Merge branch 'master' of git://gitorious.org/fg/fgdata
This commit is contained in:
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commit
0b496c3708
140 changed files with 86209 additions and 120 deletions
51
Nasal/casdisable.nas
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51
Nasal/casdisable.nas
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@ -0,0 +1,51 @@
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#disable cas when engines running- otherwise we are overflooded with error messages in the console
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call_casdisable = func {
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if ( getprop("/rotors/main/rpm")> 80.0)
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{
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setprop("/controls/flight/fcs/cas-enabled", 0);
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} else {
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setprop("/controls/flight/fcs/cas-enabled", 1.0);
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}
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#if (RUN2 ==1) {
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# setprop("/controls/flight/fcs/cas-enabled", 0);
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# } else {
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# setprop("/controls/flight/fcs/cas-enabled", 1.0);
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# }
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settimer(call_casdisable, 0.2);
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}
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init = func {
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settimer(call_casdisable, 0.0);
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}
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init();
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571
Nasal/fcs.nas
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571
Nasal/fcs.nas
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#
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# Flight Control System by Tatsuhiro Nishioka
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# $Id: fcs.nas,v 1.11 2008/08/28 02:41:04 tat Exp $
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#
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#This one simulates a jaw SAS
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var FCSFilter = {
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new : func(input_path, output_path) {
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var obj = { parents : [FCSFilter],
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input_path : input_path,
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output_path : output_path };
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obj.axis_conv = {'roll' : 'aileron', 'pitch' : 'elevator', 'yaw' : 'rudder' };
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obj.body_conv = {'roll' : 'v', 'pitch' : 'u' };
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obj.last_body_fps = {'roll' : 0.0, 'pitch' : 0.0 };
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obj.last_pos = {'roll' : 0.0, 'pitch' : 0.0, 'yaw' : 0.0};
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return obj;
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},
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# read input command for a given axis
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read : func(axis) {
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if (me.input_path == nil or me.input_path == "") {
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return getprop("/controls/flight/" ~ me.axis_conv[axis]);
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} else {
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var value = getprop(me.input_path ~ "/" ~ axis);
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value = int(value * 1000) / 1000.0;
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}
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},
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# write output command for a given axis
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# this will be the output of an next command filter (like SAS)
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write : func(axis, value) {
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if (me.output_path == nil or me.output_path == '') {
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setprop("/controls/flight/fcs/" ~ axis, me.limit(value, 1.0));
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} else {
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setprop(me.output_path ~ "/" ~ axis, me.limit(value, 1.0));
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}
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},
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toggleFilterStatus : func(name) {
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var messages = ["disengaged", "engaged"];
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var path = "/controls/flight/fcs/" ~ name ~ "-enabled";
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var status = getprop(path);
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setprop(path, 1 - status);
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screen.log.write(name ~ " " ~ messages[1 - status]);
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},
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getStatus : func(name) {
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var path = "/controls/flight/fcs/" ~ name ~ "-enabled";
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return getprop(path);
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},
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limit : func(value, range) {
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if (value > range) {
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return range;
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} elsif (value < -range) {
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return - range;
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}
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return value;
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},
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max : func(val1, val2) {
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return (val1 > val2) ? val1 : val2;
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},
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min : func(val1, val2) {
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return (val1 > val2) ? val2 : val1;
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},
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calcCounterBodyFPS : func(axis, input, offset_deg) {
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var position = getprop("/orientation/" ~ axis ~ "-deg");
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var body_fps = 0;
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var last_body_fps = me.last_body_fps[axis];
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var reaction_gain = 0;
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var heading = getprop("/orientation/heading-deg");
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var wind_speed_fps = getprop("/environment/wind-speed-kt") * 1.6878099;
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var wind_direction = getprop("/environment/wind-from-heading-deg");
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var wind_direction -= heading;
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var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
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var gear_pos = getprop("/gear/gear[0]/compression-norm") + getprop("/gear/gear[1]/compression-norm");
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var counter_fps = 0;
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var fps_axis = me.body_conv[axis]; # convert from {roll, pitch} to {u, v}
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var target_pos = offset_deg;
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var brake_deg = 0;
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body_fps = getprop("/velocities/" ~ fps_axis ~ "Body-fps");
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if (axis == 'roll') {
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var wind_fps = math.sin(wind_direction / 180 * math.pi) * wind_speed_fps;
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} else {
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var wind_fps = math.cos(wind_direction / 180 * math.pi) * wind_speed_fps;
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}
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var brake_freq = getprop("/controls/flight/fcs/gains/afcs/fps-" ~ axis ~ "-brake-freq");
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var brake_gain = getprop("/controls/flight/fcs/gains/afcs/fps-brake-gain-" ~ axis);
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body_fps -= wind_fps;
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var dfps = body_fps - me.last_body_fps[axis];
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var fps_coeff = getprop("/controls/flight/fcs/gains/afcs/fps-" ~ axis ~ "-coeff");
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target_pos -= int(body_fps * 100) / 100 * fps_coeff;
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if (axis == 'roll' and gear_pos > 0.0 and position > 0) {
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target_pos -= position * gear_pos / 5;
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}
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reaction_gain = getprop("/controls/flight/fcs/gains/afcs/fps-reaction-gain-" ~ axis);
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var brake_sensitivity = (axis == 'roll') ? 1 : 1;
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if (math.abs(position + rate / brake_freq * brake_sensitivity) > math.abs(target_pos)) {
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if (math.abs(dfps) > 1) {
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dfps = 1;
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}
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var error_deg = target_pos - position;
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brake_deg = (error_deg - rate / brake_freq) * math.abs(dfps * 10) * brake_gain;
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if (target_pos > 0) {
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brake_deg = me.min(brake_deg, 0);
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} else {
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brake_deg = me.max(brake_deg, 0);
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}
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}
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counter_fps = me.limit((target_pos + brake_deg) * reaction_gain, 1.0);
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setprop("/controls/flight/fcs/afcs/ah-" ~ fps_axis ~ "body-fps", body_fps);
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setprop("/controls/flight/fcs/afcs/ah-" ~ fps_axis ~ "body-wind-fps", wind_fps);
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setprop("/controls/flight/fcs/afcs/ah-" ~ axis ~ "-target-deg", target_pos);
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setprop("/controls/flight/fcs/afcs/ah-" ~ axis ~ "-rate", rate);
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setprop("/controls/flight/fcs/afcs/ah-delta-" ~ fps_axis ~ "body-fps", dfps);
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setprop("/controls/flight/fcs/afcs/ah-" ~ axis ~ "-brake-deg", brake_deg);
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setprop("/controls/flight/fcs/afcs/counter-fps-" ~ axis, counter_fps);
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me.last_pos[axis] = position;
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me.last_body_fps[axis] = body_fps;
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return me.limit(counter_fps + input * 0.2, 1.0);
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},
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};
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#
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# AFCS : Automatic Flight Control System
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#
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var AFCS = {
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new : func(input_path, output_path) {
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var obj = FCSFilter.new(input_path, output_path);
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obj.parents = [FCSFilter, AFCS];
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setprop("/controls/flight/fcs/auto-hover-enabled", 0);
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setprop("/controls/flight/fcs/gains/afcs/fps-brake-gain-pitch", 1.8);
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setprop("/controls/flight/fcs/gains/afcs/fps-brake-gain-roll", 0.8);
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setprop("/controls/flight/fcs/gains/afcs/fps-pitch-brake-freq", 3);
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setprop("/controls/flight/fcs/gains/afcs/fps-pitch-coeff", -0.95);
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setprop("/controls/flight/fcs/gains/afcs/fps-pitch-offset-deg", 0.9);
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setprop("/controls/flight/fcs/gains/afcs/fps-reaction-gain-pitch", -0.8);
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setprop("/controls/flight/fcs/gains/afcs/fps-reaction-gain-roll", 0.3436);
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setprop("/controls/flight/fcs/gains/afcs/fps-roll-brake-freq", 8);
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setprop("/controls/flight/fcs/gains/afcs/fps-roll-coeff", 0.8);
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setprop("/controls/flight/fcs/gains/afcs/fps-roll-offset-deg", -0.8);
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return obj;
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},
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toggleAutoHover : func() {
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me.toggleFilterStatus("auto-hover");
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},
