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IESI: transition to props.nas

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This commit is contained in:
Jonathan Redpath 2018-09-08 17:27:16 +01:00
parent 3764d88a88
commit 9c0a45045d
1 changed files with 57 additions and 35 deletions
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92
Models/Instruments/IESI/IESI.nas
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@ -11,8 +11,29 @@ var elapsedtime = 0;
var ASI = 0;
var alt = 0;
var altTens = 0;
var pitch = 0;
var roll = 0;
# props.nas nodes
var iesi_init = props.globals.initNode("/instrumentation/iesi/iesi-init", 0, "BOOL");
var iesi_time = props.globals.initNode("/instrumentation/iesi/iesi-init-time", 0.0, "DOUBLE");
var iesi_rate = props.globals.getNode("/systems/acconfig/options/iesi-rate");
var et = props.globals.getNode("/sim/time/elapsed-sec");
var aconfig = props.globals.getNode("/systems/acconfig/autoconfig-running");
var dcbat = props.globals.getNode("/systems/electrical/bus/dcbat");
var dc1 = props.globals.getNode("/systems/electrical/bus/dc1");
var dc2 = props.globals.getNode("/systems/electrical/bus/dc2");
var airspeed = props.globals.getNode("/instrumentation/airspeed-indicator/indicated-speed-kt");
var mach = props.globals.getNode("/instrumentation/airspeed-indicator/indicated-mach");
var pitch = props.globals.getNode("/orientation/pitch-deg");
var roll = props.globals.getNode("/orientation/roll-deg");
var skid = props.globals.getNode("/instrumentation/slip-skid-ball/indicated-slip-skid");
var altitude = props.globals.getNode("/instrumentation/altimeter/indicated-altitude-ft");
var altitude_ind = props.globals.getNode("/instrumentation/altimeter/indicated-altitude-ft-pfd");
var altimeter_mode = props.globals.getNode("/modes/altimeter/std");
var qnh_hpa = props.globals.getNode("/instrumentation/altimeter/setting-hpa");
var qnh_inhg = props.globals.getNode("/instrumentation/altimeter/setting-inhg");
var canvas_IESI_base = {
init: func(canvas_group, file) {
@ -58,19 +79,24 @@ var canvas_IESI_base = {
return [];
},
update: func() {
if (getprop("/systems/electrical/bus/dcbat") >= 25 or getprop("/systems/electrical/bus/dc1") >= 25 or getprop("/systems/electrical/bus/dc2") >= 25) {
if (getprop("/systems/acconfig/autoconfig-running") != 1 and getprop("/instrumentation/iesi/iesi-init") != 1) {
setprop("/instrumentation/iesi/iesi-init", 1);
setprop("/instrumentation/iesi/iesi-init-time", getprop("/sim/time/elapsed-sec"));
} else if (getprop("/systems/acconfig/autoconfig-running") == 1 and getprop("/instrumentation/iesi/iesi-init") != 1) {
setprop("/instrumentation/iesi/iesi-init", 1);
setprop("/instrumentation/iesi/iesi-init-time", getprop("/sim/time/elapsed-sec") - 87);
if (dcbat.getValue() >= 25 or dc1.getValue() >= 25 or dc2.getValue() >= 25) {
IESI.page.show();
IESI.update();
if (aconfig.getValue() != 1 and iesi_init.getValue() != 1) {
iesi_init.setBoolValue(1);
cur_time = et.getValue();
iesi_time.setValue(cur_time);
} else if (aconfig.getValue() == 1 and iesi_init.getValue() != 1) {
iesi_init.setBoolValue(1);
cur_time = et.getValue() - 87;
iesi_time.setValue(cur_time);
}
} else {
setprop("/instrumentation/iesi/iesi-init", 0);
iesi_init.setBoolValue(0);
}
if (getprop("/systems/electrical/bus/dcbat") >= 25 or getprop("/systems/electrical/bus/dc1") >= 25 or getprop("/systems/electrical/bus/dc2") >= 25) {
if (dcbat.getValue() >= 25 or dc1.getValue() >= 25 or dc2.getValue() >= 25) {
IESI.page.show();
IESI.update();
} else {
@ -90,8 +116,7 @@ var canvas_IESI = {
return ["IESI","IESI_Init","ASI_scale","ASI_mach","ASI_mach_decimal","AI_center","AI_horizon","AI_bank","AI_slipskid","ALT_scale","ALT_one","ALT_two","ALT_three","ALT_four","ALT_five","ALT_digits","ALT_tens","ALT_meters","QNH_setting","QNH_std"];
