549 lines
20 KiB
Text
549 lines
20 KiB
Text
# A3XX PFD
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# Joshua Davidson (it0uchpods)
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#########################################
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# Copyright (c) it0uchpods Design Group #
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#########################################
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var PFD_1 = nil;
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var PFD_display = nil;
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setprop("/instrumentation/pfd/vs-needle", 0);
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setprop("/instrumentation/pfd/vs-digit-trans", 0);
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setprop("/it-autoflight/input/spd-managed", 0);
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setprop("/FMGC/internal/target-ias-pfd", 0);
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setprop("/it-autoflight/output/ap1", 0);
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setprop("/it-autoflight/output/ap2", 0);
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setprop("/it-autoflight/output/fd1", 0);
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setprop("/it-autoflight/output/fd2", 0);
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setprop("/it-autoflight/output/athr", 0);
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setprop("/instrumentation/pfd/horizon-pitch", 0);
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setprop("/it-autoflight/internal/vert-speed-fpm-pfd", 0);
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setprop("/position/gear-agl-ft", 0);
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setprop("/controls/flight/aileron-input-fast", 0);
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setprop("/controls/flight/elevator-input-fast", 0);
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var ASI = 0;
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var ASItrgt = 0;
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var alt = 0;
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var altTens = 0;
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var state1 = getprop("/systems/thrust/state1");
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var state2 = getprop("/systems/thrust/state2");
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var ap1 = getprop("/it-autoflight/output/ap1");
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var ap2 = getprop("/it-autoflight/output/ap2");
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var fd1 = getprop("/it-autoflight/output/fd1");
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var fd2 = getprop("/it-autoflight/output/fd2");
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var athr = getprop("/it-autoflight/output/athr");
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var throttle_mode = getprop("/modes/pfd/fma/throttle-mode");
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var pitch_mode = getprop("/modes/pfd/fma/pitch-mode");
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var pitch_mode_armed = getprop("/modes/pfd/fma/pitch-mode-armed");
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var pitch_mode2_armed = getprop("/modes/pfd/fma/pitch-mode2-armed");
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var roll_mode = getprop("/modes/pfd/fma/roll-mode");
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var roll_mode_armed = getprop("/modes/pfd/fma/roll-mode-armed");
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var thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
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var thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
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var pitch = getprop("/orientation/pitch-deg");
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var roll = getprop("/orientation/roll-deg");
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var wow1 = getprop("/gear/gear[1]/wow");
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var wow2 = getprop("/gear/gear[2]/wow");
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var pitch = 0;
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var roll = 0;
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var spdTrend_c = 0;
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var canvas_PFD_base = {
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init: func(canvas_group, file) {
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var font_mapper = func(family, weight) {
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return "LiberationFonts/LiberationSans-Regular.ttf";
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};
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canvas.parsesvg(canvas_group, file, {'font-mapper': font_mapper});
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var svg_keys = me.getKeys();
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foreach(var key; svg_keys) {
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me[key] = canvas_group.getElementById(key);
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var svg_keys = me.getKeys();
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foreach (var key; svg_keys) {
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me[key] = canvas_group.getElementById(key);
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var clip_el = canvas_group.getElementById(key ~ "_clip");
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if (clip_el != nil) {
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clip_el.setVisible(0);
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var tran_rect = clip_el.getTransformedBounds();
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var clip_rect = sprintf("rect(%d,%d, %d,%d)",
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tran_rect[1], # 0 ys
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tran_rect[2], # 1 xe
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tran_rect[3], # 2 ye
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tran_rect[0]); #3 xs
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# coordinates are top,right,bottom,left (ys, xe, ye, xs) ref: l621 of simgear/canvas/CanvasElement.cxx
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me[key].set("clip", clip_rect);
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me[key].set("clip-frame", canvas.Element.PARENT);
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}
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}
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}
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me.AI_horizon_trans = me["AI_horizon"].createTransform();
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me.AI_horizon_rot = me["AI_horizon"].createTransform();
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me.AI_horizon_ground_trans = me["AI_horizon_ground"].createTransform();
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me.AI_horizon_ground_rot = me["AI_horizon_ground"].createTransform();
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me.AI_horizon_sky_rot = me["AI_horizon_sky"].createTransform();
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me.page = canvas_group;
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return me;
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},
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getKeys: func() {
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return [];
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},
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update: func() {
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if ((getprop("/systems/electrical/bus/ac1") >= 110 or getprop("/systems/electrical/bus/ac2") >= 110) and getprop("/controls/electrical/switches/emer-gen") != 1 and getprop("/options/test-canvas") == 1 and getprop("/controls/lighting/DU/du1") > 0) {
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PFD_1.page.show();