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toggleAirSpeedLock : func() {
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me.toggleFilterStatus("air-speed-lock");
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},
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toggleHeadingLock : func() {
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me.toggleFilterStatus("heading-lock");
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},
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toggleAltitudeLock : func() {
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me.toggleFilterStatus("altitude-lock");
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},
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#
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# auto hover : locks vBody_fps and uBody_fps regardless of wind speed/direction
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#
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autoHover : func(axis, input) {
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if (axis == 'yaw') {
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return input;
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} else {
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var offset_deg = getprop("/controls/flight/fcs/gains/afcs/fps-" ~ axis ~ "-offset-deg");
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return me.calcCounterBodyFPS(axis, input, offset_deg);
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}
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},
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altitudeLock : func(axis, input) {
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# not implemented yet
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return input;
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},
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headingLock : func(axis, input) {
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# not implementet yet
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return input;
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},
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apply : func(axis) {
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var input = me.read(axis);
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var hover_status = me.getStatus("auto-hover");
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if (hover_status == 0) {
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me.write(axis, input);
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return;
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}
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me.write(axis, me.autoHover(axis, input));
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}
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};
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#
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# SAS : Stability Augmentation System - a rate damper
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#
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var SAS = {
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#
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# new
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# initial_gains: hash of initial gains for rate damping
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# sensitivities: hash of minimum rates (deg/sec) that enables rate damper
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# authority_limit: shows how much SAS can take over control
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# 0 means no stability control, 1.0 means SAS fully takes over pilot control
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# input_path: is a base path to input axis; nil for using raw input from KB/JS
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# output_path: is a base path to output axis; nis for using /controls/flight/fcs
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#
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# with input_path / output_path, you can connect SAS, CAS, and more control filters
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#
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new : func(initial_gains, sensitivities, authority_limit, input_path, output_path) {
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var obj = FCSFilter.new(input_path, output_path);
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obj.parents = [FCSFilter, SAS];
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obj.authority_limit = authority_limit;
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obj.sensitivities = sensitivities;
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obj.initial_gains = initial_gains;
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props.globals.getNode("/controls/flight/fcs/gains/sas", 1).setValues(obj.initial_gains);
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setprop("/controls/flight/fcs/sas-enabled", 1);
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return obj;
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},
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toggleEnable : func() {
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me.toggleFilterStatus("sas");
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},
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#
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# calcGain - get gain for each axis based on air speed and dynamic pressure
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# axis: one of 'roll', 'pitch', or 'yaw'
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#
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calcGain : func(axis) {
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var mach = getprop("/velocities/mach");
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var initial_gain = getprop("/controls/flight/fcs/gains/sas/" ~ axis);
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var gain = initial_gain - 0.1 * mach * mach;
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if (math.abs(gain) < math.abs(initial_gain) * 0.01 or gain * initial_gain < 0) {
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gain = initial_gain * 0.01;
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}
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return gain;
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},
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calcAuthorityLimit : func() {
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var mach = getprop("/velocities/mach");
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var min_mach = 0.038;
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var limit = me.authority_limit;
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if (math.abs(mach < min_mach)) {
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limit += (min_mach - math.abs(mach)) / min_mach * (1 - me.authority_limit) * 0.95;
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}
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setprop("/controls/flight/fcs/gains/sas/authority-limit", limit);
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return limit;
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},
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#
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# apply - apply SAS damper to a given input axis
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# axis: one of 'roll', 'pitch', or 'yaw'
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#
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apply : func(axis) {
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var status = me.getStatus("sas");
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var input = me.read(axis);
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if (status == 0) {
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me.write(axis, input);
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return;
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}
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var mach = getprop("/velocities/mach");
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var value = 0;
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var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
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var gain = me.calcGain(axis);
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var limit = me.calcAuthorityLimit();
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if (math.abs(rate) >= me.sensitivities[axis]) {
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value = - gain * rate;
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if (value > limit) {
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value = limit;
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} elsif (value < - limit) {
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value = - limit;
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}
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}
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me.write(axis, value + input);
|
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}
|
||||
};
|
||||
|
||||
#
|
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# CAS : Control Augmentation System - makes your aircraft more meneuverable
|
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#
|
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var CAS = {
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new : func(input_gains, output_gains, sensitivities, input_path, output_path) {
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var obj = FCSFilter.new(input_path, output_path);
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obj.parents = [FCSFilter, CAS];
|
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obj.sensitivities = sensitivities;
|
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obj.input_gains = input_gains;
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obj.output_gains = output_gains;
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props.globals.getNode("/controls/flight/fcs/gains/cas/input", 1).setValues(obj.input_gains);
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props.globals.getNode("/controls/flight/fcs/gains/cas/output", 1).setValues(obj.output_gains);
|
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setprop("/autopilot/locks/altitude", '');
|
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setprop("/autopilot/locks/heading", '');
|
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setprop("/controls/flight/fcs/cas-enabled", 1);
|
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return obj;
|
||||
},
|
||||
|
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calcRollRateAdjustment : func {
|
||||
var position = getprop("/orientation/roll-deg");
|
||||
return math.abs(math.sin(position / 180 * math.pi)) / 6;
|
||||
},
|
||||
|
||||
calcSideSlipAdjustment : func {
|
||||
var mach = getprop("/velocities/mach");
|
||||
var slip = getprop("/orientation/side-slip-deg");
|
||||
if (mach < 0.015) { # works only if air speed > 10kt
|
||||
slip = 0;
|
||||
}
|
||||
var anti_slip_gain = getprop("/controls/flight/fcs/gains/cas/output/anti-side-slip-gain");
|
||||
var roll_deg = getprop("/orientation/roll-deg");
|
||||
var gain_adjuster = me.min(math.abs(mach) / 0.060, 1) * me.limit(0.2 + math.sqrt(math.abs(roll_deg)/10), 3);
|
||||
anti_slip_gain *= gain_adjuster;
|
||||
setprop("/controls/flight/fcs/cas/anti-side-slip", slip * anti_slip_gain);
|
||||
return slip * anti_slip_gain;
|
||||
},
|
||||
|
||||
# FIXME: command for CAS is just a temporal one
|
||||
calcCommand: func (axis, input) {
|
||||
var output = 0;
|
||||
var mach = getprop("/velocities/mach");
|
||||
var input_gain = me.calcGain(axis);
|
||||
var output_gain = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis);
|
||||
var target_rate = input * input_gain;
|
||||
var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
|
||||
var drate = target_rate - rate;
|
||||
var locks = {'pitch' : getprop("/autopilot/locks/altitude"),
|
||||
'roll' : getprop("/autopilot/locks/heading")};
|
||||
setprop("/controls/flight/fcs/cas/target_" ~ axis ~ "rate", target_rate);
|
||||
setprop("/controls/flight/fcs/cas/delta_" ~ axis, drate);
|
||||
|
||||
if (axis == 'roll' or axis == 'pitch') {
|
||||
if (math.abs(input > 0.7) or locks[axis] != '') {
|
||||
output = drate * output_gain;
|
||||
} else {
|
||||
output = me.calcAttitudeCommand(axis);
|
||||
}
|
||||
if (axis == 'roll' and math.abs(mach) < 0.035) {
|
||||
# FIXME: I don't know if OH-1 has this one
|
||||
output += me.calcCounterBodyFPS(axis, input, -0.8);
|
||||
}
|
||||
} elsif (axis == 'yaw') {
|
||||
output = drate * output_gain + me.calcSideSlipAdjustment();
|
||||
} else {
|
||||
output = drate * output_gain;
|
||||
}
|
||||
return output;
|
||||
},
|
||||
|
||||
toggleEnable : func() {
|
||||
me.toggleFilterStatus("cas");
|
||||
},
|
||||
|
||||
calcAttitudeCommand : func(axis) {
|
||||
var input_gain = getprop("/controls/flight/fcs/gains/cas/input/attitude-" ~ axis);
|
||||
var output_gain = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis);
|
||||
var brake_freq = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis ~ "-brake-freq");
|
||||
var brake_gain = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis ~ "-brake");
|
||||
var trim = getprop("/controls/flight/" ~ me.axis_conv[axis] ~ "-trim");
|
||||
|
||||
var current_deg = getprop("/orientation/" ~ axis ~ "-deg");
|
||||
var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
|
||||
var target_deg = (me.read(axis) + trim) * input_gain;
|
||||
var command_deg = 0;
|
||||
if (target_deg != 0) {
|
||||
command_deg = (0.094 * math.ln(math.abs(target_deg)) + 0.53) * target_deg;
|
||||
}
|
||||
|
||||
var error_deg = command_deg - current_deg;
|
||||
var brake_deg = (error_deg - rate / brake_freq) * math.abs(error_deg) * brake_gain;
|
||||
|
||||
if (command_deg > 0) {
|
||||
brake_deg = me.min(brake_deg, 0);
|
||||
} else {
|
||||
brake_deg = me.max(brake_deg, 0);
|
||||
}
|
||||
|
||||
var monitor_prefix = me.output_path ~ "/" ~ axis;
|
||||
setprop(monitor_prefix ~ "-target_deg", target_deg);
|
||||
setprop(monitor_prefix ~ "-error_deg", error_deg);
|
||||
setprop(monitor_prefix ~ "-brake_deg", brake_deg);
|
||||
setprop(monitor_prefix ~ "-deg", current_deg);
|
||||
setprop(monitor_prefix ~ "-rate", -rate);
|
||||
|
||||
return (error_deg + brake_deg) * output_gain;
