratchpadSplit[1]) <= 5 and num(scratchpadSplit[1]) != nil) {
|
||||
if (scratchpadSplit[0] >= 100 and scratchpadSplit[0] <= 340 and scratchpadSplit[1] >= 100 and scratchpadSplit[1] <= 39000) {
|
||||
if (me.type == 1) {
|
||||
fmgc.FMGCInternal.desSpdLim = scratchpadSplit[0];
|
||||
fmgc.FMGCInternal.desSpdLimSet = 1;
|
||||
if (size(scratchpadSplit[1]) != 0) {
|
||||
fmgc.FMGCInternal.desSpdLimAlt = scratchpadSplit[1];
|
||||
}
|
||||
} else {
|
||||
fmgc.FMGCInternal.clbSpdLim = scratchpadSplit[0];
|
||||
fmgc.FMGCInternal.clbSpdLimSet = 1;
|
||||
if (size(scratchpadSplit[1]) != 0) {
|
||||
fmgc.FMGCInternal.clbSpdLimAlt = scratchpadSplit[1];
|
||||
}
|
||||
}
|
||||
mcdu_scratchpad.scratchpads[me.computer].empty();
|
||||
me._setupPageWithData();
|
||||
canvas_mcdu.pageSwitch[me.computer].setBoolValue(0);
|
||||
} else {
|
||||
mcdu_message(me.computer, "ENTRY OUT OF RANGE");
|
||||
}
|
||||
} else {
|
||||
mcdu_message(me.computer, "FORMAT ERROR");
|
||||
}
|
||||
} elsif (num(scratchpadStore) != nil and size(scratchpadStore) == 3) {
|
||||
if (scratchpadStore >= 100 and scratchpadStore <= 340) {
|
||||
if (me.type == 1) {
|
||||
fmgc.FMGCInternal.desSpdLim = scratchpadStore;
|
||||
fmgc.FMGCInternal.desSpdLimSet = 1;
|
||||
} else {
|
||||
fmgc.FMGCInternal.clbSpdLim = scratchpadStore;
|
||||
fmgc.FMGCInternal.clbSpdLimSet = 1;
|
||||
}
|
||||
mcdu_scratchpad.scratchpads[me.computer].empty();
|
||||
me._setupPageWithData();
|
||||
canvas_mcdu.pageSwitch[me.computer].setBoolValue(0);
|
||||
} else {
|
||||
mcdu_message(me.computer, "ENTRY OUT OF RANGE");
|
||||
}
|
||||
} else {
|
||||
mcdu_message(me.computer, "FORMAT ERROR");
|
||||
}
|
||||
} elsif (index == 3 and me.type == 2) {
|
||||
if (scratchpadStore == "CLR") {
|
||||
me.wp.setSpeed("delete");
|
||||
mcdu_scratchpad.scratchpads[me.computer].empty();
|
||||
|
|
|
|||
|
|
@ -502,4 +502,26 @@
|
|||
|
||||
</channel>
|
||||
|
||||
<channel name="FMGC">
|
||||
|
||||
<fcs_function name="/FMGC/internal/kts-to-mach-factor">
|
||||
<function>
|
||||
<quotient>
|
||||
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
|
||||
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
|
||||
</quotient>
|
||||
</function>
|
||||
</fcs_function>
|
||||
|
||||
<fcs_function name="/FMGC/internal/mach-to-kts-factor">
|
||||
<function>
|
||||
<quotient>
|
||||
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
|
||||
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
|
||||
</quotient>
|
||||
</function>
|
||||
</fcs_function>
|
||||
|
||||
</channel>
|
||||
|
||||
</system>
|
||||
|
|
|
|||
Loading…
Reference in a new issue