# A3XX PFD # Joshua Davidson (it0uchpods) ############################################## # Copyright (c) Joshua Davidson (it0uchpods) # ############################################## var PFD_1 = nil; var PFD_2 = nil; var PFD_1_test = nil; var PFD_2_test = nil; var PFD1_display = nil; var PFD2_display = nil; var elapsedtime = 0; var ASI = 0; var ASItrgt = 0; var ASItrgtdiff = 0; var ASImax = 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; 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("/instrumentation/du/du1-test", 0); setprop("/instrumentation/du/du1-test-time", 0); setprop("/instrumentation/du/du6-test", 0); setprop("/instrumentation/du/du6-test-time", 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); setprop("/instrumentation/adirs/adr[0]/active", 0); setprop("/instrumentation/adirs/adr[1]/active", 0); setprop("/instrumentation/adirs/adr[2]/active", 0); setprop("/instrumentation/adirs/ir[0]/aligned", 0); setprop("/instrumentation/adirs/ir[1]/aligned", 0); setprop("/instrumentation/adirs/ir[2]/aligned", 0); setprop("/controls/switching/ATTHDG", 0); setprop("/controls/switching/AIRDATA", 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.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(); me.page = canvas_group; return me; }, 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_max","ASI_scale","ASI_target","ASI_mach","ASI_mach_decimal","ASI_ten_sec","ASI_digit_UP","ASI_digit_DN","ASI_decimal_UP","ASI_decimal_DN","ASI_index","ASI_error","ASI_group","ASI_frame","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","AI_error","AI_group","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","ALT_error","ALT_group","ALT_group2","ALT_frame","VS_pointer","VS_box","VS_digit","VS_error","VS_group","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","HDG_error","HDG_group","HDG_frame","TRK_pointer"]; }, update: func() { elapsedtime = getprop("/sim/time/elapsed-sec"); if (getprop("/systems/electrical/bus/ac1") >= 110 or getprop("/systems/electrical/bus/ac2") >= 110) { if (getprop("/systems/acconfig/autoconfig-running") != 1 and getprop("/instrumentation/du/du1-test") != 1) { setprop("/instrumentation/du/du1-test", 1); setprop("/instrumentation/du/du1-test-time", getprop("/sim/time/elapsed-sec")); } else if (getprop("/systems/acconfig/autoconfig-running") == 1 and getprop("/instrumentation/du/du1-test") != 1) { setprop("/instrumentation/du/du1-test", 1); setprop("/instrumentation/du/du1-test-time", getprop("/sim/time/elapsed-sec") - 35); } } else { setprop("/instrumentation/du/du1-test", 0); } if (getprop("/systems/electrical/bus/ac1") >= 110 and getprop("/systems/electrical/bus/ac2") >= 110) { if (getprop("/systems/acconfig/autoconfig-running") != 1 and getprop("/instrumentation/du/du6-test") != 1) { setprop("/instrumentation/du/du6-test", 1); setprop("/instrumentation/du/du6-test-time", getprop("/sim/time/elapsed-sec")); } else if (getprop("/systems/acconfig/autoconfig-running") == 1 and getprop("/instrumentation/du/du6-test") != 1) { setprop("/instrumentation/du/du6-test", 1); setprop("/instrumentation/du/du6-test-time", getprop("/sim/time/elapsed-sec") - 35); } } else { setprop("/instrumentation/du/du6-test", 0); } if ((getprop("/systems/electrical/bus/ac1") >= 110 or getprop("/systems/electrical/bus/ac2") >= 110) and getprop("/controls/lighting/DU/du1") > 0) { if (getprop("/instrumentation/du/du1-test-time") + 39.5 >= elapsedtime and getprop("/modes/cpt-du-xfr") != 1) { PFD_1.page.hide(); PFD_1_test.page.show(); } else if (getprop("/instrumentation/du/du2-test-time") + 38.5 >= elapsedtime and getprop("/modes/cpt-du-xfr") == 1) { PFD_1.page.hide(); PFD_1_test.page.show(); } else { PFD_1_test.page.hide(); PFD_1.page.show(); PFD_1.update(); } } else { PFD_1_test.page.hide(); 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) { if (getprop("/instrumentation/du/du6-test-time") + 39.5 >= elapsedtime and getprop("/modes/fo-du-xfr") != 1) { PFD_2.page.hide(); PFD_2_test.page.show(); } else if (getprop("/instrumentation/du/du5-test-time") + 38.5 >= elapsedtime and getprop("/modes/fo-du-xfr") == 1) { PFD_2.page.hide(); PFD_2_test.page.show(); } else { PFD_2_test.page.hide(); PFD_2.page.show(); PFD_2.update(); } } else { PFD_2_test.page.hide(); 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") and getprop("/systems/thrust/eng-out") != 1) { 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 if (athr == 1 and (state1 == "TOGA" or (state1 == "MCT" and getprop("/controls/engines/thrust-limit") == "FLX") or (state1 == "MAN THR" and thr1 >= 0.83) or state2 == "TOGA" or (state2 == "MCT" and getprop("/controls/engines/thrust-limit") == "FLX") or (state2 == "MAN THR" and thr2 >= 0.83)) and getprop("/systems/thrust/eng-out") == 1) { 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_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 { me["FMA_man"].hide(); me["FMA_manmode"].hide(); me["FMA_man_box"].hide(); me["FMA_flx_box"].hide(); me["FMA_flxtemp"].hide(); } if (getprop("/systems/thrust/eng-out") == 1) { me["FMA_lvrclb"].setText("LVR MCT"); } else { me["FMA_lvrclb"].setText("LVR CLB"); } 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 getprop("/systems/thrust/eng-out") != 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 if (athr == 1 and getprop("/systems/thrust/eng-out") == 1 and (state1 == "MAN" or state1 == "CL" or (state1 == "MAN THR" and thr1 < 0.83) or (state1 == "MCT" and getprop("/controls/engines/thrust-limit") != "FLX")) and (state2 == "MAN" or state2 == "CL" or (state2 == "MAN THR" and thr2 < 0.83) or (state2 == "MCT" and getprop("/controls/engines/thrust-limit") != "FLX"))) { 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 (getprop("/modes/pfd/fma/athr-armed") != 1) { 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; } if (getprop("/FMGC/internal/maxspeed") <= 30) { ASImax = 0 - ASI; } else if (getprop("/FMGC/internal/maxspeed") >= 420) { ASImax = 390 - ASI; } else { ASImax = getprop("/FMGC/internal/maxspeed") - 30 - ASI; } me["ASI_scale"].setTranslation(0, ASI * 6.6); me["ASI_max"].setTranslation(0, ASImax * -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(math.clamp(getprop("/instrumentation/slip-skid-ball/indicated-slip-skid"), -7, 7) * -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; }, 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"); # Errors if ((getprop("/instrumentation/adirs/adr[0]/active") == 1) or (getprop("/controls/switching/AIRDATA") == -1 and getprop("/instrumentation/adirs/adr[2]/active") == 1)) { me["ASI_group"].show(); me["ALT_group"].show(); me["ALT_group2"].show(); me["ALT_scale"].show(); me["VS_group"].show(); me["ASI_error"].hide(); me["ASI_frame"].setColor(1,1,1); me["ALT_error"].hide(); me["ALT_frame"].setColor(1,1,1); me["VS_error"].hide(); } else { me["ASI_error"].show(); me["ASI_frame"].setColor(1,0,0); me["ALT_error"].show(); me["ALT_frame"].setColor(1,0,0); me["VS_error"].show(); me["ASI_group"].hide(); me["ALT_group"].hide(); me["ALT_group2"].hide(); me["ALT_scale"].hide(); me["VS_group"].hide(); } if ((getprop("/instrumentation/adirs/ir[0]/aligned") == 1) or (getprop("/instrumentation/adirs/ir[2]/aligned") == 1 and getprop("/controls/switching/ATTHDG") == -1)) { me["AI_group"].show(); me["HDG_group"].show(); me["AI_error"].hide(); me["HDG_error"].hide(); me["HDG_frame"].setColor(1,1,1); } else { me["AI_error"].show(); me["HDG_error"].show(); me["HDG_frame"].setColor(1,0,0); me["AI_group"].hide(); me["HDG_group"].hide(); } # 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; }, 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"); # Errors if ((getprop("/instrumentation/adirs/adr[1]/active") == 1) or (getprop("/controls/switching/AIRDATA") == 1 and getprop("/instrumentation/adirs/adr[2]/active") == 1)) { me["ASI_group"].show(); me["ALT_group"].show(); me["ALT_group2"].show(); me["ALT_scale"].show(); me["VS_group"].show(); me["ASI_error"].hide(); me["ASI_frame"].setColor(1,1,1); me["ALT_error"].hide(); me["ALT_frame"].setColor(1,1,1); me["VS_error"].hide(); } else { me["ASI_error"].show(); me["ASI_frame"].setColor(1,0,0); me["ALT_error"].show(); me["ALT_frame"].setColor(1,0,0); me["VS_error"].show(); me["ASI_group"].hide(); me["ALT_group"].hide(); me["ALT_group2"].hide(); me["ALT_scale"].hide(); me["VS_group"].hide(); } if ((getprop("/instrumentation/adirs/ir[1]/aligned") == 1) or (getprop("/instrumentation/adirs/ir[2]/aligned") == 1 and getprop("/controls/switching/ATTHDG") == 1)) { me["AI_group"].show(); me["HDG_group"].show(); me["AI_error"].hide(); me["HDG_error"].hide(); me["HDG_frame"].setColor(1,1,1); } else { me["AI_error"].show(); me["HDG_error"].show(); me["HDG_frame"].setColor(1,0,0); me["AI_group"].hide(); me["HDG_group"].hide(); } # 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(); }, }; var canvas_PFD_1_test = { 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}); me.page = canvas_group; return me; }, new: func(canvas_group, file) { var m = {parents: [canvas_PFD_1_test]}; m.init(canvas_group, file); return m; }, }; var canvas_PFD_2_test = { 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}); me.page = canvas_group; return me; }, new: func(canvas_group, file) { var m = {parents: [canvas_PFD_2_test]}; m.init(canvas_group, file); return m; }, }; 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_pfd1_test = PFD1_display.createGroup(); var group_pfd2 = PFD2_display.createGroup(); var group_pfd2_test = PFD2_display.createGroup(); PFD_1 = canvas_PFD_1.new(group_pfd1, "Aircraft/IDG-A32X/Models/Instruments/PFD/res/pfd.svg"); PFD_1_test = canvas_PFD_1_test.new(group_pfd1_test, "Aircraft/IDG-A32X/Models/Instruments/Common/res/du-test.svg"); PFD_2 = canvas_PFD_2.new(group_pfd2, "Aircraft/IDG-A32X/Models/Instruments/PFD/res/pfd.svg"); PFD_2_test = canvas_PFD_2_test.new(group_pfd2_test, "Aircraft/IDG-A32X/Models/Instruments/Common/res/du-test.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; } };