|
||||
},
|
||||
|
||||
# FixMe: gain should be calculated using both speed and dynamic pressure
|
||||
calcGain : func(axis) {
|
||||
var mach = getprop("/velocities/mach");
|
||||
var input_gain = getprop("/controls/flight/fcs/gains/cas/input/" ~ axis);
|
||||
var gain = input_gain;
|
||||
if (axis == 'pitch') {
|
||||
gain += 0.1 * mach * mach;
|
||||
} elsif (axis== 'yaw') {
|
||||
gain *= ((1 - mach) * (1 - mach));
|
||||
}
|
||||
if (gain * input_gain < 0.0 ) {
|
||||
gain = 0;
|
||||
}
|
||||
return gain;
|
||||
},
|
||||
|
||||
apply : func(axis) {
|
||||
var input = me.read(axis);
|
||||
var status = me.getStatus("cas");
|
||||
var cas_command = 0;
|
||||
# FIXME : hmm, a bit nasty. CAS should be enabled even with auto-hover....
|
||||
if (status == 0 or (me.getStatus("auto-hover") == 1 and axis != 'yaw')) {
|
||||
me.write(axis, input);
|
||||
return;
|
||||
}
|
||||
cas_command = me.calcCommand(axis, input);
|
||||
me.write(axis, cas_command);
|
||||
}
|
||||
};
|
||||
|
||||
#
|
||||
# Tail hstab, "stabilator," for stabilize the nose
|
||||
#
|
||||
var Stabilator = {
|
||||
new : func() {
|
||||
var obj = { parents : [Stabilator] };
|
||||
setprop("/controls/flight/fcs/gains/stabilator", -1.8);
|
||||
setprop("/controls/flight/fcs/auto-stabilator", 1);
|
||||
# 0 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160, 170, 180, .....
|
||||
me.gainTable = [-0.9, -0.8, 0.1, -0.5, 0.0, 0.7, 0.8, 0.9, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 0.9, 0.8, 0.6, 0.4, 0.2, -1.0];
|
||||
return obj;
|
||||
},
|
||||
|
||||
toggleManual : func {
|
||||
var status = getprop("/controls/flight/fcs/auto-stabilator");
|
||||
getprop("/controls/flight/fcs/auto-stabilator", 1 - status);
|
||||
},
|
||||
|
||||
apply : func(delta) {
|
||||
setprop("/controls/flight/fcs/auto-stabilator", 0);
|
||||
var value = getprop("/controls/flight/fcs/stabilator");
|
||||
getprop("/controls/flight/fcs/stabilator", value + delta);
|
||||
},
|
||||
|
||||
calcPosition : func() {
|
||||
var speed = getprop("/velocities/mach") / 0.001497219; # in knot
|
||||
var index = int(math.abs(speed) / 10);
|
||||
if (index >= size(me.gainTable) - 1) {
|
||||
index = size(me.gainTable) - 2;
|
||||
}
|
||||
var mod = math.mod(int(math.abs(speed)), 10);
|
||||
var position = me.gainTable[index] * ((10 - mod) / 10) + me.gainTable[index-1] * (mod) / 10;
|
||||
if (speed < -20) {
|
||||
position = - position;
|
||||
}
|
||||
return position;
|
||||
},
|
||||
|
||||
update : func() {
|
||||
var status = getprop("/controls/flight/fcs/auto-stabilator");
|
||||
if (status == 0) {
|
||||
return;
|
||||
}
|
||||
var gain = getprop("/controls/flight/fcs/gains/stabilator");
|
||||
var mach = getprop("/velocities/mach");
|
||||
var throttle = getprop("/controls/flight/throttle");
|
||||
var stabilator_norm = 0;
|
||||
|
||||
stabilator_norm = me.calcPosition();
|
||||
setprop("/controls/flight/fcs/stabilator", stabilator_norm);
|
||||
}
|
||||
};
|
||||
|
||||
var TailRotorCollective = {
|
||||
new : func(minimum=0.10, maximum=1.0, low_limit=0.00011, high_limit=0.0035) {
|
||||
var obj = FCSFilter.new("/controls/engines/engine[1]", "/controls/flight/fcs/tail-rotor");
|
||||
obj.parents = [FCSFilter, TailRotorCollective];
|
||||
obj.adjuster = 0.0;
|
||||
setprop("/controls/flight/fcs/tail-rotor/src-minimum", minimum);
|
||||
setprop("/controls/flight/fcs/tail-rotor/src-maximum", maximum);
|
||||
setprop("/controls/flight/fcs/tail-rotor/low-limit", low_limit);
|
||||
setprop("/controls/flight/fcs/tail-rotor/high-limit", high_limit);
|
||||
setprop("/controls/flight/fcs/gains/tail-rotor/error-adjuster-gain", -0.5);
|
||||
return obj;
|
||||
},
|
||||
|
||||
update : func() {
|
||||
var throttle = me.read("throttle");
|
||||
var pedal_pos_deg = getprop("/controls/flight/fcs/yaw");
|
||||
var cas_input = cas.read('yaw');
|
||||
var cas_input_gain = cas.calcGain('yaw');
|
||||
var target_rate = cas_input * cas_input_gain;
|
||||
var rate = getprop("/orientation/yaw-rate-degps");
|
||||
var error_rate = getprop("/controls/flight/fcs/cas/delta_yaw");
|
||||
var error_adjuster_gain = getprop("/controls/flight/fcs/gains/tail-rotor/error-adjuster-gain");
|
||||
|
||||
var minimum = getprop("/controls/flight/fcs/tail-rotor/src-minimum");
|
||||
var maximum = getprop("/controls/flight/fcs/tail-rotor/src-maximum");
|
||||
var low_limit = getprop("/controls/flight/fcs/tail-rotor/low-limit");
|
||||
var high_limit = getprop("/controls/flight/fcs/tail-rotor/high-limit");
|
||||
var output = 0;
|
||||
var range = maximum - minimum;
|
||||
|
||||
if (throttle < minimum) {
|
||||
output = low_limit;
|
||||
} elsif (throttle > maximum) {
|
||||
output = high_limit;
|
||||
} else {
|
||||
output = low_limit + (throttle - minimum) / range * (high_limit - low_limit);
|
||||
}
|
||||
|
||||
# CAS driven tail rotor thrust adjuster
|
||||
me.adjuster = error_rate * error_adjuster_gain;
|
||||
me.adjuster = me.limit(me.adjuster, 0.3);
|
||||
output += me.adjuster;
|
||||
|
||||
setprop("/controls/flight/fcs/tail-rotor/error-rate", error_rate);
|
||||
setprop("/controls/flight/fcs/tail-rotor/adjuster", me.adjuster);
|
||||
|
||||
me.write("throttle", output);
|
||||
}
|
||||
};
|
||||
|
||||
var sas = nil;
|
||||
var cas = nil;
|
||||
var afcs = nil;
|
||||
var stabilator = nil;
|
||||
var tail = nil;
|
||||
var count = 0;
|
||||
|
||||
var sensitivities = {'roll' : 0.0, 'pitch' : 0.0, 'yaw' : 1.125 };
|
||||
var sas_initial_gains = {'roll' : 0, 'pitch' : 0, 'yaw' : 0.004 };
|
||||
var cas_input_gains = {'roll' : 30, 'pitch' : -60, 'yaw' : 30,
|
||||
'attitude-roll' : 80, 'attitude-pitch' : -80 };
|
||||
var cas_output_gains = {'roll' : 0.06, 'pitch' : -0.1, 'yaw' : 0.5,
|
||||
'roll-brake-freq' : 10, 'pitch-brake-freq' : 3,
|
||||
'roll-brake' : 0.4, 'pitch-brake' : 6,
|
||||
'anti-side-slip-gain' : -4.5};
|
||||
|
||||
var update = func {
|
||||
count += 1;
|
||||
# AFCS, CAS, and SAS run at 60Hz
|
||||
if (math.mod(count, 2) == 0) {
|
||||
return;
|
||||
}
|
||||
cas.apply('roll');
|
||||
cas.apply('pitch');
|
||||
cas.apply('yaw');
|
||||
|
||||
afcs.apply('roll');
|
||||
afcs.apply('pitch');
|
||||
afcs.apply('yaw');
|
||||
|
||||
sas.apply('roll');
|
||||
sas.apply('pitch');
|
||||
sas.apply('yaw');
|
||||
stabilator.update();
|
||||
tail.update();
|
||||
}
|
||||
|
||||
var initialize = func {
|
||||
cas = CAS.new(cas_input_gains, cas_output_gains, sensitivities, nil, "/controls/flight/fcs/cas");
|
||||
afcs = AFCS.new("/controls/flight/fcs/cas", "/controls/flight/fcs/afcs");
|
||||
sas = SAS.new(sas_initial_gains, sensitivities, 3, "/controls/flight/fcs/afcs", "/controls/flight/fcs");
|
||||
stabilator = Stabilator.new();
|
||||
tail = TailRotorCollective.new();
|
||||
setlistener("/rotors/main/cone-deg", update);
|
||||
}
|
||||
|
||||
_setlistener("/sim/signals/fdm-initialized", initialize);
|
||||
|
||||
570
Nasal/fcs2.nas
Normal file
570
Nasal/fcs2.nas
Normal file
|
|
@ -0,0 +1,570 @@
|
|||
#
|
||||
# Flight Control System by Tatsuhiro Nishioka
|
||||
# $Id: fcs.nas,v 1.11 2008/08/28 02:41:04 tat Exp $
|
||||
#
|
||||
#This one simulates a P/R and Jaw SAS
|
||||
|
||||
var FCSFilter = {
|
||||
new : func(input_path, output_path) {
|
||||
var obj = { parents : [FCSFilter],
|
||||
input_path : input_path,
|
||||
output_path : output_path };
|
||||
obj.axis_conv = {'roll' : 'aileron', 'pitch' : 'elevator', 'yaw' : 'rudder' };
|
||||
obj.body_conv = {'roll' : 'v', 'pitch' : 'u' };
|
||||
obj.last_body_fps = {'roll' : 0.0, 'pitch' : 0.0 };
|
||||
obj.last_pos = {'roll' : 0.0, 'pitch' : 0.0, 'yaw' : 0.0};
|
||||
return obj;
|
||||
},
|
||||
|
||||
# read input command for a given axis
|
||||
read : func(axis) {
|
||||
if (me.input_path == nil or me.input_path == "") {
|
||||
return getprop("/controls/flight/" ~ me.axis_conv[axis]);
|
||||
} else {
|
||||
var value = getprop(me.input_path ~ "/" ~ axis);
|
||||
value = int(value * 1000) / 1000.0;
|
||||
}
|
||||
},
|
||||
|
||||
# write output command for a given axis
|
||||
# this will be the output of an next command filter (like SAS)
|
||||
write : func(axis, value) {
|
||||
if (me.output_path == nil or me.output_path == '') {
|
||||
setprop("/controls/flight/fcs/" ~ axis, me.limit(value, 1.0));
|
||||
} else {
|
||||
setprop(me.output_path ~ "/" ~ axis, me.limit(value, 1.0));
|
||||
}
|
||||
},
|
||||
|
||||
toggleFilterStatus : func(name) {
|
||||
var messages = ["disengaged", "engaged"];
|
||||
var path = "/controls/flight/fcs/" ~ name ~ "-enabled";
|
||||
var status = getprop(path);
|
||||
setprop(path, 1 - status);
|
||||
#screen.log.write(name ~ " " ~ messages[1 - status]);
|
||||
},
|
||||
|
||||
getStatus : func(name) {
|
||||
var path = "/controls/flight/fcs/" ~ name ~ "-enabled";
|
||||
return getprop(path);
|
||||
},
|
||||
|
||||
limit : func(value, range) {
|
||||
if (value > range) {
|
||||
return range;
|
||||
} elsif (value < -range) {
|
||||
return - range;
|
||||
}
|
||||
return value;
|
||||
},
|
||||
|
||||
max : func(val1, val2) {
|
||||
return (val1 > val2) ? val1 : val2;
|
||||
},
|
||||
|
||||
min : func(val1, val2) {
|
||||
return (val1 > val2) ? val2 : val1;
|
||||
},
|
||||
|
||||
calcCounterBodyFPS : func(axis, input, offset_deg) {
|
||||
var position = getprop("/orientation/" ~ axis ~ "-deg");
|
||||
var body_fps = 0;
|
||||
var last_body_fps = me.last_body_fps[axis];
|
||||
var reaction_gain = 0;
|
||||
var heading = getprop("/orientation/heading-deg");
|
||||
var wind_speed_fps = getprop("/environment/wind-speed-kt") * 1.6878099;
|
||||
var wind_direction = getprop("/environment/wind-from-heading-deg");
|
||||
var wind_direction -= heading;
|
||||
var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
|
||||
var gear_pos = getprop("/gear/gear[0]/compression-norm") + getprop("/gear/gear[1]/compression-norm");
|
||||
var counter_fps = 0;
|
||||
var fps_axis = me.body_conv[axis]; # convert from {roll, pitch} to {u, v}
|
||||
var target_pos = offset_deg;
|
||||
var brake_deg = 0;
|
||||
|
||||
body_fps = getprop("/velocities/" ~ fps_axis ~ "Body-fps");
|
||||
if (axis == 'roll') {
|
||||
var wind_fps = math.sin(wind_direction / 180 * math.pi) * wind_speed_fps;
|
||||
} else {
|
||||
var wind_fps = math.cos(wind_direction / 180 * math.pi) * wind_speed_fps;
|
||||
}
|
||||
var brake_freq = getprop("/controls/flight/fcs/gains/afcs/fps-" ~ axis ~ "-brake-freq");
|
||||
var brake_gain = getprop("/controls/flight/fcs/gains/afcs/fps-brake-gain-" ~ axis);
|
||||
body_fps -= wind_fps;
|
||||
var dfps = body_fps - me.last_body_fps[axis];
|
||||
var fps_coeff = getprop("/controls/flight/fcs/gains/afcs/fps-" ~ axis ~ "-coeff");
|
||||
target_pos -= int(body_fps * 100) / 100 * fps_coeff;
|
||||
if (axis == 'roll' and gear_pos > 0.0 and position > 0) {
|
||||
target_pos -= position * gear_pos / 5;
|
||||
}
|
||||
reaction_gain = getprop("/controls/flight/fcs/gains/afcs/fps-reaction-gain-" ~ axis);
|
||||
var brake_sensitivity = (axis == 'roll') ? 1 : 1;
|
||||
if (math.abs(position + rate / brake_freq * brake_sensitivity) > math.abs(target_pos)) {
|
||||
if (math.abs(dfps) > 1) {
|
||||
dfps = 1;
|
||||
}
|
||||
var error_deg = target_pos - position;
|
||||
brake_deg = (error_deg - rate / brake_freq) * math.abs(dfps * 10) * brake_gain;
|
||||
if (target_pos > 0) {
|
||||
brake_deg = me.min(brake_deg, 0);
|
||||
} else {
|
||||
brake_deg = me.max(brake_deg, 0);
|
||||
}
|
||||
}
|
||||
counter_fps = me.limit((target_pos + brake_deg) * reaction_gain, 1.0);
|
||||
|
||||
setprop("/controls/flight/fcs/afcs/ah-" ~ fps_axis ~ "body-fps", body_fps);
|
||||
setprop("/controls/flight/fcs/afcs/ah-" ~ fps_axis ~ "body-wind-fps", wind_fps);
|
||||
setprop("/controls/flight/fcs/afcs/ah-" ~ axis ~ "-target-deg", target_pos);
|
||||
setprop("/controls/flight/fcs/afcs/ah-" ~ axis ~ "-rate", rate);
|
||||
setprop("/controls/flight/fcs/afcs/ah-delta-" ~ fps_axis ~ "body-fps", dfps);
|
||||
setprop("/controls/flight/fcs/afcs/ah-" ~ axis ~ "-brake-deg", brake_deg);
|
||||
|
||||
setprop("/controls/flight/fcs/afcs/counter-fps-" ~ axis, counter_fps);
|
||||
me.last_pos[axis] = position;
|
||||
me.last_body_fps[axis] = body_fps;
|
||||
return me.limit(counter_fps + input * 0.2, 1.0);
|
||||
},
|
||||
|
||||
};
|
||||
|
||||
#
|
||||
# AFCS : Automatic Flight Control System
|
||||
#
|
||||
var AFCS = {
|
||||
new : func(input_path, output_path) {
|
||||
var obj = FCSFilter.new(input_path, output_path);
|
||||
obj.parents = [FCSFilter, AFCS];
|
||||
setprop("/controls/flight/fcs/auto-hover-enabled", 0);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-brake-gain-pitch", 1.8);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-brake-gain-roll", 0.8);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-pitch-brake-freq", 3);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-pitch-coeff", -0.95);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-pitch-offset-deg", 0.9);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-reaction-gain-pitch", -0.8);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-reaction-gain-roll", 0.3436);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-roll-brake-freq", 8);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-roll-coeff", 0.8);
|
||||
setprop("/controls/flight/fcs/gains/afcs/fps-roll-offset-deg", -0.8);
|
||||
return obj;
|
||||
},
|
||||
|
||||
toggleAutoHover : func() {
|
||||
me.toggleFilterStatus("auto-hover");
|
||||
},
|
||||
|
||||
toggleAirSpeedLock : func() {
|
||||
me.toggleFilterStatus("air-speed-lock");
|
||||
},
|
||||
|
||||
toggleHeadingLock : func() {
|
||||
me.toggleFilterStatus("heading-lock");
|
||||
},
|
||||
|
||||
toggleAltitudeLock : func() {
|
||||
me.toggleFilterStatus("altitude-lock");
|
||||
},
|
||||
|
||||
#
|
||||
# auto hover : locks vBody_fps and uBody_fps regardless of wind speed/direction
|
||||
#
|
||||
autoHover : func(axis, input) {
|
||||
if (axis == 'yaw') {
|
||||
return input;
|
||||
} else {
|
||||
var offset_deg = getprop("/controls/flight/fcs/gains/afcs/fps-" ~ axis ~ "-offset-deg");
|
||||
return me.calcCounterBodyFPS(axis, input, offset_deg);
|
||||
}
|
||||
},
|
||||
|
||||
altitudeLock : func(axis, input) {
|
||||
# not implemented yet
|
||||
return input;
|
||||
},
|
||||
|
||||
headingLock : func(axis, input) {
|
||||
# not implementet yet
|
||||
return input;
|
||||
},
|
||||
|
||||
apply : func(axis) {
|
||||
var input = me.read(axis);
|
||||
var hover_status = me.getStatus("auto-hover");
|
||||
if (hover_status == 0) {
|
||||
me.write(axis, input);
|
||||
return;
|
||||
}
|
||||
me.write(axis, me.autoHover(axis, input));
|
||||
}
|
||||
};
|
||||
|
||||
#
|
||||
# SAS : Stability Augmentation System - a rate damper
|
||||
#
|
||||
var SAS = {
|
||||
#
|
||||
# new
|