},
update: func() {
elapsedtime = getprop("/sim/time/elapsed-sec");
if (getprop("/instrumentation/iesi/iesi-init-time") + 90 >= elapsedtime) {
if (iesi_time.getValue() + 90 >= et.getValue()) {
me["IESI"].hide();
me["IESI_Init"].show();
} else {
@ -101,16 +126,16 @@ var canvas_IESI = {
# 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) {
if (airspeed.getValue() <= 30) {
ASI = 0;
} else if (getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") >= 420) {
} else if (airspeed.getValue() >= 420) {
ASI = 390;
} else {
ASI = getprop("/instrumentation/airspeed-indicator/indicated-speed-kt") - 30;
ASI = airspeed.getValue() - 30;
}
me["ASI_scale"].setTranslation(0, ASI * 8.295);
if (getprop("/instrumentation/airspeed-indicator/indicated-mach") >= 0.5) {
if (mach.getValue() >= 0.5) {
me["ASI_mach_decimal"].show();
me["ASI_mach"].show();
} else {
@ -118,26 +143,23 @@ var canvas_IESI = {
me["ASI_mach"].hide();
}
if (getprop("/instrumentation/airspeed-indicator/indicated-mach") >= 0.999) {
if (mach.getValue() >= 0.999) {
me["ASI_mach"].setText("99");
} else {
me["ASI_mach"].setText(sprintf("%2.0f", getprop("/instrumentation/airspeed-indicator/indicated-mach") * 100));
me["ASI_mach"].setText(sprintf("%2.0f", mach.getValue() * 100));
}
# Attitude
pitch = getprop("/orientation/pitch-deg") or 0;
roll = getprop("/orientation/roll-deg") or 0;
me.AI_horizon_trans.setTranslation(0, pitch * 16.74);
me.AI_horizon_rot.setRotation(-roll * D2R, me["AI_center"].getCenter());
me.AI_horizon_trans.setTranslation(0, pitch.getValue() * 16.74);
me.AI_horizon_rot.setRotation(-roll.getValue() * 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);
me["AI_slipskid"].setTranslation(math.clamp(skid.getValue(), -7, 7) * -15, 0);
me["AI_bank"].setRotation(-roll.getValue() * D2R);
# 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.altOffset = altitude.getValue() / 500 - int(altitude.getValue() / 500);
me.middleAltText = roundaboutAlt(altitude.getValue() / 100);
me.middleAltOffset = nil;
if (me.altOffset > 0.5) {
me.middleAltOffset = -(me.altOffset - 1) * 258.5528;
@ -152,17 +174,17 @@ var canvas_IESI = {
me["ALT_two"].setText(sprintf("%03d", abs(me.middleAltText-5)));
me["ALT_one"].setText(sprintf("%03d", abs(me.middleAltText-10)));
me["ALT_digits"].setText(sprintf("%s", getprop("/instrumentation/altimeter/indicated-altitude-ft-pfd")));
me["ALT_meters"].setText(sprintf("%5.0f", getprop("/instrumentation/altimeter/indicated-altitude-ft") * 0.3048));
altTens = num(right(sprintf("%02d", getprop("/instrumentation/altimeter/indicated-altitude-ft")), 2));
me["ALT_digits"].setText(sprintf("%s", altitude_ind.getValue()));
me["ALT_meters"].setText(sprintf("%5.0f", altitude.getValue() * 0.3048));
altTens = num(right(sprintf("%02d", altitude_ind.getValue()), 2));
me["ALT_tens"].setTranslation(0, altTens * 3.16);
# QNH
if (getprop("/modes/altimeter/std") == 1) {
if (altimeter_mode.getValue() == 1) {
me["QNH_setting"].hide();
me["QNH_std"].show();
} else {
me["QNH_setting"].setText(sprintf("%4.0f", getprop("/instrumentation/altimeter/setting-hpa")) ~ "/" ~ sprintf("%2.2f", getprop("/instrumentation/altimeter/setting-inhg")));
me["QNH_setting"].setText(sprintf("%4.0f", qnh_hpa.getValue()) ~ "/" ~ sprintf("%2.2f", qnh_inhg.getValue()));
me["QNH_setting"].show();
me["QNH_std"].hide();
}
@ -182,13 +204,13 @@ setlistener("sim/signals/fdm-initialized", func {
IESI = canvas_IESI.new(group_IESI, "Aircraft/IDG-A32X/Models/Instruments/IESI/res/iesi.svg");
IESI_update.start();
if (getprop("/systems/acconfig/options/iesi-rate") > 1) {
if (iesi_rate.getValue() > 1) {
rateApply();
}
});
var rateApply = func {
IESI_update.restart(0.07 * getprop("/systems/acconfig/options/iesi-rate"));
IESI_update.restart(0.07 * iesi_rate.getValue());
}
var IESI_update = maketimer(0.07, func {