This repository has been archived on 2021-09-26. You can view files and clone it, but cannot push or open issues or pull requests.
IDG-A32X/Models/Instruments/PFD/PFD.nas
2017-11-18 11:06:32 -05:00

842 lines
32 KiB
Text

# A3XX PFD
# Joshua Davidson (it0uchpods)
##############################################
# Copyright (c) Joshua Davidson (it0uchpods) #
##############################################
var PFD_1 = nil;
var PFD_2 = nil;
var PFD1_display = nil;
var PFD2_display = nil;
setprop("/instrumentation/pfd/vs-needle", 0);
setprop("/instrumentation/pfd/vs-digit-trans", 0);
setprop("/it-autoflight/input/spd-managed", 0);
setprop("/FMGC/internal/target-ias-pfd", 0);
setprop("/it-autoflight/output/ap1", 0);
setprop("/it-autoflight/output/ap2", 0);
setprop("/it-autoflight/output/fd1", 0);
setprop("/it-autoflight/output/fd2", 0);
setprop("/it-autoflight/output/athr", 0);
setprop("/instrumentation/pfd/alt-diff", 0);
setprop("/instrumentation/pfd/heading-deg", 0);
setprop("/instrumentation/pfd/horizon-pitch", 0);
setprop("/instrumentation/pfd/horizon-ground", 0);
setprop("/instrumentation/pfd/hdg-diff", 0);
setprop("/instrumentation/pfd/heading-scale", 0);
setprop("/instrumentation/pfd/track-deg", 0);
setprop("/instrumentation/pfd/track-hdg-diff", 0);
setprop("/it-autoflight/internal/vert-speed-fpm-pfd", 0);
setprop("/position/gear-agl-ft", 0);
setprop("/controls/flight/aileron-input-fast", 0);
setprop("/controls/flight/elevator-input-fast", 0);
var ASI = 0;
var ASItrgt = 0;
var ASItrgtdiff = 0;
var alt = 0;
var altTens = 0;
var state1 = getprop("/systems/thrust/state1");
var state2 = getprop("/systems/thrust/state2");
var ap1 = getprop("/it-autoflight/output/ap1");
var ap2 = getprop("/it-autoflight/output/ap2");
var fd1 = getprop("/it-autoflight/output/fd1");
var fd2 = getprop("/it-autoflight/output/fd2");
var athr = getprop("/it-autoflight/output/athr");
var throttle_mode = getprop("/modes/pfd/fma/throttle-mode");
var pitch_mode = getprop("/modes/pfd/fma/pitch-mode");
var pitch_mode_armed = getprop("/modes/pfd/fma/pitch-mode-armed");
var pitch_mode2_armed = getprop("/modes/pfd/fma/pitch-mode2-armed");
var roll_mode = getprop("/modes/pfd/fma/roll-mode");
var roll_mode_armed = getprop("/modes/pfd/fma/roll-mode-armed");
var thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
var thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
var pitch = getprop("/orientation/pitch-deg");
var roll = getprop("/orientation/roll-deg");
var wow1 = getprop("/gear/gear[1]/wow");
var wow2 = getprop("/gear/gear[2]/wow");
var pitch = 0;
var roll = 0;
var spdTrend_c = 0;
var canvas_PFD_base = {
init: func(canvas_group, file) {
var font_mapper = func(family, weight) {
return "LiberationFonts/LiberationSans-Regular.ttf";
};
canvas.parsesvg(canvas_group, file, {'font-mapper': font_mapper});
var svg_keys = me.getKeys();
foreach(var key; svg_keys) {
me[key] = canvas_group.getElementById(key);
var svg_keys = me.getKeys();
foreach (var key; svg_keys) {
me[key] = canvas_group.getElementById(key);
var clip_el = canvas_group.getElementById(key ~ "_clip");
if (clip_el != nil) {
clip_el.setVisible(0);
var tran_rect = clip_el.getTransformedBounds();
var clip_rect = sprintf("rect(%d,%d, %d,%d)",
tran_rect[1], # 0 ys
tran_rect[2], # 1 xe
tran_rect[3], # 2 ye
tran_rect[0]); #3 xs
# coordinates are top,right,bottom,left (ys, xe, ye, xs) ref: l621 of simgear/canvas/CanvasElement.cxx
me[key].set("clip", clip_rect);
me[key].set("clip-frame", canvas.Element.PARENT);
}
}
}
me.page = canvas_group;
me.AI_horizon_trans = me["AI_horizon"].createTransform();
me.AI_horizon_rot = me["AI_horizon"].createTransform();
me.AI_horizon_ground_trans = me["AI_horizon_ground"].createTransform();
me.AI_horizon_ground_rot = me["AI_horizon_ground"].createTransform();
me.AI_horizon_sky_rot = me["AI_horizon_sky"].createTransform();
me.AI_horizon_hdg_trans = me["AI_heading"].createTransform();