||||
# initial_gains: hash of initial gains for rate damping
|
||||
# sensitivities: hash of minimum rates (deg/sec) that enables rate damper
|
||||
# authority_limit: shows how much SAS can take over control
|
||||
# 0 means no stability control, 1.0 means SAS fully takes over pilot control
|
||||
# input_path: is a base path to input axis; nil for using raw input from KB/JS
|
||||
# output_path: is a base path to output axis; nis for using /controls/flight/fcs
|
||||
#
|
||||
# with input_path / output_path, you can connect SAS, CAS, and more control filters
|
||||
#
|
||||
new : func(initial_gains, sensitivities, authority_limit, input_path, output_path) {
|
||||
var obj = FCSFilter.new(input_path, output_path);
|
||||
obj.parents = [FCSFilter, SAS];
|
||||
obj.authority_limit = authority_limit;
|
||||
obj.sensitivities = sensitivities;
|
||||
obj.initial_gains = initial_gains;
|
||||
props.globals.getNode("/controls/flight/fcs/gains/sas", 1).setValues(obj.initial_gains);
|
||||
setprop("/controls/flight/fcs/sas-enabled", 1);
|
||||
return obj;
|
||||
},
|
||||
|
||||
toggleEnable : func() {
|
||||
me.toggleFilterStatus("sas");
|
||||
},
|
||||
|
||||
#
|
||||
# calcGain - get gain for each axis based on air speed and dynamic pressure
|
||||
# axis: one of 'roll', 'pitch', or 'yaw'
|
||||
#
|
||||
calcGain : func(axis) {
|
||||
var mach = getprop("/velocities/mach");
|
||||
var initial_gain = getprop("/controls/flight/fcs/gains/sas/" ~ axis);
|
||||
var gain = initial_gain - 0.1 * mach * mach;
|
||||
if (math.abs(gain) < math.abs(initial_gain) * 0.01 or gain * initial_gain < 0) {
|
||||
gain = initial_gain * 0.01;
|
||||
}
|
||||
return gain;
|
||||
},
|
||||
|
||||
calcAuthorityLimit : func() {
|
||||
var mach = getprop("/velocities/mach");
|
||||
var min_mach = 0.038;
|
||||
var limit = me.authority_limit;
|
||||
if (math.abs(mach < min_mach)) {
|
||||
limit += (min_mach - math.abs(mach)) / min_mach * (1 - me.authority_limit) * 0.95;
|
||||
}
|
||||
setprop("/controls/flight/fcs/gains/sas/authority-limit", limit);
|
||||
return limit;
|
||||
},
|
||||
|
||||
#
|
||||
# apply - apply SAS damper to a given input axis
|
||||
# axis: one of 'roll', 'pitch', or 'yaw'
|
||||
#
|
||||
apply : func(axis) {
|
||||
var status = me.getStatus("sas");
|
||||
var input = me.read(axis);
|
||||
if (status == 0) {
|
||||
me.write(axis, input);
|
||||
return;
|
||||
}
|
||||
var mach = getprop("/velocities/mach");
|
||||
var value = 0;
|
||||
var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
|
||||
var gain = me.calcGain(axis);
|
||||
var limit = me.calcAuthorityLimit();
|
||||
if (math.abs(rate) >= me.sensitivities[axis]) {
|
||||
value = - gain * rate;
|
||||
if (value > limit) {
|
||||
value = limit;
|
||||
} elsif (value < - limit) {
|
||||
value = - limit;
|
||||
}
|
||||
}
|
||||
me.write(axis, value + input);
|
||||
}
|
||||
};
|
||||
|
||||
#
|
||||
# CAS : Control Augmentation System - makes your aircraft more meneuverable
|
||||
#
|
||||
var CAS = {
|
||||
new : func(input_gains, output_gains, sensitivities, input_path, output_path) {
|
||||
var obj = FCSFilter.new(input_path, output_path);
|
||||
obj.parents = [FCSFilter, CAS];
|
||||
obj.sensitivities = sensitivities;
|
||||
obj.input_gains = input_gains;
|
||||
obj.output_gains = output_gains;
|
||||
props.globals.getNode("/controls/flight/fcs/gains/cas/input", 1).setValues(obj.input_gains);
|
||||
props.globals.getNode("/controls/flight/fcs/gains/cas/output", 1).setValues(obj.output_gains);
|
||||
setprop("/autopilot/locks/altitude", '');
|
||||
setprop("/autopilot/locks/heading", '');
|
||||
setprop("/controls/flight/fcs/cas-enabled", 1);
|
||||
return obj;
|
||||
},
|
||||
|
||||
calcRollRateAdjustment : func {
|
||||
var position = getprop("/orientation/roll-deg");
|
||||
return math.abs(math.sin(position / 180 * math.pi)) / 6;
|
||||
},
|
||||
|
||||
calcSideSlipAdjustment : func {
|
||||
var mach = getprop("/velocities/mach");
|
||||
var slip = getprop("/orientation/side-slip-deg");
|
||||
if (mach < 0.015) { # works only if air speed > 10kt
|
||||
slip = 0;
|
||||
}
|
||||
var anti_slip_gain = getprop("/controls/flight/fcs/gains/cas/output/anti-side-slip-gain");
|
||||
var roll_deg = getprop("/orientation/roll-deg");
|
||||
var gain_adjuster = me.min(math.abs(mach) / 0.060, 1) * me.limit(0.2 + math.sqrt(math.abs(roll_deg)/10), 3);
|
||||
anti_slip_gain *= gain_adjuster;
|
||||
setprop("/controls/flight/fcs/cas/anti-side-slip", slip * anti_slip_gain);
|
||||
return slip * anti_slip_gain;
|
||||
},
|
||||
|
||||
# FIXME: command for CAS is just a temporal one
|
||||
calcCommand: func (axis, input) {
|
||||
var output = 0;
|
||||
var mach = getprop("/velocities/mach");
|
||||
var input_gain = me.calcGain(axis);
|
||||
var output_gain = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis);
|
||||
var target_rate = input * input_gain;
|
||||
var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
|
||||
var drate = target_rate - rate;
|
||||
var locks = {'pitch' : getprop("/autopilot/locks/altitude"),
|
||||
'roll' : getprop("/autopilot/locks/heading")};
|
||||
setprop("/controls/flight/fcs/cas/target_" ~ axis ~ "rate", target_rate);
|
||||
setprop("/controls/flight/fcs/cas/delta_" ~ axis, drate);
|
||||
|
||||
if (axis == 'roll' or axis == 'pitch') {
|
||||
if (math.abs(input > 0.7) or locks[axis] != '') {
|
||||
output = drate * output_gain;
|
||||
} else {
|
||||
output = me.calcAttitudeCommand(axis);
|
||||
}
|
||||
if (axis == 'roll' and math.abs(mach) < 0.035) {
|
||||
# FIXME: I don't know if OH-1 has this one
|
||||
output += me.calcCounterBodyFPS(axis, input, -0.8);
|
||||
}
|
||||
} elsif (axis == 'yaw') {
|
||||
output = drate * output_gain + me.calcSideSlipAdjustment();
|
||||
} else {
|
||||
output = drate * output_gain;
|
||||
}
|
||||
return output;
|
||||
},
|
||||
|
||||
toggleEnable : func() {
|
||||
me.toggleFilterStatus("cas");
|
||||
},
|
||||
|
||||
calcAttitudeCommand : func(axis) {
|
||||
var input_gain = getprop("/controls/flight/fcs/gains/cas/input/attitude-" ~ axis);
|
||||
var output_gain = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis);
|
||||
var brake_freq = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis ~ "-brake-freq");
|
||||
var brake_gain = getprop("/controls/flight/fcs/gains/cas/output/" ~ axis ~ "-brake");
|
||||
var trim = getprop("/controls/flight/" ~ me.axis_conv[axis] ~ "-trim");
|
||||
|
||||
var current_deg = getprop("/orientation/" ~ axis ~ "-deg");
|
||||
var rate = getprop("/orientation/" ~ axis ~ "-rate-degps");
|
||||
var target_deg = (me.read(axis) + trim) * input_gain;
|
||||
var command_deg = 0;
|
||||
if (target_deg != 0) {
|
||||
command_deg = (0.094 * math.ln(math.abs(target_deg)) + 0.53) * target_deg;
|
||||
}
|
||||
|
||||
var error_deg = command_deg - current_deg;
|
||||
var brake_deg = (error_deg - rate / brake_freq) * math.abs(error_deg) * brake_gain;
|
||||
|
||||
if (command_deg > 0) {
|
||||
brake_deg = me.min(brake_deg, 0);
|
||||
} else {
|
||||
brake_deg = me.max(brake_deg, 0);
|
||||
}
|
||||
|
||||
var monitor_prefix = me.output_path ~ "/" ~ axis;
|
||||
setprop(monitor_prefix ~ "-target_deg", target_deg);
|
||||
setprop(monitor_prefix ~ "-error_deg", error_deg);
|
||||
setprop(monitor_prefix ~ "-brake_deg", brake_deg);
|
||||
setprop(monitor_prefix ~ "-deg", current_deg);
|
||||
setprop(monitor_prefix ~ "-rate", -rate);
|
||||
|
||||
return (error_deg + brake_deg) * output_gain;
|
||||
},
|
||||
|
||||
# FixMe: gain should be calculated using both speed and dynamic pressure
|
||||
calcGain : func(axis) {
|
||||
var mach = getprop("/velocities/mach");
|
||||
var input_gain = getprop("/controls/flight/fcs/gains/cas/input/" ~ axis);
|
||||
var gain = input_gain;
|
||||
if (axis == 'pitch') {
|
||||
gain += 0.1 * mach * mach;
|
||||
} elsif (axis== 'yaw') {
|
||||
gain *= ((1 - mach) * (1 - mach));
|
||||
}
|
||||
if (gain * input_gain < 0.0 ) {
|
||||
gain = 0;
|
||||
}
|
||||
return gain;
|
||||
},
|
||||
|
||||
apply : func(axis) {
|
||||
var input = me.read(axis);
|
||||
var status = me.getStatus("cas");
|
||||
var cas_command = 0;
|
||||
# FIXME : hmm, a bit nasty. CAS should be enabled even with auto-hover....
|
||||
if (status == 0 or (me.getStatus("auto-hover") == 1 and axis != 'yaw')) {
|
||||
me.write(axis, input);
|
||||
return;
|
||||
}
|
||||
cas_command = me.calcCommand(axis, input);
|
||||
me.write(axis, cas_command);
|
||||
}
|
||||
};
|
||||
|
||||
#
|
||||
# Tail hstab, "stabilator," for stabilize the nose
|
||||
#
|
||||
var Stabilator = {
|
||||
new : func() {
|
||||
var obj = { parents : [Stabilator] };
|
||||
setprop("/controls/flight/fcs/gains/stabilator", -1.8);
|
||||
setprop("/controls/flight/fcs/auto-stabilator", 1);
|
||||
# 0 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160, 170, 180, .....
|
||||
me.gainTable = [-0.9, -0.8, 0.1, -0.5, 0.0, 0.7, 0.8, 0.9, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 0.9, 0.8, 0.6, 0.4, 0.2, -1.0];
|
||||
return obj;
|
||||
},
|
||||
|
||||
toggleManual : func {
|
||||
var status = getprop("/controls/flight/fcs/auto-stabilator");
|
||||
getprop("/controls/flight/fcs/auto-stabilator", 1 - status);
|
||||
},
|
||||
|
||||
apply : func(delta) {
|
||||
setprop("/controls/flight/fcs/auto-stabilator", 0);
|
||||
var value = getprop("/controls/flight/fcs/stabilator");
|
||||
getprop("/controls/flight/fcs/stabilator", value + delta);
|
||||
},
|
||||
|
||||
calcPosition : func() {
|
||||
var speed = getprop("/velocities/mach") / 0.001497219; # in knot
|
||||
var index = int(math.abs(speed) / 10);
|
||||
if (index >= size(me.gainTable) - 1) {
|
||||
index = size(me.gainTable) - 2;
|
||||
}
|
||||
var mod = math.mod(int(math.abs(speed)), 10);
|
||||
var position = me.gainTable[index] * ((10 - mod) / 10) + me.gainTable[index-1] * (mod) / 10;
|
||||
if (speed < -20) {
|
||||
position = - position;
|
||||
}
|
||||
return position;
|
||||
},
|
||||
|
||||
update : func() {
|
||||
var status = getprop("/controls/flight/fcs/auto-stabilator");
|
||||
if (status == 0) {
|
||||
return;
|
||||
}
|
||||
var gain = getprop("/controls/flight/fcs/gains/stabilator");
|
||||
var mach = getprop("/velocities/mach");
|
||||
var throttle = getprop("/controls/flight/throttle");
|
||||
var stabilator_norm = 0;
|
||||
|
||||
stabilator_norm = me.calcPosition();
|
||||
setprop("/controls/flight/fcs/stabilator", stabilator_norm);
|
||||
}
|
||||
};
|
||||
|
||||
var TailRotorCollective = {
|
||||
new : func(minimum=0.10, maximum=1.0, low_limit=0.00011, high_limit=0.0035) {
|
||||
var obj = FCSFilter.new("/controls/engines/engine[1]", "/controls/flight/fcs/tail-rotor");
|
||||
obj.parents = [FCSFilter, TailRotorCollective];
|
||||
obj.adjuster = 0.0;
|
||||
setprop("/controls/flight/fcs/tail-rotor/src-minimum", minimum);
|
||||
setprop("/controls/flight/fcs/tail-rotor/src-maximum", maximum);
|
||||
setprop("/controls/flight/fcs/tail-rotor/low-limit", low_limit);
|
||||
setprop("/controls/flight/fcs/tail-rotor/high-limit", high_limit);
|
||||
setprop("/controls/flight/fcs/gains/tail-rotor/error-adjuster-gain", -0.5);
|
||||
return obj;
|
||||
},
|
||||
|
||||
update : func() {
|
||||
var throttle = me.read("throttle");
|
||||
var pedal_pos_deg = getprop("/controls/flight/fcs/yaw");
|
||||
var cas_input = cas.read('yaw');
|
||||
var cas_input_gain = cas.calcGain('yaw');
|
||||
var target_rate = cas_input * cas_input_gain;
|
||||
var rate = getprop("/orientation/yaw-rate-degps");
|
||||
var error_rate = getprop("/controls/flight/fcs/cas/delta_yaw");
|
||||
var error_adjuster_gain = getprop("/controls/flight/fcs/gains/tail-rotor/error-adjuster-gain");
|
||||
|
||||
var minimum = getprop("/controls/flight/fcs/tail-rotor/src-minimum");
|
||||
var maximum = getprop("/controls/flight/fcs/tail-rotor/src-maximum");
|
||||
var low_limit = getprop("/controls/flight/fcs/tail-rotor/low-limit");
|
||||
var high_limit = getprop("/controls/flight/fcs/tail-rotor/high-limit");
|
||||
var output = 0;
|
||||
var range = maximum - minimum;
|
||||
|
||||
if (throttle < minimum) {
|
||||
output = low_limit;
|
||||
} elsif (throttle > maximum) {
|
||||
output = high_limit;
|
||||
} else {
|
||||
output = low_limit + (throttle - minimum) / range * (high_limit - low_limit);
|
||||
}
|
||||
|
||||
# CAS driven tail rotor thrust adjuster
|
||||
me.adjuster = error_rate * error_adjuster_gain;
|
||||
me.adjuster = me.limit(me.adjuster, 0.3);
|
||||
output += me.adjuster;
|
||||
|
||||
setprop("/controls/flight/fcs/tail-rotor/error-rate", error_rate);
|
||||
setprop("/controls/flight/fcs/tail-rotor/adjuster", me.adjuster);
|
||||
|
||||
me.write("throttle", output);
|
||||
}
|
||||
};
|
||||
|
||||
var sas = nil;
|
||||
var cas = nil;
|
||||
var afcs = nil;
|
||||
var stabilator = nil;
|
||||
var tail = nil;
|
||||
var count = 0;
|
||||
|
||||
var sensitivities = {'roll' : 0.0, 'pitch' : 0.0, 'yaw' : 1.125 };
|
||||
var sas_initial_gains = {'roll' : 0.0011, 'pitch' : -0.0042, 'yaw' : 0.004 };
|
||||
var cas_input_gains = {'roll' : 30, 'pitch' : -60, 'yaw' : 30,
|
||||
'attitude-roll' : 80, 'attitude-pitch' : -80 };
|
||||
var cas_output_gains = {'roll' : 0.06, 'pitch' : -0.1, 'yaw' : 0.5,
|
||||
'roll-brake-freq' : 10, 'pitch-brake-freq' : 3,
|
||||
'roll-brake' : 0.4, 'pitch-brake' : 6,
|
||||
'anti-side-slip-gain' : -4.5};
|
||||
var update = func {
|
||||
count += 1;
|
||||
# AFCS, CAS, and SAS run at 60Hz
|
||||
if (math.mod(count, 2) == 0) {
|
||||
return;
|
||||
}
|
||||
cas.apply('roll');
|
||||
cas.apply('pitch');
|
||||
cas.apply('yaw');
|
||||
|
||||
afcs.apply('roll');
|
||||
afcs.apply('pitch');
|
||||
afcs.apply('yaw');
|
||||
|
||||
sas.apply('roll');
|
||||
sas.apply('pitch');
|
||||
sas.apply('yaw');
|
||||
stabilator.update();
|
||||
tail.update();
|
||||
}
|
||||
|
||||
var initialize = func {
|
||||
cas = CAS.new(cas_input_gains, cas_output_gains, sensitivities, nil, "/controls/flight/fcs/cas");
|
||||
afcs = AFCS.new("/controls/flight/fcs/cas", "/controls/flight/fcs/afcs");
|
||||
sas = SAS.new(sas_initial_gains, sensitivities, 3, "/controls/flight/fcs/afcs", "/controls/flight/fcs");
|
||||
stabilator = Stabilator.new();
|
||||
tail = TailRotorCollective.new();
|
||||
setlistener("/rotors/main/cone-deg", update);
|
||||
}
|
||||
|
||||
_setlistener("/sim/signals/fdm-initialized", initialize);
|
||||
|
||||
BIN
Ressource/default.fuselage.jpg
Normal file
BIN
Ressource/default.fuselage.jpg
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 797 KiB |
BIN
Ressource/default.tail.jpg
Normal file
BIN
Ressource/default.tail.jpg
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 515 KiB |
|
|
@ -1,120 +1,118 @@
|
|||
// -*- mode: C; -*-
|
||||
// Licence: GPL v2
|
||||
// Author: Vivian Meazza.