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PFD_1.update();
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} else {
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PFD_1.page.hide();
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}
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},
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};
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var canvas_PFD_1 = {
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new: func(canvas_group, file) {
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var m = {parents: [canvas_PFD_1, canvas_PFD_base]};
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m.init(canvas_group, file);
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return m;
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},
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getKeys: func() {
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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",
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"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",
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"FMA_Middle1","FMA_Middle2","ASI_scale","ASI_target","ASI_mach","ASI_mach_decimal","ASI_ten_sec","AI_center","AI_bank","AI_slipskid","AI_horizon","AI_horizon_ground","AI_horizon_sky","AI_stick","AI_stick_pos","AI_agl_g","AI_agl","FD_roll","FD_pitch",
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"ALT_digits","ALT_tens","VS_pointer","VS_box","VS_digit","QNH","QNH_setting","QNH_std","QNH_box","LOC_pointer","LOC_scale","GS_scale","GS_pointer","HDG_target"];
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},
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update: func() {
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state1 = getprop("/systems/thrust/state1");
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state2 = getprop("/systems/thrust/state2");
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ap1 = getprop("/it-autoflight/output/ap1");
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ap2 = getprop("/it-autoflight/output/ap2");
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fd1 = getprop("/it-autoflight/output/fd1");
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fd2 = getprop("/it-autoflight/output/fd2");
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athr = getprop("/it-autoflight/output/athr");
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throttle_mode = getprop("/modes/pfd/fma/throttle-mode");
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pitch_mode = getprop("/modes/pfd/fma/pitch-mode");
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pitch_mode_armed = getprop("/modes/pfd/fma/pitch-mode-armed");
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pitch_mode2_armed = getprop("/modes/pfd/fma/pitch-mode2-armed");
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roll_mode = getprop("/modes/pfd/fma/roll-mode");
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roll_mode_armed = getprop("/modes/pfd/fma/roll-mode-armed");
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thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
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thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
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pitch = getprop("/orientation/pitch-deg");
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roll = getprop("/orientation/roll-deg");
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wow1 = getprop("/gear/gear[1]/wow");
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wow2 = getprop("/gear/gear[2]/wow");
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# FMA MAN TOGA MCT FLX THR
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if (athr == 1 and (state1 == "TOGA" or state1 == "MCT" or state1 == "MAN THR" or state2 == "TOGA" or state2 == "MCT" or state2 == "MAN THR")) {
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me["FMA_man"].show();
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me["FMA_manmode"].show();
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if (state1 == "TOGA" or state2 == "TOGA") {
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me["FMA_flx_box"].hide();
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me["FMA_flxtemp"].hide();
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me["FMA_man_box"].show();
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me["FMA_manmode"].setText("TOGA");
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me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
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} else if ((state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83)) {
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me["FMA_flx_box"].hide();
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me["FMA_flxtemp"].hide();
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me["FMA_man_box"].show();
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me["FMA_manmode"].setText("THR");
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me["FMA_man_box"].setColor(0.7333,0.3803,0);
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} else if ((state1 == "MCT" or state2 == "MCT") and getprop("/controls/engines/thrust-limit") != "FLX") {
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me["FMA_flx_box"].hide();
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me["FMA_flxtemp"].hide();
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me["FMA_man_box"].show();
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me["FMA_manmode"].setText("MCT");
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me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
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} else if ((state1 == "MCT" or state2 == "MCT") and getprop("/controls/engines/thrust-limit") == "FLX") {
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me["FMA_flxtemp"].setText(sprintf("%s", "+" ~ getprop("/FMGC/internal/flex")));
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me["FMA_man_box"].hide();
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me["FMA_flx_box"].show();
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me["FMA_flxtemp"].show();
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me["FMA_manmode"].setText("FLX ");
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me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
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} else if ((state1 == "MAN THR" and thr1 < 0.83) or (state2 == "MAN THR" and thr2 < 0.83)) {
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me["FMA_flx_box"].hide();
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me["FMA_flxtemp"].hide();
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me["FMA_man_box"].show();
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me["FMA_manmode"].setText("THR");
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me["FMA_man_box"].setColor(0.7333,0.3803,0);
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}
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} else {
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me["FMA_man"].hide();
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me["FMA_manmode"].hide();
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me["FMA_man_box"].hide();
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me["FMA_flx_box"].hide();
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me["FMA_flxtemp"].hide();
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}
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if (athr == 1 and getprop("/systems/thrust/lvrclb") == 1) {
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me["FMA_lvrclb"].show();
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} else {
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me["FMA_lvrclb"].hide();
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}
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# FMA A/THR