me.AI_horizon_hdg_rot = me["AI_heading"].createTransform();
return me;
},
getKeys: func() {
return [];
},
update: func() {
if ((getprop("/systems/electrical/bus/ac1") >= 110 or getprop("/systems/electrical/bus/ac2") >= 110) and getprop("/controls/lighting/DU/du1") > 0) {
PFD_1.page.show();
PFD_1.update();
} else {
PFD_1.page.hide();
}
if (getprop("/systems/electrical/bus/ac1") >= 110 and getprop("/systems/electrical/ac1-src") != "RAT" and getprop("/systems/electrical/bus/ac2") >= 110 and getprop("/systems/electrical/ac2-src") != "RAT" and getprop("/controls/lighting/DU/du6") > 0) {
PFD_2.page.show();
PFD_2.update();
} else {
PFD_2.page.hide();
}
},
updateCommon: func () {
state1 = getprop("/systems/thrust/state1");
state2 = getprop("/systems/thrust/state2");
ap1 = getprop("/it-autoflight/output/ap1");
ap2 = getprop("/it-autoflight/output/ap2");
fd1 = getprop("/it-autoflight/output/fd1");
fd2 = getprop("/it-autoflight/output/fd2");
athr = getprop("/it-autoflight/output/athr");
throttle_mode = getprop("/modes/pfd/fma/throttle-mode");
pitch_mode = getprop("/modes/pfd/fma/pitch-mode");
pitch_mode_armed = getprop("/modes/pfd/fma/pitch-mode-armed");
pitch_mode2_armed = getprop("/modes/pfd/fma/pitch-mode2-armed");
roll_mode = getprop("/modes/pfd/fma/roll-mode");
roll_mode_armed = getprop("/modes/pfd/fma/roll-mode-armed");
thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
pitch = getprop("/orientation/pitch-deg");
roll = getprop("/orientation/roll-deg");
wow1 = getprop("/gear/gear[1]/wow");
wow2 = getprop("/gear/gear[2]/wow");
# FMA MAN TOGA MCT FLX THR
if (athr == 1 and (state1 == "TOGA" or state1 == "MCT" or state1 == "MAN THR" or state2 == "TOGA" or state2 == "MCT" or state2 == "MAN THR")) {
me["FMA_man"].show();
me["FMA_manmode"].show();
if (state1 == "TOGA" or state2 == "TOGA") {
me["FMA_flx_box"].hide();
me["FMA_flxtemp"].hide();
me["FMA_man_box"].show();
me["FMA_manmode"].setText("TOGA");
me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
} else if ((state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83)) {
me["FMA_flx_box"].hide();
me["FMA_flxtemp"].hide();
me["FMA_man_box"].show();
me["FMA_manmode"].setText("THR");
me["FMA_man_box"].setColor(0.7333,0.3803,0);
} else if ((state1 == "MCT" or state2 == "MCT") and getprop("/controls/engines/thrust-limit") != "FLX") {
me["FMA_flx_box"].hide();
me["FMA_flxtemp"].hide();
me["FMA_man_box"].show();
me["FMA_manmode"].setText("MCT");
me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
} else if ((state1 == "MCT" or state2 == "MCT") and getprop("/controls/engines/thrust-limit") == "FLX") {
me["FMA_flxtemp"].setText(sprintf("%s", "+" ~ getprop("/FMGC/internal/flex")));
me["FMA_man_box"].hide();
me["FMA_flx_box"].show();
me["FMA_flxtemp"].show();
me["FMA_manmode"].setText("FLX ");
me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
} else if ((state1 == "MAN THR" and thr1 < 0.83) or (state2 == "MAN THR" and thr2 < 0.83)) {
me["FMA_flx_box"].hide();
me["FMA_flxtemp"].hide();
me["FMA_man_box"].show();
me["FMA_manmode"].setText("THR");
me["FMA_man_box"].setColor(0.7333,0.3803,0);
}
} else {
me["FMA_man"].hide();
me["FMA_manmode"].hide();
me["FMA_man_box"].hide();
me["FMA_flx_box"].hide();
me["FMA_flxtemp"].hide();
}
if (athr == 1 and getprop("/systems/thrust/lvrclb") == 1) {
me["FMA_lvrclb"].show();
} else {
me["FMA_lvrclb"].hide();
}
# FMA A/THR
if (athr == 1 and ((state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL"))) {
me["FMA_thrust"].show();
if (getprop("/modes/pfd/fma/throttle-mode-box") == 1 and throttle_mode != " ") {
me["FMA_thrust_box"].show();
} else {
me["FMA_thrust_box"].hide();
}
} else {
me["FMA_thrust"].hide();
me["FMA_thrust_box"].hide();
}
me["FMA_thrust"].setText(sprintf("%s", throttle_mode));
# FMA Pitch Roll Common
me["FMA_combined"].setText(sprintf("%s", pitch_mode));