|
||||
|
||||
#version 120
|
||||
|
||||
varying vec4 rawpos;
|
||||
varying vec4 ecPosition;
|
||||
varying vec3 VNormal;
|
||||
varying vec3 Normal;
|
||||
varying vec4 constantColor;
|
||||
varying vec3 vViewVec;
|
||||
varying vec3 reflVec;
|
||||
|
||||
varying vec4 Diffuse;
|
||||
varying vec3 lightDir, halfVector;
|
||||
varying float alpha, fogCoord;
|
||||
|
||||
uniform samplerCube Environment;
|
||||
uniform sampler2D Rainbow;
|
||||
uniform sampler2D BaseTex;
|
||||
uniform sampler2D Fresnel;
|
||||
uniform sampler2D Map;
|
||||
uniform sampler3D Noise;
|
||||
|
||||
uniform float refl_correction;
|
||||
uniform float rainbowiness;
|
||||
uniform float fresneliness;
|
||||
uniform float noisiness;
|
||||
uniform float ambient_correction;
|
||||
uniform float reflect_map;
|
||||
|
||||
void main (void)
|
||||
{
|
||||
if (!gl_FrontFacing) discard;
|
||||
|
||||
vec3 n, halfV;
|
||||
float NdotL, NdotHV;
|
||||
vec4 color = constantColor;
|
||||
vec4 specular = vec4(0.0);
|
||||
n = VNormal;
|
||||
NdotL = max(0.0, dot(n, lightDir));
|
||||
|
||||
// calculate the specular light
|
||||
if (NdotL > 0.0) {
|
||||
color += Diffuse * NdotL;
|
||||
halfV = normalize(halfVector);
|
||||
NdotHV = max(dot(n, halfV), 0.0);
|
||||
if (gl_FrontMaterial.shininess > 0.0)
|
||||
specular.rgb = (gl_FrontMaterial.specular.rgb
|
||||
* gl_LightSource[0].specular.rgb
|
||||
* pow(NdotHV, gl_FrontMaterial.shininess));
|
||||
}
|
||||
|
||||
color.a = alpha;
|
||||
color = clamp(color, 0.0, 1.0);
|
||||
vec4 texel = texture2D(BaseTex, gl_TexCoord[0].st);
|
||||
vec4 texelcolor = color * texel + specular;
|
||||
|
||||
// calculate the fog factor
|
||||
float fogCoord = ecPosition.z;
|
||||
const float LOG2 = 1.442695;
|
||||
float fogFactor = exp2(-gl_Fog.density * gl_Fog.density * fogCoord * fogCoord * LOG2);
|
||||
fogFactor = clamp(fogFactor, 0.0, 1.0);
|
||||
|
||||
if(gl_Fog.density == 1.0)
|
||||
fogFactor=1.0;
|
||||
|
||||
vec3 normal = normalize(VNormal);
|
||||
vec3 viewVec = normalize(vViewVec);
|
||||
|
||||
// Map a rainbowish color
|
||||
float v = dot(viewVec, normal);
|
||||
vec4 rainbow = texture2D(Rainbow, vec2(v, 0.0));
|
||||
|
||||
// Map a fresnel effect
|
||||
vec4 fresnel = texture2D(Fresnel, vec2(v, 0.0));
|
||||
|
||||
// map the refection of the environment
|
||||
vec4 reflection = textureCube(Environment, reflVec);
|
||||
|
||||
// set the user shininess offse
|
||||
float transparency_offset = clamp(refl_correction, -1.0, 1.0);
|
||||
float reflFactor = 0.0;
|
||||
|
||||
if(reflect_map > 0){
|
||||
// map the shininess of the object with user input
|
||||
vec4 map = texture2D(Map, gl_TexCoord[0].st);
|
||||
//float pam = (map.a * -2) + 1; //reverse map
|
||||
reflFactor = map.a + transparency_offset;
|
||||
} else {
|
||||
// set the reflectivity proportional to shininess with user
|
||||
// input
|
||||
reflFactor = (gl_FrontMaterial.shininess / 128) + transparency_offset;
|
||||
}
|
||||
|
||||
reflFactor = clamp(reflFactor, 0.0, 1.0);
|
||||
|
||||
// set ambient adjustment to remove bluiness with user input
|
||||
float ambient_offset = clamp(ambient_correction, -1.0, 1.0);
|
||||
vec4 ambient_Correction = vec4(gl_LightSource[0].ambient.rg, gl_LightSource[0].ambient.b * 0.6, 0.5) * ambient_offset ;
|
||||
ambient_Correction = clamp(ambient_Correction, -1.0, 1.0);
|
||||
|
||||
// map noise vectore
|
||||
vec4 noisevec = texture3D(Noise, rawpos.xyz);
|
||||
|
||||
// add fringing fresnel and rainbow effects and modulate by reflection
|
||||
vec4 reflcolor = mix(reflection, rainbow, rainbowiness * v);
|
||||
vec4 reflfrescolor = mix(reflcolor, fresnel, fresneliness * v);
|
||||
vec4 noisecolor = mix(reflfrescolor, noisevec, noisiness);
|
||||
vec4 raincolor = vec4(noisecolor.rgb, 1.0) * reflFactor;
|
||||
|
||||
vec4 mixedcolor = mix(texel, raincolor, reflFactor);
|
||||
|
||||
// the final reflection
|
||||
vec4 reflColor = color * mixedcolor + specular + ambient_Correction ;
|
||||
reflColor = clamp(reflColor, 0.0, 1.0);
|
||||
|
||||
gl_FragColor = mix(gl_Fog.color, reflColor, fogFactor);
|
||||
}
|
||||
// -*- mode: C; -*-
|
||||
// Licence: GPL v2
|
||||
// Author: Vivian Meazza.
|
||||
|
||||
#version 120
|
||||
|
||||
varying vec4 rawpos;
|
||||
varying vec4 ecPosition;
|
||||
varying vec3 VNormal;
|
||||
varying vec3 Normal;
|
||||
varying vec4 constantColor;
|
||||
varying vec3 vViewVec;
|
||||
varying vec3 reflVec;
|
||||
|
||||
varying vec4 Diffuse;
|
||||
varying vec3 lightDir, halfVector;
|
||||
varying float alpha, fogCoord;
|
||||
|
||||
uniform samplerCube Environment;
|
||||
uniform sampler2D Rainbow;
|
||||
uniform sampler2D BaseTex;
|
||||
uniform sampler2D Fresnel;
|
||||
uniform sampler2D Map;
|
||||
uniform sampler3D Noise;
|
||||
|
||||
uniform float refl_correction;
|
||||
uniform float rainbowiness;
|
||||
uniform float fresneliness;
|
||||
uniform float noisiness;
|
||||
uniform float ambient_correction;
|
||||
uniform float reflect_map;
|
||||
|
||||
void main (void)
|
||||
{
|
||||
vec3 n, halfV;
|
||||
float NdotL, NdotHV;
|
||||
vec4 color = constantColor;
|
||||
vec4 specular = vec4(0.0);
|
||||
n = VNormal;
|
||||
NdotL = max(0.0, dot(n, lightDir));
|
||||
|
||||
// calculate the specular light
|
||||
if (NdotL > 0.0) {
|
||||
color += Diffuse * NdotL;
|
||||
halfV = normalize(halfVector);
|
||||
NdotHV = max(dot(n, halfV), 0.0);
|
||||
if (gl_FrontMaterial.shininess > 0.0)
|
||||
specular.rgb = (gl_FrontMaterial.specular.rgb
|
||||
* gl_LightSource[0].specular.rgb
|
||||
* pow(NdotHV, gl_FrontMaterial.shininess));
|
||||
}
|
||||
|
||||
color.a = alpha;
|
||||
color = clamp(color, 0.0, 1.0);
|
||||
vec4 texel = texture2D(BaseTex, gl_TexCoord[0].st);
|
||||
vec4 texelcolor = color * texel + specular;
|
||||
|
||||
// calculate the fog factor
|
||||
float fogCoord = ecPosition.z;
|
||||
const float LOG2 = 1.442695;
|
||||
float fogFactor = exp2(-gl_Fog.density * gl_Fog.density * fogCoord * fogCoord * LOG2);
|
||||
fogFactor = clamp(fogFactor, 0.0, 1.0);
|
||||
|
||||
if(gl_Fog.density == 1.0)
|
||||
fogFactor=1.0;
|
||||
|
||||
vec3 normal = normalize(VNormal);
|
||||
vec3 viewVec = normalize(vViewVec);
|
||||
|
||||
// Map a rainbowish color
|
||||
float v = dot(viewVec, normal);
|
||||
vec4 rainbow = texture2D(Rainbow, vec2(v, 0.0));
|
||||
|
||||
// Map a fresnel effect
|
||||
vec4 fresnel = texture2D(Fresnel, vec2(v, 0.0));
|
||||
|
||||
// map the refection of the environment
|
||||
vec4 reflection = textureCube(Environment, reflVec);
|
||||
|
||||
// set the user shininess offse
|
||||
float transparency_offset = clamp(refl_correction, -1.0, 1.0);
|
||||
float reflFactor = 0.0;
|
||||
|
||||
if(reflect_map > 0){
|
||||
// map the shininess of the object with user input
|
||||
vec4 map = texture2D(Map, gl_TexCoord[0].st);
|
||||
//float pam = (map.a * -2) + 1; //reverse map
|
||||
reflFactor = map.a + transparency_offset;
|
||||
} else {
|
||||
// set the reflectivity proportional to shininess with user
|
||||
// input
|
||||
reflFactor = (gl_FrontMaterial.shininess / 128) + transparency_offset;
|
||||
}
|
||||
|
||||
reflFactor = clamp(reflFactor, 0.0, 1.0);
|
||||
|
||||
// set ambient adjustment to remove bluiness with user input
|
||||
float ambient_offset = clamp(ambient_correction, -1.0, 1.0);
|
||||
vec4 ambient_Correction = vec4(gl_LightSource[0].ambient.rg, gl_LightSource[0].ambient.b * 0.6, 0.5) * ambient_offset ;
|
||||
ambient_Correction = clamp(ambient_Correction, -1.0, 1.0);
|
||||
|
||||
// map noise vectore
|
||||
vec4 noisevec = texture3D(Noise, rawpos.xyz);
|
||||
|
||||
// add fringing fresnel and rainbow effects and modulate by reflection
|
||||
vec4 reflcolor = mix(reflection, rainbow, rainbowiness * v);
|
||||
vec4 reflfrescolor = mix(reflcolor, fresnel, fresneliness * v);
|
||||
vec4 noisecolor = mix(reflfrescolor, noisevec, noisiness);
|
||||
vec4 raincolor = vec4(noisecolor.rgb, 1.0) * reflFactor;
|
||||
|
||||
vec4 mixedcolor = mix(texel, raincolor, reflFactor);
|
||||
|
||||
// the final reflection
|
||||
vec4 reflColor = color * mixedcolor + specular + ambient_Correction ;
|
||||
reflColor = clamp(reflColor, 0.0, 1.0);
|
||||
|
||||
gl_FragColor = mix(gl_Fog.color, reflColor, fogFactor);
|
||||
}
|
||||
|
|
|
|||
BIN
Sounds/GE-M134.wav
Normal file
BIN
Sounds/GE-M134.wav
Normal file
Binary file not shown.