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if (athr == 1 and ((state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL"))) {
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me["FMA_thrust"].show();
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if (getprop("/modes/pfd/fma/throttle-mode-box") == 1 and throttle_mode != " ") {
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me["FMA_thrust_box"].show();
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} else {
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me["FMA_thrust_box"].hide();
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}
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} else {
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me["FMA_thrust"].hide();
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me["FMA_thrust_box"].hide();
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}
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me["FMA_thrust"].setText(sprintf("%s", throttle_mode));
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# FMA Pitch Roll Common
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me["FMA_combined"].setText(sprintf("%s", pitch_mode));
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if (pitch_mode == "LAND" or pitch_mode == "FLARE" or pitch_mode == "ROLL OUT") {
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me["FMA_pitch"].hide();
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me["FMA_roll"].hide();
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me["FMA_pitch_box"].hide();
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me["FMA_roll_box"].hide();
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me["FMA_pitcharm_box"].hide();
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me["FMA_rollarm_box"].hide();
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me["FMA_Middle1"].hide();
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me["FMA_Middle2"].hide();
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if (getprop("/it-fbw/law") == 2) {
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me["FMA_ctr_msg"].setText("USE MAN PITCH TRIM");
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me["FMA_ctr_msg"].setColor(0.7333,0.3803,0);
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me["FMA_ctr_msg"].show();
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} else if (getprop("/it-fbw/law") == 3) {
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me["FMA_ctr_msg"].setText("MAN PITCH TRIM ONLY");
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me["FMA_ctr_msg"].setColor(1,0,0);
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me["FMA_ctr_msg"].show();
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} else {
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me["FMA_ctr_msg"].hide();
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}
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me["FMA_combined"].show();
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if (getprop("/modes/pfd/fma/pitch-mode-box") == 1 and pitch_mode != " ") {
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me["FMA_combined_box"].show();
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} else {
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me["FMA_combined_box"].hide();
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}
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} else {
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me["FMA_combined"].hide();
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me["FMA_combined_box"].hide();
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if (getprop("/it-fbw/law") == 2) {
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me["FMA_ctr_msg"].setText("USE MAN PITCH TRIM");
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me["FMA_ctr_msg"].setColor(0.7333,0.3803,0);
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me["FMA_Middle1"].hide();
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me["FMA_Middle2"].show();
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me["FMA_ctr_msg"].show();
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} else if (getprop("/it-fbw/law") == 3) {
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me["FMA_ctr_msg"].setText("MAN PITCH TRIM ONLY");
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me["FMA_ctr_msg"].setColor(1,0,0);
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me["FMA_Middle1"].hide();
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me["FMA_Middle2"].show();
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me["FMA_ctr_msg"].show();
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} else {
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me["FMA_ctr_msg"].hide();
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me["FMA_Middle1"].show();
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me["FMA_Middle2"].hide();
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}
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if (ap1 or ap2 or fd1 or fd2) {
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me["FMA_pitch"].show();
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me["FMA_roll"].show();
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} else {
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me["FMA_pitch"].hide();
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me["FMA_roll"].hide();
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}
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if (getprop("/modes/pfd/fma/pitch-mode-box") == 1 and pitch_mode != " " and (ap1 or ap2 or fd1 or fd2)) {
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me["FMA_pitch_box"].show();
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} else {
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me["FMA_pitch_box"].hide();
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}
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if (pitch_mode_armed == " " and pitch_mode2_armed == " ") {
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me["FMA_pitcharm_box"].hide();
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} else {
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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)) {
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me["FMA_pitcharm_box"].show();
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} else {
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me["FMA_pitcharm_box"].hide();
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}
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}
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if (getprop("/modes/pfd/fma/roll-mode-box") == 1 and roll_mode != " " and (ap1 or ap2 or fd1 or fd2)) {
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me["FMA_roll_box"].show();
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} else {
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me["FMA_roll_box"].hide();
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}
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if (getprop("/modes/pfd/fma/roll-mode-armed-box") == 1 and roll_mode_armed != " " and (ap1 or ap2 or fd1 or fd2)) {
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me["FMA_rollarm_box"].show();
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} else {
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me["FMA_rollarm_box"].hide();
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}
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}
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if (ap1 or ap2 or fd1 or fd2) {
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me["FMA_pitcharm"].show();
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me["FMA_pitcharm2"].show();
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me["FMA_rollarm"].show();
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} else {
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me["FMA_pitcharm"].hide();
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me["FMA_pitcharm2"].hide();