if (pitch_mode == "LAND" or pitch_mode == "FLARE" or pitch_mode == "ROLL OUT") {
me["FMA_pitch"].hide();
me["FMA_roll"].hide();
me["FMA_pitch_box"].hide();
me["FMA_roll_box"].hide();
me["FMA_pitcharm_box"].hide();
me["FMA_rollarm_box"].hide();
me["FMA_Middle1"].hide();
me["FMA_Middle2"].hide();
if (getprop("/it-fbw/law") == 2) {
me["FMA_ctr_msg"].setText("USE MAN PITCH TRIM");
me["FMA_ctr_msg"].setColor(0.7333,0.3803,0);
me["FMA_ctr_msg"].show();
} else if (getprop("/it-fbw/law") == 3) {
me["FMA_ctr_msg"].setText("MAN PITCH TRIM ONLY");
me["FMA_ctr_msg"].setColor(1,0,0);
me["FMA_ctr_msg"].show();
} else {
me["FMA_ctr_msg"].hide();
}
me["FMA_combined"].show();
if (getprop("/modes/pfd/fma/pitch-mode-box") == 1 and pitch_mode != " ") {
me["FMA_combined_box"].show();
} else {
me["FMA_combined_box"].hide();
}
} else {
me["FMA_combined"].hide();
me["FMA_combined_box"].hide();
if (getprop("/it-fbw/law") == 2) {
me["FMA_ctr_msg"].setText("USE MAN PITCH TRIM");
me["FMA_ctr_msg"].setColor(0.7333,0.3803,0);
me["FMA_Middle1"].hide();
me["FMA_Middle2"].show();
me["FMA_ctr_msg"].show();
} else if (getprop("/it-fbw/law") == 3) {
me["FMA_ctr_msg"].setText("MAN PITCH TRIM ONLY");
me["FMA_ctr_msg"].setColor(1,0,0);
me["FMA_Middle1"].hide();
me["FMA_Middle2"].show();
me["FMA_ctr_msg"].show();
} else {
me["FMA_ctr_msg"].hide();
me["FMA_Middle1"].show();
me["FMA_Middle2"].hide();
}
if (ap1 or ap2 or fd1 or fd2) {
me["FMA_pitch"].show();
me["FMA_roll"].show();
} else {
me["FMA_pitch"].hide();
me["FMA_roll"].hide();
}
if (getprop("/modes/pfd/fma/pitch-mode-box") == 1 and pitch_mode != " " and (ap1 or ap2 or fd1 or fd2)) {
me["FMA_pitch_box"].show();
} else {
me["FMA_pitch_box"].hide();
}
if (pitch_mode_armed == " " and pitch_mode2_armed == " ") {
me["FMA_pitcharm_box"].hide();
} else {
if ((getprop("/modes/pfd/fma/pitch-mode-armed-box") == 1 or getprop("/modes/pfd/fma/pitch-mode2-armed-box") == 1) and (ap1 or ap2 or fd1 or fd2)) {
me["FMA_pitcharm_box"].show();
} else {
me["FMA_pitcharm_box"].hide();
}
}
if (getprop("/modes/pfd/fma/roll-mode-box") == 1 and roll_mode != " " and (ap1 or ap2 or fd1 or fd2)) {
me["FMA_roll_box"].show();
} else {
me["FMA_roll_box"].hide();
}
if (getprop("/modes/pfd/fma/roll-mode-armed-box") == 1 and roll_mode_armed != " " and (ap1 or ap2 or fd1 or fd2)) {
me["FMA_rollarm_box"].show();
} else {
me["FMA_rollarm_box"].hide();
}
}
if (ap1 or ap2 or fd1 or fd2) {
me["FMA_pitcharm"].show();
me["FMA_pitcharm2"].show();
me["FMA_rollarm"].show();
} else {
me["FMA_pitcharm"].hide();
me["FMA_pitcharm2"].hide();
me["FMA_rollarm"].hide();
}
# FMA Pitch
me["FMA_pitch"].setText(sprintf("%s", pitch_mode));
me["FMA_pitcharm"].setText(sprintf("%s", pitch_mode_armed));
me["FMA_pitcharm2"].setText(sprintf("%s", pitch_mode2_armed));
# FMA Roll
me["FMA_roll"].setText(sprintf("%s", roll_mode));
me["FMA_rollarm"].setText(sprintf("%s", roll_mode_armed));
# FMA CAT DH
me["FMA_catmode"].hide();
me["FMA_cattype"].hide();
me["FMA_catmode_box"].hide();
me["FMA_cattype_box"].hide();
me["FMA_cat_box"].hide();
me["FMA_nodh"].hide();
me["FMA_dh_box"].hide();
# FMA AP FD ATHR
me["FMA_ap"].setText(sprintf("%s", getprop("/modes/pfd/fma/ap-mode")));
me["FMA_fd"].setText(sprintf("%s", getprop("/modes/pfd/fma/fd-mode")));
me["FMA_athr"].setText(sprintf("%s", getprop("/modes/pfd/fma/at-mode")));
if ((state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL")) {
me["FMA_athr"].setColor(0.8078,0.8039,0.8078);
} else {
me["FMA_athr"].setColor(0.0862,0.5176,0.6470);
}
if (getprop("/modes/pfd/fma/ap-mode-box") == 1 and getprop("/modes/pfd/fma/ap-mode") != " ") {
me["FMA_ap_box"].show();
} else {
me["FMA_ap_box"].hide();
}
if (getprop("/modes/pfd/fma/fd-mode-box") == 1 and getprop("/modes/pfd/fma/fd-mode") != " ") {
me["FMA_fd_box"].show();
} else {
me["FMA_fd_box"].hide();
}
if (getprop("/modes/pfd/fma/athr-mode-box") == 1 and getprop("/modes/pfd/fma/at-mode") != " ") {