BIN
Sounds/HOT.wav
Normal file
BIN
Sounds/HOT.wav
Normal file
Binary file not shown.
BIN
Sounds/R-1535Slow.wav
Normal file
BIN
Sounds/R-1535Slow.wav
Normal file
Binary file not shown.
BIN
Sounds/TC1.wav
Normal file
BIN
Sounds/TC1.wav
Normal file
Binary file not shown.
BIN
Sounds/blade_vortex.wav
Normal file
BIN
Sounds/blade_vortex.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_idle-inside.wav
Normal file
BIN
Sounds/ec135_idle-inside.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_rotor.wav
Normal file
BIN
Sounds/ec135_rotor.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_rotor_in.wav
Normal file
BIN
Sounds/ec135_rotor_in.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_rotor_out.wav
Normal file
BIN
Sounds/ec135_rotor_out.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_shut_ec_in.wav
Normal file
BIN
Sounds/ec135_shut_ec_in.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_shut_ec_out.wav
Normal file
BIN
Sounds/ec135_shut_ec_out.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_turbine_idle_in.wav
Normal file
BIN
Sounds/ec135_turbine_idle_in.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_turbine_idle_out.wav
Normal file
BIN
Sounds/ec135_turbine_idle_out.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_turbine_idle_out2.wav
Normal file
BIN
Sounds/ec135_turbine_idle_out2.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_turbine_strt_in.wav
Normal file
BIN
Sounds/ec135_turbine_strt_in.wav
Normal file
Binary file not shown.
BIN
Sounds/ec135_turbine_strt_out.wav
Normal file
BIN
Sounds/ec135_turbine_strt_out.wav
Normal file
Binary file not shown.
BIN
Sounds/ec_rotor_in.wav
Normal file
BIN
Sounds/ec_rotor_in.wav
Normal file
Binary file not shown.
BIN
Sounds/ec_rotor_out2.wav
Normal file
BIN
Sounds/ec_rotor_out2.wav
Normal file
Binary file not shown.
BIN
Sounds/fenestron_ec135.wav
Normal file
BIN
Sounds/fenestron_ec135.wav
Normal file
Binary file not shown.
BIN
Sounds/flight_ec135_out.wav
Normal file
BIN
Sounds/flight_ec135_out.wav
Normal file
Binary file not shown.
BIN
Sounds/idle_ec135_out.wav
Normal file
BIN
Sounds/idle_ec135_out.wav
Normal file
Binary file not shown.
BIN
Sounds/rotor_stall.wav
Normal file
BIN
Sounds/rotor_stall.wav
Normal file
Binary file not shown.
813
Sounds/sound.xml
Normal file
813
Sounds/sound.xml
Normal file
|
|
@ -0,0 +1,813 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
thanks to the SAR simulation (GPL) for the helicopter sounds,
|
||||
and the Urban game (LGPL) for the weapon sounds
|
||||
|
||||
+x = aft
|
||||
+y = left
|
||||
+z = up
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
<fx>
|
||||
<starter>
|
||||
<name>starter0_start</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/starter_start.wav</path>
|
||||
<condition>
|
||||
<property>controls/engines/engine[0]/starter</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.1</factor>
|
||||
</volume>
|
||||
<position>
|
||||
<x>-0.88</x>
|
||||
<y>0.40</y>
|
||||
<z>0.5</z>
|
||||
</position>
|
||||
<reference-dist>5</reference-dist>
|
||||
<max-dist>10</max-dist>
|
||||
</starter>
|
||||
|
||||
<starter>
|
||||
<name>starter0_loop</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/starter_loop.wav</path>
|
||||
<condition>
|
||||
<property>controls/engines/engine[0]/starter</property>
|
||||
</condition>
|
||||
<delay-sec>11.6</delay-sec>
|
||||
<volume>
|
||||
<factor>0.1</factor>
|
||||
</volume>
|
||||
<position>
|
||||
<x>-0.88</x>
|
||||
<y>0.40</y>
|
||||
<z>0.5</z>
|
||||
</position>
|
||||
<reference-dist>5</reference-dist>
|
||||
<max-dist>10</max-dist>
|
||||
</starter>
|
||||
|
||||
<starter>
|
||||
<name>starter0_stop</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/starter_stop.wav</path>
|
||||
<condition>
|
||||
<not>
|
||||
<property>controls/engines/engine[0]/starter</property>
|
||||
</not>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.3</factor>
|
||||
</volume>
|
||||
<position>
|
||||
<x>-0.88</x>
|
||||
<y>0.40</y>
|
||||
<z>0.5</z>
|
||||
</position>
|
||||
<reference-dist>5</reference-dist>
|
||||
<max-dist>10</max-dist>
|
||||
</starter>
|
||||
|
||||
<starter>
|
||||
<name>starter1_start</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/starter_start.wav</path>
|
||||
<condition>
|
||||
<property>controls/engines/engine[1]/starter</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.3</factor>
|
||||
</volume>
|
||||
<position>
|
||||
<x>-0.88</x>
|
||||
<y>-0.40</y>
|
||||
<z>0.5</z>
|
||||
</position>
|
||||
<reference-dist>5</reference-dist>
|
||||
<max-dist>10</max-dist>
|
||||
</starter>
|
||||
|
||||
<starter>
|
||||
<name>starter1_loop</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/starter_loop.wav</path>
|
||||
<condition>
|
||||
<property>controls/engines/engine[1]/starter</property>
|
||||
</condition>
|
||||
<delay-sec>11.6</delay-sec>
|
||||
<volume>
|
||||
<factor>0.1</factor>
|
||||
</volume>
|
||||
<position>
|
||||
<x>-0.88</x>
|
||||
<y>-0.40</y>
|
||||
<z>0.5</z>
|
||||
</position>
|
||||
<reference-dist>5</reference-dist>
|
||||
<max-dist>10</max-dist>
|
||||
</starter>
|
||||
|
||||
<starter>
|
||||
<name>starter1_stop</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/starter_stop.wav</path>
|
||||
<condition>
|
||||
<not>
|
||||
<property>controls/engines/engine[1]/starter</property>
|
||||
</not>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.1</factor>
|
||||
</volume>
|
||||
<position>
|
||||
<x>-0.88</x>
|
||||
<y>-0.40</y>
|
||||
<z>0.5</z>
|
||||
</position>
|
||||
<reference-dist>5</reference-dist>
|
||||
<max-dist>10</max-dist>
|
||||
</starter>
|
||||
|
||||
<engine>
|
||||
<name>turbine0-start</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/strt_ec135_out2.wav</path>
|
||||
<condition>
|
||||
<greater-than>
|
||||
<property>engines/engine[0]/n1-pct</property>
|
||||
<value>0.1</value>
|
||||
</greater-than>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.03</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>5</factor>
|
||||
</volume>
|
||||
<reference-dist>50</reference-dist>
|
||||
<max-dist>200</max-dist>
|
||||
</engine>
|
||||
|
||||
<engine>
|
||||
<name>turbine0-loop</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/idle_ec135_out.wav</path>
|
||||
<condition>
|
||||
<property>engines/engine[0]/running</property>
|
||||
</condition>
|
||||
<delay-sec>45</delay-sec>
|
||||
<volume>
|
||||
<factor>0.03</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>5</factor>
|
||||
</volume>
|
||||
<reference-dist>50</reference-dist>
|
||||
<max-dist>200</max-dist>
|
||||
</engine>
|
||||
|
||||
<engine>
|
||||
<name>turbine0-shutdown</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/turbine_shutdown.wav</path>
|
||||
<condition>
|
||||
<not>
|
||||
<property>engines/engine[0]/running</property>
|
||||
</not>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.03</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>5</factor>
|
||||
</volume>
|
||||
<reference-dist>50</reference-dist>
|
||||
<max-dist>200</max-dist>
|
||||
</engine>
|
||||
|
||||
<engine>
|
||||
<name>turbine1-start</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/strt_ec135_out2.wav</path>
|
||||
<condition>
|
||||
<greater-than>
|
||||
<property>engines/engine[1]/n1-pct</property>
|
||||
<value>0.1</value>
|
||||
</greater-than>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.03</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>5</factor>
|
||||
</volume>
|
||||
<reference-dist>50</reference-dist>
|
||||
<max-dist>200</max-dist>
|
||||
</engine>
|
||||
|
||||
<engine>
|
||||
<name>turbine1-loop</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/idle_ec135_out.wav</path>
|
||||
<condition>
|
||||
<property>engines/engine[1]/running</property>
|
||||
</condition>
|
||||
<delay-sec>45</delay-sec>
|
||||
<volume>
|
||||
<factor>0.03</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>5</factor>
|
||||
</volume>
|
||||
<reference-dist>50</reference-dist>
|
||||
<max-dist>200</max-dist>
|
||||
</engine>
|
||||
|
||||
<engine>
|
||||
<name>turbine1-shutdown</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/turbine_shutdown.wav</path>
|
||||
<condition>
|
||||
<not>
|
||||
<property>engines/engine[1]/running</property>
|
||||
</not>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.03</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>5</factor>
|
||||
</volume>
|
||||
<reference-dist>50</reference-dist>
|
||||
<max-dist>200</max-dist>
|
||||
</engine>
|
||||
|
||||
|
||||
<rotor>
|
||||
<name>rotor-outside</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/flight_ec135_out.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<not>
|
||||
<property>sim/current-view/internal</property>
|
||||
</not>
|
||||
<greater-than>
|
||||
<property>rotors/main/rpm</property>
|
||||
<value>200</value>
|
||||
</greater-than>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<property>rotors/main/rpm</property>
|
||||
<factor>0.002</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>rotors/main/rpm</property>
|
||||
<factor>0.00252</factor>
|
||||
<offset>0</offset>
|
||||
<min>0</min>
|
||||
<max>1.5</max>
|
||||
</pitch>
|
||||
|
||||
<reference-dist>200</reference-dist>
|
||||
<max-dist>1000</max-dist>
|
||||
</rotor>
|
||||
|
||||
<rotor>
|
||||
<name>rotor-inside</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/rotor.wav</path>
|
||||
<path>Aircraft/ec135/Sounds/ec_rotor_in.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<property>sim/current-view/internal</property>
|
||||
<greater-than>
|
||||
<property>rotors/main/rpm</property>
|
||||
<value>200</value>
|
||||
</greater-than>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.5</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>rotors/main/rpm</property>
|
||||
<factor>0.002</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>rotors/main/rpm</property>
|
||||
<factor>0.00252</factor>
|
||||
<offset>0</offset>
|
||||
<min>0</min>
|
||||
<max>1.5</max>
|
||||
</pitch>
|
||||
<reference-dist>500</reference-dist>
|
||||
<max-dist>1000</max-dist>
|
||||
</rotor>
|
||||
|
||||
<rotor>
|
||||
<name>stall</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/R-1535Slow.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<greater-than>
|
||||
<property>rotors/main/rpm</property>
|
||||
<value>50</value>
|
||||
</greater-than>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/volume</property>
|
||||
<factor>0.8</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>rotors/main/stall-filtered</property>
|
||||
<factor>75</factor>
|
||||
<max>1.0</max>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>rotors/main/rpm</property>
|
||||
<factor>0.00252</factor>
|
||||
<offset>0</offset>
|
||||
<max>1.75</max>
|
||||
</pitch>
|
||||
<reference-dist>500</reference-dist>
|
||||
<max-dist>1500</max-dist>
|
||||
</rotor>
|
||||
|
||||
<rotor>
|
||||
<name>blade-vortex-interaction</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/R-1535Slow.wav</path>
|
||||
<condition>
|
||||
<greater-than>
|
||||
<property>sim/sound/vibration</property>
|
||||
<value>0.01</value>
|
||||
</greater-than>
|
||||
</condition>
|
||||
<volume>
|
||||
<property>sim/sound/vibration</property>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>rotors/main/rpm</property>
|
||||
<factor>0.00252</factor>
|
||||
<offset>0</offset>
|
||||
<min>0</min>
|
||||
<max>1.5</max>
|
||||
</pitch>
|
||||
<reference-dist>500</reference-dist>
|
||||
<max-dist>3000</max-dist>
|
||||
</rotor>
|
||||
|
||||
|
||||
|
||||
<overspeed>
|
||||
<name>overspeed</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/overspeed.wav</path>
|
||||
<condition>
|
||||
<greater-than>
|
||||
<property>velocities/airspeed-kt</property>
|
||||
<value>146</value>
|
||||
</greater-than>
|
||||
<equals>
|
||||
<property>sim/current-view/view-number</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.1</factor>
|
||||
</pitch>
|
||||
<reference-dist>1.0</reference-dist>
|
||||
<max-dist>2.0</max-dist>
|
||||
</overspeed>
|
||||
|
||||
|
||||
|
||||
<warning>
|
||||
<name>650 Hz</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/warn650.wav</path>
|
||||
<condition>
|
||||
<property>sim/sound/warn650</property>
|
||||
</condition>
|
||||
<reference-dist>0.5</reference-dist>
|
||||
<max-dist>1.0</max-dist>
|
||||
</warning>
|
||||
|
||||
<warning>
|
||||
<name>2600 Hz</name>
|
||||
<mode>looped</mode>
|
||||
<path>Aircraft/ec135/Sounds/warn2600.wav</path>
|
||||
<condition>
|
||||
<property>sim/sound/warn2600</property>
|
||||
</condition>
|
||||
<reference-dist>0.5</reference-dist>
|
||||
<max-dist>1.0</max-dist>
|
||||
</warning>
|
||||
|
||||
|
||||
<contact>
|
||||
<name>ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/TC1.wav</path>
|
||||
<condition>
|
||||
<property>gear/gear[0]/wow</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.01</factor>
|
||||
</pitch>
|
||||
<reference-dist>5.0</reference-dist>
|
||||
<max-dist>10.0</max-dist>
|
||||
</contact>
|
||||
|
||||
<contact>
|
||||
<name>ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/TC1.wav</path>
|
||||
<condition>
|
||||
<property>gear/gear[1]/wow</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.01</factor>
|
||||
</pitch>
|
||||
<reference-dist>5.0</reference-dist>
|
||||
<max-dist>10.0</max-dist>
|
||||
</contact>
|
||||
|
||||
<contact>
|
||||