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me["FMA_rollarm"].hide();
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}
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# FMA Pitch
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me["FMA_pitch"].setText(sprintf("%s", pitch_mode));
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me["FMA_pitcharm"].setText(sprintf("%s", pitch_mode_armed));
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me["FMA_pitcharm2"].setText(sprintf("%s", pitch_mode2_armed));
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# FMA Roll
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me["FMA_roll"].setText(sprintf("%s", roll_mode));
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me["FMA_rollarm"].setText(sprintf("%s", roll_mode_armed));
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# FMA CAT DH
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me["FMA_catmode"].hide();
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me["FMA_cattype"].hide();
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me["FMA_catmode_box"].hide();
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me["FMA_cattype_box"].hide();
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me["FMA_cat_box"].hide();
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me["FMA_nodh"].hide();
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me["FMA_dh_box"].hide();
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# FMA AP FD ATHR
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me["FMA_ap"].setText(sprintf("%s", getprop("/modes/pfd/fma/ap-mode")));
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me["FMA_fd"].setText(sprintf("%s", getprop("/modes/pfd/fma/fd-mode")));
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me["FMA_athr"].setText(sprintf("%s", getprop("/modes/pfd/fma/at-mode")));
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if ((state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL")) {
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me["FMA_athr"].setColor(0.8078,0.8039,0.8078);
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} else {
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me["FMA_athr"].setColor(0.0862,0.5176,0.6470);
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}
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if (getprop("/modes/pfd/fma/ap-mode-box") == 1 and getprop("/modes/pfd/fma/ap-mode") != " ") {
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me["FMA_ap_box"].show();
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} else {
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me["FMA_ap_box"].hide();
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}
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if (getprop("/modes/pfd/fma/fd-mode-box") == 1 and getprop("/modes/pfd/fma/fd-mode") != " ") {
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me["FMA_fd_box"].show();
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} else {
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me["FMA_fd_box"].hide();
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}
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if (getprop("/modes/pfd/fma/athr-mode-box") == 1 and getprop("/modes/pfd/fma/at-mode") != " ") {
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me["FMA_athr_box"].show();
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} else {
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me["FMA_athr_box"].hide();
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}
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# Airspeed
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# Subtract 30, since the scale starts at 30, but don't allow less than 0, or more than 420 situations
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if (getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") <= 30) {
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ASI = 0;
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} else if (getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") >= 420) {
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ASI = 390;
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} else {
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ASI = getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") - 30;
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}
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me["ASI_scale"].setTranslation(0, ASI * 6.6);
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if (getprop("/instrumentation/airspeed-indicator/indicated-mach") >= 0.5) {
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me["ASI_mach_decimal"].show();
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me["ASI_mach"].show();
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} else {
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me["ASI_mach_decimal"].hide();
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me["ASI_mach"].hide();
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}
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if (getprop("/instrumentation/airspeed-indicator/indicated-mach") >= 0.999) {
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me["ASI_mach"].setText("999");
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} else {
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me["ASI_mach"].setText(sprintf("%3.0f", getprop("/instrumentation/airspeed-indicator/indicated-mach") * 1000));
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}
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if (getprop("/it-autoflight/input/spd-managed") == 1) {
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me["ASI_target"].setColor(0.6901,0.3333,0.7450);
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} else {
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me["ASI_target"].setColor(0.0862,0.5176,0.6470);
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}
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if (getprop("/FMGC/internal/target-ias-pfd") <= 30) {
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ASItrgt = 0 - ASI;
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} else if (getprop("/FMGC/internal/target-ias-pfd") >= 420) {
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ASItrgt = 390 - ASI;
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} else {
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ASItrgt = getprop("/FMGC/internal/target-ias-pfd") - 30 - ASI;
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}
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me["ASI_target"].setTranslation(0, ASItrgt * -6.6);
|
|
|
|
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 (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();
|
|
}
|
|
|
|
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["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);
|
|
|
|
# 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("%s", "0" ~ getprop("/it-autoflight/internal/vert-speed-fpm-pfd")));
|
|
} else {
|
|
me["VS_digit"].setText(sprintf("%s", getprop("/it-autoflight/internal/vert-speed-fpm-pfd")));
|
|
}
|
|
|
|
# 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) {
|
|
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) {
|
|
me["GS_pointer"].show();
|
|
} else {
|
|
me["GS_pointer"].hide();
|
|
}
|
|
|
|
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
|
|
# if (getprop("/it-autoflight/custom/show-hdg") == 1) {
|
|
# me["HDG_target"].show();
|
|
# } else {
|
|
me["HDG_target"].hide();
|
|
# }
|
|
},
|
|
};
|
|
|
|
setprop("/testing", 0); # REMOVE WHEN PFD FINISHED
|
|
|
|
setlistener("sim/signals/fdm-initialized", func {
|
|
PFD_display = canvas.new({
|
|
"name": "PFD",
|
|
"size": [1024, 1024],
|
|
"view": [1024, 1024],
|
|
"mipmapping": 1
|
|
});
|
|
PFD_display.addPlacement({"node": "pfd1.screen"});
|
|
var group_pfd1 = PFD_display.createGroup();
|
|
|
|
PFD_1 = canvas_PFD_1.new(group_pfd1, "Aircraft/IDG-A32X/Models/Instruments/PFD-WIP/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(PFD_display);
|
|
}
|