me["FMA_athr_box"].show();
} else {
me["FMA_athr_box"].hide();
}
# Airspeed
# Subtract 30, since the scale starts at 30, but don't allow less than 0, or more than 420 situations
if (getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") <= 30) {
ASI = 0;
} else if (getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") >= 420) {
ASI = 390;
} else {
ASI = getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") - 30;
}
me["ASI_scale"].setTranslation(0, ASI * 6.6);
if (getprop("/instrumentation/airspeed-indicator/indicated-mach") >= 0.5) {
me["ASI_mach_decimal"].show();
me["ASI_mach"].show();
} else {
me["ASI_mach_decimal"].hide();
me["ASI_mach"].hide();
}
if (getprop("/instrumentation/airspeed-indicator/indicated-mach") >= 0.999) {
me["ASI_mach"].setText("999");
} else {
me["ASI_mach"].setText(sprintf("%3.0f", getprop("/instrumentation/airspeed-indicator/indicated-mach") * 1000));
}
if (getprop("/it-autoflight/input/spd-managed") == 1) {
me["ASI_target"].setColor(0.6901,0.3333,0.7450);
me["ASI_digit_UP"].setColor(0.6901,0.3333,0.7450);
me["ASI_decimal_UP"].setColor(0.6901,0.3333,0.7450);
me["ASI_digit_DN"].setColor(0.6901,0.3333,0.7450);
me["ASI_decimal_DN"].setColor(0.6901,0.3333,0.7450);
} else {
me["ASI_target"].setColor(0.0862,0.5176,0.6470);
me["ASI_digit_UP"].setColor(0.0862,0.5176,0.6470);
me["ASI_decimal_UP"].setColor(0.0862,0.5176,0.6470);
me["ASI_digit_DN"].setColor(0.0862,0.5176,0.6470);
me["ASI_decimal_DN"].setColor(0.0862,0.5176,0.6470);
}
if (getprop("/FMGC/internal/target-ias-pfd") <= 30) {
ASItrgt = 0 - ASI;
} else if (getprop("/FMGC/internal/target-ias-pfd") >= 420) {
ASItrgt = 390 - ASI;
} else {
ASItrgt = getprop("/FMGC/internal/target-ias-pfd") - 30 - ASI;
}
ASItrgtdiff = getprop("/FMGC/internal/target-ias-pfd") - getprop("/instrumentation/airspeed-indicator/indicated-speed-kt");
if (ASItrgtdiff >= -42 and ASItrgtdiff <= 42) {
me["ASI_target"].setTranslation(0, ASItrgt * -6.6);
me["ASI_digit_UP"].hide();
me["ASI_decimal_UP"].hide();
me["ASI_digit_DN"].hide();
me["ASI_decimal_DN"].hide();
me["ASI_target"].show();
} else if (ASItrgtdiff < -42) {
if (getprop("/it-autoflight/input/kts-mach") == 1) {
me["ASI_digit_DN"].setText(sprintf("%3.0f", getprop("/it-autoflight/input/spd-mach") * 1000));
me["ASI_decimal_UP"].hide();
me["ASI_decimal_DN"].show();
} else {
me["ASI_digit_DN"].setText(sprintf("%3.0f", getprop("/it-autoflight/input/spd-kts")));
me["ASI_decimal_UP"].hide();
me["ASI_decimal_DN"].hide();
}
me["ASI_digit_DN"].show();
me["ASI_digit_UP"].hide();
me["ASI_target"].hide();
} else if (ASItrgtdiff > 42) {
if (getprop("/it-autoflight/input/kts-mach") == 1) {
me["ASI_digit_UP"].setText(sprintf("%3.0f", getprop("/it-autoflight/input/spd-mach") * 1000));
me["ASI_decimal_UP"].show();
me["ASI_decimal_DN"].hide();
} else {
me["ASI_digit_UP"].setText(sprintf("%3.0f", getprop("/it-autoflight/input/spd-kts")));
me["ASI_decimal_UP"].hide();
me["ASI_decimal_DN"].hide();
}
me["ASI_digit_UP"].show();
me["ASI_digit_DN"].hide();
me["ASI_target"].hide();
}
me["ASI_ten_sec"].hide();
# Attitude Indicator
pitch = getprop("/orientation/pitch-deg") or 0;
roll = getprop("/orientation/roll-deg") or 0;
me.AI_horizon_trans.setTranslation(0, pitch * 11.825);
me.AI_horizon_rot.setRotation(-roll * D2R, me["AI_center"].getCenter());
me.AI_horizon_ground_trans.setTranslation(0, getprop("/instrumentation/pfd/horizon-ground") * 11.825);
me.AI_horizon_ground_rot.setRotation(-roll * D2R, me["AI_center"].getCenter());
me.AI_horizon_sky_rot.setRotation(-roll * D2R, me["AI_center"].getCenter());
me["AI_slipskid"].setTranslation(getprop("/instrumentation/slip-skid-ball/indicated-slip-skid") * -15, 0);
me["AI_bank"].setRotation(-roll * D2R);
if (getprop("/it-fbw/law") == 0) {
me["AI_bank_lim"].show();
} else {
me["AI_bank_lim"].hide();
}
if (getprop("/it-autoflight/fd/roll-bar") != nil) {