<name>ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/TC1.wav</path>
|
||||
<condition>
|
||||
<property>gear/gear[2]/wow</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.01</factor>
|
||||
</pitch>
|
||||
<reference-dist>5.0</reference-dist>
|
||||
<max-dist>10.0</max-dist>
|
||||
</contact>
|
||||
|
||||
<contact>
|
||||
<name>ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/TC1.wav</path>
|
||||
<condition>
|
||||
<property>gear/gear[3]/wow</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.01</factor>
|
||||
</pitch>
|
||||
<reference-dist>5.0</reference-dist>
|
||||
<max-dist>10.0</max-dist>
|
||||
</contact>
|
||||
|
||||
<contact>
|
||||
<name>ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/TC1.wav</path>
|
||||
<condition>
|
||||
<property>gear/gear[4]/wow</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.01</factor>
|
||||
</pitch>
|
||||
<reference-dist>5.0</reference-dist>
|
||||
<max-dist>10.0</max-dist>
|
||||
</contact>
|
||||
|
||||
<contact>
|
||||
<name>ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Aircraft/ec135/Sounds/TC1.wav</path>
|
||||
<condition>
|
||||
<property>gear/gear[5]/wow</property>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>1.0</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.01</factor>
|
||||
</pitch>
|
||||
<reference-dist>5.0</reference-dist>
|
||||
<max-dist>10.0</max-dist>
|
||||
</contact>
|
||||
|
||||
<slide>
|
||||
<name>skid sliding1</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/rumble.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<property>gear/gear[0]/wow</property>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.5</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/slide[0]/volume</property>
|
||||
<max>1</max>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>sim/model/ec135/sound/slide[0]/pitch</property>
|
||||
</pitch>
|
||||
</slide>
|
||||
|
||||
<slide>
|
||||
<name>skid sliding2</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/rumble.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<property>gear/gear[1]/wow</property>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.5</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/slide[1]/volume</property>
|
||||
<max>1</max>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>sim/model/ec135/sound/slide[1]/pitch</property>
|
||||
</pitch>
|
||||
</slide>
|
||||
|
||||
<slide>
|
||||
<name>skid sliding3</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/rumble.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<property>gear/gear[2]/wow</property>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.5</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/slide[2]/volume</property>
|
||||
<max>1</max>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>sim/model/ec135/sound/slide[2]/pitch</property>
|
||||
</pitch>
|
||||
</slide>
|
||||
|
||||
<slide>
|
||||
<name>skid sliding4</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/rumble.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<property>gear/gear[3]/wow</property>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<factor>0.5</factor>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>sim/model/ec135/sound/slide[3]/volume</property>
|
||||
<max>1</max>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>sim/model/ec135/sound/slide[3]/pitch</property>
|
||||
</pitch>
|
||||
</slide>
|
||||
|
||||
<wind>
|
||||
<name>wind</name>
|
||||
<mode>looped</mode>
|
||||
<path>Sounds/wind.wav</path>
|
||||
<condition>
|
||||
<and>
|
||||
<property>velocities/airspeed-kt</property>
|
||||
<not>
|
||||
<property>sim/crashed</property>
|
||||
</not>
|
||||
</and>
|
||||
</condition>
|
||||
<volume>
|
||||
<property>position/altitude-ft</property>
|
||||
<factor>-0.000015</factor>
|
||||
<offset>1.0</offset>
|
||||
<min>0.1</min>
|
||||
<max>1.0</max>
|
||||
</volume>
|
||||
<volume>
|
||||
<property>velocities/airspeed-kt</property>
|
||||
<factor>0.0015</factor>
|
||||
<min>0.03</min>
|
||||
<max>0.25</max>
|
||||
</volume>
|
||||
<pitch>
|
||||
<property>velocities/airspeed-kt</property>
|
||||
<factor>0.01</factor>
|
||||
<offset>1.25</offset>
|
||||
</pitch>
|
||||
<reference-dist>3</reference-dist>
|
||||
<max-dist>4</max-dist>
|
||||
</wind>
|
||||
|
||||
<crash>
|
||||
<name>intense ground contact</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/crash.wav</path>
|
||||
<property>sim/crashed</property>
|
||||
<volume>
|
||||
<factor>1</factor>
|
||||
</volume>
|
||||
<pitch>
|
||||
<factor>0.1</factor>
|
||||
</pitch>
|
||||
<reference-dist>100</reference-dist>
|
||||
<max-dist>500</max-dist>
|
||||
</crash>
|
||||
|
||||
|
||||
|
||||
<door>
|
||||
<name>close right frontdoor</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/door_close.wav</path>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>sim/model/ec135/doors/door[0]/position-norm</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<position>
|
||||
<x>1.0</x>
|
||||
<y>1.5</y>
|
||||
<z>-1.5</z>
|
||||
</position>
|
||||
<volume>
|
||||
<factor>0.3</factor>
|
||||
</volume>
|
||||
<reference-dist>15</reference-dist>
|
||||
<max-dist>50</max-dist>
|
||||
</door>
|
||||
|
||||
<door>
|
||||
<name>close left frontdoor</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/door_close.wav</path>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>sim/model/ec135/doors/door[1]/position-norm</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<position>
|
||||
<x>-1.0</x>
|
||||
<y>1.5</y>
|
||||
<z>-1.5</z>
|
||||
</position>
|
||||
<volume>
|
||||
<factor>0.3</factor>
|
||||
</volume>
|
||||
<reference-dist>15</reference-dist>
|
||||
<max-dist>50</max-dist>
|
||||
</door>
|
||||
|
||||
<door>
|
||||
<name>close right backdoor</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/door_close.wav</path>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>sim/model/ec135/doors/door[2]/position-norm</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<position>
|
||||
<x>1.0</x>
|
||||
<y>1.0</y>
|
||||
<z>-1.5</z>
|
||||
</position>
|
||||
<volume>
|
||||
<factor>0.3</factor>
|
||||
</volume>
|
||||
<reference-dist>15</reference-dist>
|
||||
<max-dist>50</max-dist>
|
||||
</door>
|
||||
|
||||
<door>
|
||||
<name>close left backdoor</name>
|
||||
<mode>once</mode>
|
||||
<path>Sounds/door_close.wav</path>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>sim/model/ec135/doors/door[3]/position-norm</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<position>
|
||||
<x>-1.0</x>
|
||||
<y>1.0</y>
|
||||
<z>-1.5</z>
|
||||
</position>
|
||||
<volume>
|
||||
<factor>0.3</factor>
|
||||
</volume>
|
||||
<reference-dist>15</reference-dist>
|
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Sounds/starter_stop.wav
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BIN
Sounds/starter_stop.wav
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BIN
Sounds/strt_ec135_out2.wav
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Sounds/strt_ec135_out2.wav
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BIN
Sounds/warn2600.wav
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Sounds/warn2600.wav
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Sounds/warn650.wav
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Sounds/warn650.wav
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instrumentation/FDM1.rgb
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instrumentation/FDM1.rgb
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instrumentation/GH14-391/ai.png
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58
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58
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instrumentation/GH14-391/face.2.png
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instrumentation/GH14-391/face.2.png
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BIN
instrumentation/GH14-391/face.png
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instrumentation/GH14-391/face.png
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After Width: | Height: | Size: 85 KiB |
BIN
instrumentation/GH14-391/face2.png
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instrumentation/GH14-391/face2.png
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15834
instrumentation/GH14-391/gh14391.ac
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15834
instrumentation/GH14-391/gh14391.ac
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1536
instrumentation/ai_small/STBYai.ac
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1536
instrumentation/ai_small/STBYai.ac
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BIN
instrumentation/ai_small/STBYai.png
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instrumentation/ai_small/STBYai.png
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68
instrumentation/ai_small/STBYai.xml
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68
instrumentation/ai_small/STBYai.xml
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instrumentation/ai_small/tach.png
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instrumentation/ai_small/tach.png
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7247
instrumentation/alt/alt2.ac
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7247
instrumentation/alt/alt2.ac
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BIN
instrumentation/alt/altimeter.png
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instrumentation/alt/altimeter.png
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BIN
instrumentation/alt/altimeter.rgb
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159
instrumentation/alt/altimeter.xml
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159
instrumentation/alt/altimeter.xml
Normal file
|
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BIN
instrumentation/alt/vsi.png
Normal file
BIN
instrumentation/alt/vsi.png
Normal file
Binary file not shown.
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After Width: | Height: | Size: 106 KiB |
7247
instrumentation/alt2/alt2.ac
Normal file
7247
instrumentation/alt2/alt2.ac
Normal file
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BIN
instrumentation/alt2/altimeter.png
Normal file
BIN
instrumentation/alt2/altimeter.png
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 151 KiB |
BIN
instrumentation/alt2/altimeter.rgb
Normal file
BIN
instrumentation/alt2/altimeter.rgb
Normal file
Binary file not shown.
159
instrumentation/alt2/altimeter.xml
Normal file
159
instrumentation/alt2/altimeter.xml
Normal file
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instrumentation/clock/clock.xml
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1537
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instrumentation/dme/dme.png
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instrumentation/dme/dme.png
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instrumentation/dme/dme.rgb
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instrumentation/dme/dme.xml
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instrumentation/dme/dme.xml
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<command>property-assign</command>
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<property>instrumentation/dme/frequencies/source</property>
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<value>instrumentation/nav[0]/frequencies/selected-mhz</value>
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<binding>
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7122
instrumentation/engine_panel/engine_panel.ac
Normal file
7122
instrumentation/engine_panel/engine_panel.ac
Normal file
File diff suppressed because it is too large
Load diff
BIN
instrumentation/engine_panel/engine_panel.png
Normal file
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instrumentation/engine_panel/engine_panel.png
Normal file
Binary file not shown.
|
After Width: | Height: | Size: 401 KiB |
14
instrumentation/engine_panel/engine_panel.xml
Normal file
14
instrumentation/engine_panel/engine_panel.xml
Normal file
|
|
@ -0,0 +1,14 @@
|
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<PropertyList>
|
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|
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<object-name>Plane</object-name>
|
||||
|
||||
<emission>
|
||||
<red>0.028</red>
|
||||
<green>0.014</green>
|
||||
<blue>0.007</blue>
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||||
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|
||||
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|
||||
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298
instrumentation/fdm1.ac
Normal file
298
instrumentation/fdm1.ac
Normal file
|
|
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|
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AC3Db
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||||
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||||
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||||
data 4
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fdm1
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<!--
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||||
$Id: hsi-bk-hi.xml,v 1.1 2007/06/03 14:58:44 mfranz Exp $
|
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This is the Bendix/King KI252 HSI 3d instrument.