me["FD_roll"].setTranslation((getprop("/it-autoflight/fd/roll-bar")) * 2.2, 0);
}
if (getprop("/it-autoflight/fd/pitch-bar") != nil) {
me["FD_pitch"].setTranslation(0, -(getprop("/it-autoflight/fd/pitch-bar")) * 3.8);
}
me["AI_agl"].setText(sprintf("%s", math.round(getprop("/position/gear-agl-ft"))));
if (getprop("/position/gear-agl-ft") <= getprop("/instrumentation/mk-viii/inputs/arinc429/decision-height")) {
me["AI_agl"].setColor(0.7333,0.3803,0);
} else {
me["AI_agl"].setColor(0.0509,0.7529,0.2941);
}
if (getprop("/position/gear-agl-ft") <= 2500) {
me["AI_agl"].show();
} else {
me["AI_agl"].hide();
}
me["AI_agl_g"].setRotation(-roll * D2R);
if ((wow1 or wow2) and getprop("/FMGC/status/phase") != 0 and getprop("/FMGC/status/phase") != 1) {
me["AI_stick"].show();
me["AI_stick_pos"].show();
} else if ((wow1 or wow2) and (getprop("/FMGC/status/phase") == 0 or getprop("/FMGC/status/phase") == 1) and (getprop("/engines/engine[0]/state") == 3 or getprop("/engines/engine[1]/state") == 3)) {
me["AI_stick"].show();
me["AI_stick_pos"].show();
} else {
me["AI_stick"].hide();
me["AI_stick_pos"].hide();
}
me["AI_stick_pos"].setTranslation(getprop("/controls/flight/aileron-input-fast") * 196.8, getprop("/controls/flight/elevator-input-fast") * 151.5);
# Altitude
me.altitude = getprop("/instrumentation/altimeter/indicated-altitude-ft");
me.altOffset = me.altitude / 500 - int(me.altitude / 500);
me.middleAltText = roundaboutAlt(me.altitude / 100);
me.middleAltOffset = nil;
if (me.altOffset > 0.5) {
me.middleAltOffset = -(me.altOffset - 1) * 243.3424;
} else {
me.middleAltOffset = -me.altOffset * 243.3424;
}
me["ALT_scale"].setTranslation(0, -me.middleAltOffset);
me["ALT_scale"].update();
me["ALT_five"].setText(sprintf("%03d", me.middleAltText+10));
me["ALT_four"].setText(sprintf("%03d", me.middleAltText+5));
me["ALT_three"].setText(sprintf("%03d", me.middleAltText));
me["ALT_two"].setText(sprintf("%03d", me.middleAltText-5));
me["ALT_one"].setText(sprintf("%03d", me.middleAltText-10));
me["ALT_digits"].setText(sprintf("%s", getprop("/instrumentation/altimeter/indicated-altitude-ft-pfd")));
altTens = num(right(sprintf("%02d", getprop("/instrumentation/altimeter/indicated-altitude-ft")), 2));
me["ALT_tens"].setTranslation(0, altTens * 1.392);
if (getprop("/instrumentation/pfd/alt-diff") >= -565 and getprop("/instrumentation/pfd/alt-diff") <= 565) {
me["ALT_target"].setTranslation(0, (getprop("/instrumentation/pfd/alt-diff") / 100) * -48.66856);
me["ALT_target_digit"].setText(sprintf("%03d", math.round(getprop("/it-autoflight/internal/alt") / 100)));
me["ALT_digit_UP"].hide();
me["ALT_digit_DN"].hide();
me["ALT_target"].show();
} else if (getprop("/instrumentation/pfd/alt-diff") < -565) {
if (getprop("/modes/altimeter/std") == 1) {
if (getprop("/it-autoflight/internal/alt") < 10000) {
me["ALT_digit_DN"].setText(sprintf("%s", "FL " ~ getprop("/it-autoflight/internal/alt") / 100));
} else {
me["ALT_digit_DN"].setText(sprintf("%s", "FL " ~ getprop("/it-autoflight/internal/alt") / 100));
}
} else {
me["ALT_digit_DN"].setText(sprintf("%5.0f", getprop("/it-autoflight/internal/alt")));
}
me["ALT_digit_DN"].show();
me["ALT_digit_UP"].hide();
me["ALT_target"].hide();
} else if (getprop("/instrumentation/pfd/alt-diff") > 565) {
if (getprop("/modes/altimeter/std") == 1) {
if (getprop("/it-autoflight/internal/alt") < 10000) {
me["ALT_digit_UP"].setText(sprintf("%s", "FL " ~ getprop("/it-autoflight/internal/alt") / 100));
} else {
me["ALT_digit_UP"].setText(sprintf("%s", "FL " ~ getprop("/it-autoflight/internal/alt") / 100));
}
} else {
me["ALT_digit_UP"].setText(sprintf("%5.0f", getprop("/it-autoflight/internal/alt")));
}
me["ALT_digit_UP"].show();
me["ALT_digit_DN"].hide();
me["ALT_target"].hide();
}
# QNH
if (getprop("/modes/altimeter/std") == 1) {
me["QNH"].hide();
me["QNH_setting"].hide();
me["QNH_std"].show();
me["QNH_box"].show();
} else if (getprop("/modes/altimeter/inhg") == 0) {
me["QNH_setting"].setText(sprintf("%4.0f", getprop("/instrumentation/altimeter/setting-hpa")));
me["QNH"].show();
me["QNH_setting"].show();
me["QNH_std"].hide();
me["QNH_box"].hide();
} else if (getprop("/modes/altimeter/inhg") == 1) {
me["QNH_setting"].setText(sprintf("%2.2f", getprop("/instrumentation/altimeter/setting-inhg")));
me["QNH"].show();
me["QNH_setting"].show();
me["QNH_std"].hide();
me["QNH_box"].hide();
}
# Vertical Speed
me["VS_pointer"].setRotation(getprop("/instrumentation/pfd/vs-needle") * D2R);
me["VS_box"].setTranslation(0, getprop("/instrumentation/pfd/vs-digit-trans"));
if (getprop("/it-autoflight/internal/vert-speed-fpm-pfd") < 2) {
me["VS_box"].hide();
} else {
me["VS_box"].show();
}
if (getprop("/it-autoflight/internal/vert-speed-fpm-pfd") < 10) {
me["VS_digit"].setText(sprintf("%02d", "0" ~ getprop("/it-autoflight/internal/vert-speed-fpm-pfd")));
} else {
me["VS_digit"].setText(sprintf("%02d", getprop("/it-autoflight/internal/vert-speed-fpm-pfd")));
}
# ILS
me["LOC_pointer"].setTranslation(getprop("/instrumentation/nav[0]/heading-needle-deflection-norm") * 197, 0);
me["GS_pointer"].setTranslation(0, getprop("/instrumentation/nav[0]/gs-needle-deflection-norm") * -197);
# Heading
me.heading = getprop("/instrumentation/pfd/heading-scale");
me.headOffset = me.heading / 10 - int(me.heading / 10);
me.middleText = roundabout(me.heading / 10);
me.middleOffset = nil;
if(me.middleText == 36) {
me.middleText = 0;
}
me.leftText1 = me.middleText == 0?35:me.middleText - 1;
me.rightText1 = me.middleText == 35?0:me.middleText + 1;
me.leftText2 = me.leftText1 == 0?35:me.leftText1 - 1;
me.rightText2 = me.rightText1 == 35?0:me.rightText1 + 1;
me.leftText3 = me.leftText2 == 0?35:me.leftText2 - 1;
me.rightText3 = me.rightText2 == 35?0:me.rightText2 + 1;
if (me.headOffset > 0.5) {
me.middleOffset = -(me.headOffset - 1) * 98.5416;
} else {
me.middleOffset = -me.headOffset * 98.5416;
}
me["HDG_scale"].setTranslation(me.middleOffset, 0);
me["HDG_scale"].update();
me["HDG_four"].setText(sprintf("%d", me.middleText));
me["HDG_five"].setText(sprintf("%d", me.rightText1));
me["HDG_three"].setText(sprintf("%d", me.leftText1));
me["HDG_six"].setText(sprintf("%d", me.rightText2));
me["HDG_two"].setText(sprintf("%d", me.leftText2));
me["HDG_seven"].setText(sprintf("%d", me.rightText3));
me["HDG_one"].setText(sprintf("%d", me.leftText3));
me["HDG_four"].setFontSize(fontSizeHDG(me.middleText), 1);
me["HDG_five"].setFontSize(fontSizeHDG(me.rightText1), 1);
me["HDG_three"].setFontSize(fontSizeHDG(me.leftText1), 1);
me["HDG_six"].setFontSize(fontSizeHDG(me.rightText2), 1);
me["HDG_two"].setFontSize(fontSizeHDG(me.leftText2), 1);
me["HDG_seven"].setFontSize(fontSizeHDG(me.rightText3), 1);
me["HDG_one"].setFontSize(fontSizeHDG(me.leftText3), 1);
if (getprop("/it-autoflight/custom/show-hdg") == 1 and getprop("/instrumentation/pfd/hdg-diff") >= -23.62 and getprop("/instrumentation/pfd/hdg-diff") <= 23.62) {
me["HDG_target"].setTranslation((getprop("/instrumentation/pfd/hdg-diff") / 10) * 98.5416, 0);
me["HDG_digit_L"].hide();
me["HDG_digit_R"].hide();
me["HDG_target"].show();
} else if (getprop("/it-autoflight/custom/show-hdg") == 1 and getprop("/instrumentation/pfd/hdg-diff") < -23.62 and getprop("/instrumentation/pfd/hdg-diff") >= -180) {
me["HDG_digit_L"].setText(sprintf("%3.0f", getprop("/it-autoflight/input/hdg")));
me["HDG_digit_L"].show();
me["HDG_digit_R"].hide();
me["HDG_target"].hide();
} else if (getprop("/it-autoflight/custom/show-hdg") == 1 and getprop("/instrumentation/pfd/hdg-diff") > 23.62 and getprop("/instrumentation/pfd/hdg-diff") <= 180) {
me["HDG_digit_R"].setText(sprintf("%3.0f", getprop("/it-autoflight/input/hdg")));
me["HDG_digit_R"].show();
me["HDG_digit_L"].hide();
me["HDG_target"].hide();
} else {
me["HDG_digit_L"].hide();
me["HDG_digit_R"].hide();
me["HDG_target"].hide();
}
me["TRK_pointer"].setTranslation((getprop("/instrumentation/pfd/track-hdg-diff") / 10) * 98.5416, 0);
me["CRS_pointer"].hide();
# AI HDG
me.AI_horizon_hdg_trans.setTranslation(me.middleOffset, getprop("/instrumentation/pfd/horizon-pitch") * 11.825);
me.AI_horizon_hdg_rot.setRotation(-roll * D2R, me["AI_center"].getCenter());
me["AI_heading"].update();
},
};
var canvas_PFD_1 = {
new: func(canvas_group, file) {
var m = {parents: [canvas_PFD_1, canvas_PFD_base]};
m.init(canvas_group, file);
return m;
},
getKeys: func() {
return ["FMA_man","FMA_manmode","FMA_flxtemp","FMA_thrust","FMA_lvrclb","FMA_pitch","FMA_pitcharm","FMA_pitcharm2","FMA_roll","FMA_rollarm","FMA_combined","FMA_ctr_msg","FMA_catmode","FMA_cattype","FMA_nodh","FMA_dh","FMA_dhn","FMA_ap","FMA_fd",
"FMA_athr","FMA_man_box","FMA_flx_box","FMA_thrust_box","FMA_pitch_box","FMA_pitcharm_box","FMA_roll_box","FMA_rollarm_box","FMA_combined_box","FMA_catmode_box","FMA_cattype_box","FMA_cat_box","FMA_dh_box","FMA_ap_box","FMA_fd_box","FMA_athr_box",
"FMA_Middle1","FMA_Middle2","ASI_scale","ASI_target","ASI_mach","ASI_mach_decimal","ASI_ten_sec","ASI_digit_UP","ASI_digit_DN","ASI_decimal_UP","ASI_decimal_DN","AI_center","AI_bank","AI_bank_lim","AI_slipskid","AI_horizon","AI_horizon_ground",
"AI_horizon_sky","AI_stick","AI_stick_pos","AI_heading","AI_agl_g","AI_agl","FD_roll","FD_pitch","ALT_scale","ALT_target","ALT_target_digit","ALT_one","ALT_two","ALT_three","ALT_four","ALT_five","ALT_digits","ALT_tens","ALT_digit_UP","ALT_digit_DN",
"VS_pointer","VS_box","VS_digit","QNH","QNH_setting","QNH_std","QNH_box","LOC_pointer","LOC_scale","GS_scale","GS_pointer","CRS_pointer","HDG_target","HDG_scale","HDG_one","HDG_two","HDG_three","HDG_four","HDG_five","HDG_six","HDG_seven","HDG_digit_L",
"HDG_digit_R","TRK_pointer"];
},
update: func() {
fd1 = getprop("/it-autoflight/output/fd1");
fd2 = getprop("/it-autoflight/output/fd2");
pitch_mode = getprop("/modes/pfd/fma/pitch-mode");
roll_mode = getprop("/modes/pfd/fma/roll-mode");
pitch = getprop("/orientation/pitch-deg");
roll = getprop("/orientation/roll-deg");
wow1 = getprop("/gear/gear[1]/wow");
wow2 = getprop("/gear/gear[2]/wow");
# FD
if (fd1 == 1 and ((!wow1 and !wow2 and roll_mode != " ") or roll_mode != " ") and getprop("/it-autoflight/custom/trk-fpa") == 0 and pitch < 25 and pitch > -13 and roll < 45 and roll > -45) {
me["FD_roll"].show();
} else {
me["FD_roll"].hide();
}
if (fd1 == 1 and ((!wow1 and !wow2 and pitch_mode != " ") or pitch_mode != " ") and getprop("/it-autoflight/custom/trk-fpa") == 0 and pitch < 25 and pitch > -13 and roll < 45 and roll > -45) {
me["FD_pitch"].show();
} else {
me["FD_pitch"].hide();
}
# ILS
if (getprop("/modes/pfd/ILS1") == 1) {
me["LOC_scale"].show();
me["GS_scale"].show();
} else {
me["LOC_scale"].hide();
me["GS_scale"].hide();
}
if (getprop("/modes/pfd/ILS1") == 1 and getprop("/instrumentation/nav[0]/in-range") == 1 and getprop("/instrumentation/nav[0]/nav-loc") == 1 and getprop("/instrumentation/nav[0]/signal-quality-norm") > 0.99) {
me["LOC_pointer"].show();
} else {
me["LOC_pointer"].hide();
}
if (getprop("/modes/pfd/ILS1") == 1 and getprop("/instrumentation/nav[0]/gs-in-range") == 1 and getprop("/instrumentation/nav[0]/has-gs") == 1 and getprop("/instrumentation/nav[0]/signal-quality-norm") > 0.99) {
me["GS_pointer"].show();
} else {
me["GS_pointer"].hide();
}
me.updateCommon();
},
};
var canvas_PFD_2 = {
new: func(canvas_group, file) {
var m = {parents: [canvas_PFD_2, canvas_PFD_base]};
m.init(canvas_group, file);
return m;
},
getKeys: func() {
return ["FMA_man","FMA_manmode","FMA_flxtemp","FMA_thrust","FMA_lvrclb","FMA_pitch","FMA_pitcharm","FMA_pitcharm2","FMA_roll","FMA_rollarm","FMA_combined","FMA_ctr_msg","FMA_catmode","FMA_cattype","FMA_nodh","FMA_dh","FMA_dhn","FMA_ap","FMA_fd",
"FMA_athr","FMA_man_box","FMA_flx_box","FMA_thrust_box","FMA_pitch_box","FMA_pitcharm_box","FMA_roll_box","FMA_rollarm_box","FMA_combined_box","FMA_catmode_box","FMA_cattype_box","FMA_cat_box","FMA_dh_box","FMA_ap_box","FMA_fd_box","FMA_athr_box",
"FMA_Middle1","FMA_Middle2","ASI_scale","ASI_target","ASI_mach","ASI_mach_decimal","ASI_ten_sec","ASI_digit_UP","ASI_digit_DN","ASI_decimal_UP","ASI_decimal_DN","AI_center","AI_bank","AI_bank_lim","AI_slipskid","AI_horizon","AI_horizon_ground",
"AI_horizon_sky","AI_stick","AI_stick_pos","AI_heading","AI_agl_g","AI_agl","FD_roll","FD_pitch","ALT_scale","ALT_target","ALT_target_digit","ALT_one","ALT_two","ALT_three","ALT_four","ALT_five","ALT_digits","ALT_tens","ALT_digit_UP","ALT_digit_DN",
"VS_pointer","VS_box","VS_digit","QNH","QNH_setting","QNH_std","QNH_box","LOC_pointer","LOC_scale","GS_scale","GS_pointer","CRS_pointer","HDG_target","HDG_scale","HDG_one","HDG_two","HDG_three","HDG_four","HDG_five","HDG_six","HDG_seven","HDG_digit_L",
"HDG_digit_R","TRK_pointer"];
},
update: func() {
fd1 = getprop("/it-autoflight/output/fd1");
fd2 = getprop("/it-autoflight/output/fd2");
pitch_mode = getprop("/modes/pfd/fma/pitch-mode");
roll_mode = getprop("/modes/pfd/fma/roll-mode");
pitch = getprop("/orientation/pitch-deg");
roll = getprop("/orientation/roll-deg");
wow1 = getprop("/gear/gear[1]/wow");
wow2 = getprop("/gear/gear[2]/wow");
# FD
if (fd2 == 1 and ((!wow1 and !wow2 and roll_mode != " ") or roll_mode != " ") and getprop("/it-autoflight/custom/trk-fpa") == 0 and pitch < 25 and pitch > -13 and roll < 45 and roll > -45) {
me["FD_roll"].show();
} else {
me["FD_roll"].hide();
}
if (fd2 == 1 and ((!wow1 and !wow2 and pitch_mode != " ") or pitch_mode != " ") and getprop("/it-autoflight/custom/trk-fpa") == 0 and pitch < 25 and pitch > -13 and roll < 45 and roll > -45) {
me["FD_pitch"].show();
} else {
me["FD_pitch"].hide();
}
# ILS
if (getprop("/modes/pfd/ILS2") == 1) {
me["LOC_scale"].show();
me["GS_scale"].show();
} else {
me["LOC_scale"].hide();
me["GS_scale"].hide();
}
if (getprop("/modes/pfd/ILS2") == 1 and getprop("/instrumentation/nav[0]/in-range") == 1 and getprop("/instrumentation/nav[0]/nav-loc") == 1 and getprop("/instrumentation/nav[0]/signal-quality-norm") > 0.99) {
me["LOC_pointer"].show();
} else {
me["LOC_pointer"].hide();
}
if (getprop("/modes/pfd/ILS2") == 1 and getprop("/instrumentation/nav[0]/gs-in-range") == 1 and getprop("/instrumentation/nav[0]/has-gs") == 1 and getprop("/instrumentation/nav[0]/signal-quality-norm") > 0.99) {
me["GS_pointer"].show();
} else {
me["GS_pointer"].hide();
}
me.updateCommon();
},
};
setprop("/testing", 0); # REMOVE WHEN PFD FINISHED
setlistener("sim/signals/fdm-initialized", func {
PFD1_display = canvas.new({
"name": "PFD1",
"size": [1024, 1024],
"view": [1024, 1024],
"mipmapping": 1
});
PFD2_display = canvas.new({
"name": "PFD2",
"size": [1024, 1024],
"view": [1024, 1024],
"mipmapping": 1
});
PFD1_display.addPlacement({"node": "pfd1.screen"});
PFD2_display.addPlacement({"node": "pfd2.screen"});
var group_pfd1 = PFD1_display.createGroup();
var group_pfd2 = PFD2_display.createGroup();
PFD_1 = canvas_PFD_1.new(group_pfd1, "Aircraft/IDG-A32X/Models/Instruments/PFD/res/pfd.svg");
PFD_2 = canvas_PFD_2.new(group_pfd2, "Aircraft/IDG-A32X/Models/Instruments/PFD/res/pfd.svg");
PFD_update.start();
});
var PFD_update = maketimer(0.05, func {
canvas_PFD_base.update();
});
var showPFD1 = func {
var dlg = canvas.Window.new([512, 512], "dialog").set("resize", 1);
dlg.setCanvas(PFD1_display);
}
var showPFD2 = func {
var dlg = canvas.Window.new([512, 512], "dialog").set("resize", 1);
dlg.setCanvas(PFD2_display);
}
var roundabout = func(x) {
var y = x - int(x);
return y < 0.5 ? int(x) : 1 + int(x) ;
};
var roundaboutAlt = func(x) {
var y = x * 0.2 - int(x * 0.2);
return y < 0.5 ? 5 * int(x*0.2) : 5 + 5 * int(x*0.2) ;
};
var fontSizeHDG = func(input) {
var test = input / 3;
if (test == int(test)) {
return 42;
} else {
return 32;
}
};