|
||||
Maintainer: Torsten Dreyer
|
||||
|
||||
$Log: hsi-bk-hi.xml,v $
|
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Revision 1.1 2007/06/03 14:58:44 mfranz
|
||||
Heiko SCHULZ: EC135 v0.2
|
||||
|
||||
Revision 1.2 2006-11-23 14:27:03 mfranz
|
||||
Torsten DREYER:
|
||||
|
||||
"""
|
||||
- Added instruments lights for night flights
|
||||
- Addes flashing strobe effect in clouds at night
|
||||
- OBS knob on vor2 clickable
|
||||
- subscale knob on altimeter clickable
|
||||
- changes on aircraft 3d-model
|
||||
- Fixed bug in HSI, wrong deflection of glideslope indicator and
|
||||
transparency issue
|
||||
- Added Roberto Inzerillo's nice nose gear and animations, new main gear
|
||||
"""
|
||||
|
||||
Revision 1.1 2006-06-01 12:58:33 mfranz
|
||||
Torsten Dreyer: version 0.3 of the PA34-200T Seneca II (2006.05.30)
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<object-name>hsi.NAVFlag</object-name>
|
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<condition>
|
||||
<not>
|
||||
<property>/instrumentation/nav[0]/in-range</property>
|
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</not>
|
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</condition>
|
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</animation>
|
||||
|
||||
<!-- fixme: whould be nicer to have a rotation bound to spin -->
|
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<animation>
|
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<type>select</type>
|
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<object-name>hsi.HDGFlag</object-name>
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<condition>
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<or>
|
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<not>
|
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<property>/instrumentation/heading-indicator/serviceable</property>
|
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</not>
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<less-than>
|
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<property>/instrumentation/heading-indicator/spin</property>
|
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<value type="double">0.9</value>
|
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</less-than>
|
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</or>
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</condition>
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</animation>
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<animation>
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<type>select</type>
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<object-name>hsi.TOFlag</object-name>
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<condition>
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<property>/instrumentation/nav[0]/to-flag</property>
|
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</condition>
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</animation>
|
||||
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<animation>
|
||||
<type>select</type>
|
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<object-name>hsi.FROMFlag</object-name>
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<condition>
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|
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|
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116
instrumentation/instrumentation.xml
Normal file
116
instrumentation/instrumentation.xml
Normal file
|
|
@ -0,0 +1,116 @@
|
|||
<?xml version="1.0"?>
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||||
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<adf>
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<adf>
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|
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|
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|
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<airspeed-indicator>
|
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<name>airspeed-indicator</name>
|
||||
<number>0</number>
|
||||
<pitot-port>/systems/pitot</pitot-port>
|
||||
<static-port>/systems/static</static-port>
|
||||
</airspeed-indicator>
|
||||
|
||||
<altimeter>
|
||||
<name>altimeter</name>
|
||||
<number>0</number>
|
||||
<static-port>/systems/static</static-port>
|
||||
</altimeter>
|
||||
|
||||
<attitude-indicator>
|
||||
<name>attitude-indicator</name>
|
||||
<number>0</number>
|
||||
<vacuum-system>/systems/vacuum</vacuum-system>
|
||||
</attitude-indicator>
|
||||
|
||||
<clock>
|
||||
<name>clock</name>
|
||||
<number>0</number>
|
||||
</clock>
|
||||
|
||||
<dme>
|
||||
<name>dme</name>
|
||||
<number>0</number>
|
||||
</dme>
|
||||
|
||||
<encoder>
|
||||
<name>encoder</name>
|
||||
<number>0</number>
|
||||
<static-port>/systems/static</static-port>
|
||||
</encoder>
|
||||
|
||||
<gsdi>
|
||||
<name>gsdi</name>
|
||||
<number>0</number>
|
||||
</gsdi>
|
||||
|
||||
<marker-beacon>
|
||||
<name>marker-beacon</name>
|
||||
<number>0</number>
|
||||
</marker-beacon>
|
||||
|
||||
<heading-indicator>
|
||||
<name>heading-indicator</name>
|
||||
<number>0</number>
|
||||
<vacuum-system>/systems/vacuum</vacuum-system>
|
||||
</heading-indicator>
|
||||
|
||||
<KT-70>
|
||||
<name>kt-70</name>
|
||||
<number>0</number>
|
||||
</KT-70>
|
||||
|
||||
<magnetic-compass>
|
||||
<name>magnetic-compass</name>
|
||||
<number>0</number>
|
||||
</magnetic-compass>
|
||||
|
||||
<nav-radio>
|
||||
<name>nav</name>
|
||||
<number>0</number>
|
||||
</nav-radio>
|
||||
|
||||
<nav-radio>
|
||||
<name>nav</name>
|
||||
<number>1</number>
|
||||
</nav-radio>
|
||||
|
||||
<slip-skid-ball>
|
||||
<name>slip-skid-ball</name>
|
||||
<number>0</number>
|
||||
</slip-skid-ball>
|
||||
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||||
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|
||||
<name>transponder</name>
|
||||
<number>0</number>
|
||||
<encoder>/instrumentation/encoder</encoder>
|
||||
</transponder>
|
||||
|
||||
<turn-indicator>
|
||||
<name>turn-indicator</name>
|
||||
<number>0</number>
|
||||
</turn-indicator>
|
||||
|
||||
<vertical-speed-indicator>
|
||||
<name>vertical-speed-indicator</name>
|
||||
<number>0</number>
|
||||
<static-port>/systems/static</static-port>
|
||||
</vertical-speed-indicator>
|
||||
|
||||
<gps>
|
||||
<name>gps</name>
|
||||
<number>0</number>
|
||||
</gps>
|
||||
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||||
<tacan>
|
||||
<name>tacan</name>
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||||
<number>0</number>
|
||||
</tacan>
|
||||
</PropertyList>
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instrumentation/kfc200/face.png
Normal file
BIN
instrumentation/kfc200/face.png
Normal file
Binary file not shown.
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467
instrumentation/kfc200/fd-annun.ac
Normal file
467
instrumentation/kfc200/fd-annun.ac
Normal file
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|
@ -0,0 +1,467 @@
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instrumentation/kfc200/fd-annun.xml
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175
instrumentation/kfc200/fd-annun.xml
Normal file
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<?xml version="1.0"?>
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714
instrumentation/kfc200/fd-control.ac
Normal file
714
instrumentation/kfc200/fd-control.ac
Normal file
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@ -0,0 +1,714 @@
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198
instrumentation/kfc200/fd-control.xml
Normal file
198
instrumentation/kfc200/fd-control.xml
Normal file
|
|
@ -0,0 +1,198 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
KFC-200 FlightDirector / Autopilot Controller
|
||||
Syd Adams
|
||||
-->
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||||
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||||
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||||
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<object-name>FDbase</object-name>
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||||
<green>0.014</green>
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||||
<blue>0.007</blue>
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||||
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|
||||
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||||
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|
||||
<!--
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||||
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||||
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||||
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||||
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||||
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||||
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||||
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|
||||
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|
||||
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|
||||
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<command>property-adjust</command>
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<property>/autopilot/settings/target-pitch-deg</property>
|
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|
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|
||||
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|
||||
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|
||||
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|
||||
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|
||||
<min>-15.0</min>
|
||||
<max>15.0</max>
|
||||
<wrap>false</wrap>
|
||||
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|
||||
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|
||||
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|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>HDG.btn</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>nasal</command>
|
||||
<script>
|
||||
if(getprop("/instrumentation/kfc200/fdmode") != "hdg"){
|
||||
setprop("/instrumentation/kfc200/fdmode","hdg");}
|
||||
else{setprop("/instrumentation/kfc200/fdmode","off");}
|
||||
</script>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>FD.btn</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>/instrumentation/kfc200/fd-on</property>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
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|
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|
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<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>nasal</command>
|
||||
<script>
|
||||
if(getprop("/instrumentation/kfc200/fdmodeV") != "alt-arm"){
|
||||
setprop("/instrumentation/kfc200/fdmodeV","alt-arm");}
|
||||
else{setprop("/instrumentation/kfc200/fdmodeV","off");}
|
||||
</script>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>NAV.btn</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>nasal</command>
|
||||
<script>
|
||||
if(getprop("/instrumentation/kfc200/fdmode") != "nav-arm"){
|
||||
setprop("/instrumentation/kfc200/fdmode","nav-arm");}
|
||||
else{setprop("/instrumentation/kfc200/fdmode","off");}
|
||||
</script>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>BC.btn</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>nasal</command>
|
||||
<script>
|
||||
if(getprop("/instrumentation/kfc200/fdmode") != "bc"){
|
||||
setprop("/instrumentation/kfc200/fdmode","bc");}
|
||||
else{setprop("/instrumentation/kfc200/fdmode","off");}
|
||||
</script>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>APPR.btn</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>nasal</command>
|
||||
<script>
|
||||
if(getprop("/instrumentation/kfc200/fdmode") != "appr"){
|
||||
setprop("/instrumentation/kfc200/fdmode","appr");}
|
||||
else{setprop("/instrumentation/kfc200/fdmode","off");}
|
||||
</script>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>APtoggle</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>property-toggle</command>
|
||||
<property>/autopilot/locks/passive-mode</property>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
-->
|
||||
<animation>
|
||||
<type>rotate</type>
|
||||
<object-name>APtoggle</object-name>
|
||||
<property>/autopilot/locks/passive-mode</property>
|
||||
<factor>40</factor>
|
||||
<axis>
|
||||
<x>0.0</x>
|
||||
<y>1.0</y>
|
||||
<z>0.0</z>
|
||||
</axis>
|
||||
<center>
|
||||
<x-m>0.002</x-m>
|
||||
<y-m>0.046</y-m>
|
||||
<z-m>0.002</z-m>
|
||||
</center>
|
||||
</animation>
|
||||
|
||||
</PropertyList>
|
||||
BIN
instrumentation/kfc200/hdg1.rgb
Normal file
BIN
instrumentation/kfc200/hdg1.rgb
Normal file
Binary file not shown.
649
instrumentation/kfc200/kas297.ac
Normal file
649
instrumentation/kfc200/kas297.ac
Normal file
|
|
@ -0,0 +1,649 @@
|
|||
AC3Db
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||||
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||||
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8 0.139534652233 0.0253909472376
|
||||
9 0.139534652233 0.0253906790167
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
2 0.457330524921 0.145992904902
|
||||
6 0.457330405712 0.145992904902
|
||||
11 0.338432312012 0.0253906194121
|
||||
10 0.338432431221 0.0253906790167
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
0 0.020636677742 0.851326823235
|
||||
4 0.020636677742 0.851326942444
|
||||
13 0.139534711838 0.971929192543
|
||||
12 0.139534711838 0.971929192543
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
5 0.45733076334 0.851326525211
|
||||
1 0.457330584526 0.851326823235
|
||||
14 0.338432490826 0.971929192543
|
||||
15 0.338432490826 0.971928715706
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
6 0.457330405712 0.145992904902
|
||||
7 0.0206365585327 0.145992994308
|
||||
9 0.139534652233 0.0253906790167
|
||||
11 0.338432312012 0.0253906194121
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
4 0.020636677742 0.851326942444
|
||||
5 0.45733076334 0.851326525211
|
||||
15 0.338432490826 0.971928715706
|
||||
13 0.139534711838 0.971929192543
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
10 0.338432431221 0.0253906790167
|
||||
11 0.338432312012 0.0253906194121
|
||||
9 0.139534652233 0.0253906790167
|
||||
8 0.139534652233 0.0253909472376
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
12 0.139534711838 0.971929192543
|
||||
13 0.139534711838 0.971929192543
|
||||
15 0.338432490826 0.971928715706
|
||||
14 0.338432490826 0.971929192543
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
5 0.45733076334 0.851326525211
|
||||
4 0.020636677742 0.851326942444
|
||||
16 0.0811778306961 0.71433955431
|
||||
17 0.291848778725 0.714339256287
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
6 0.457330405712 0.145992904902
|
||||
5 0.45733076334 0.851326525211
|
||||
17 0.291848778725 0.714339256287
|
||||
18 0.291848599911 0.242245286703
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
7 0.0206365585327 0.145992994308
|
||||
6 0.457330405712 0.145992904902
|
||||
18 0.291848599911 0.242245286703
|
||||
19 0.0811777710915 0.242245346308
|
||||
SURF 0x00
|
||||
mat 1
|
||||
refs 4
|
||||
4 0.020636677742 0.851326942444
|
||||
7 0.0206365585327 0.145992994308
|
||||
19 0.0811777710915 0.242245346308
|
||||
16 0.0811778306961 0.71433955431
|
||||
kids 0
|
||||
BIN
instrumentation/kfc200/kas297.rgb
Normal file
BIN
instrumentation/kfc200/kas297.rgb
Normal file
Binary file not shown.
229
instrumentation/kfc200/kas297.xml
Normal file
229
instrumentation/kfc200/kas297.xml
Normal file
|
|
@ -0,0 +1,229 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
KAS 297 ALTITUDE SELECTOR
|
||||
Syd Adams
|
||||
|
||||
*** requires kfc200.nas to run ***
|
||||
-->
|
||||
<PropertyList>
|
||||
|
||||
<path>kas297.ac</path>
|
||||
|
||||
<animation>
|
||||
<type>material</type>
|
||||
<object-name>Arm.btn</object-name>
|
||||
<object-name>Set.knob</object-name>
|
||||
<emission>
|
||||
<red>0.028</red>
|
||||
<green>0.014</green>
|
||||
<blue>0.007</blue>
|
||||
<factor-prop>systems/electrical/outputs/instrument-lights</factor-prop>
|
||||
</emission>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>altmsg</object-name>
|
||||
<object-name>altmsg.001</object-name>
|
||||
<object-name>altmsg.002</object-name>
|
||||
<object-name>altmsg.003</object-name>
|
||||
<object-name>altmsg.004</object-name>
|
||||
<condition>
|
||||
<greater-than>
|
||||
<property>systems/electrical/volts</property>
|
||||
<value>1</value>
|
||||
</greater-than>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>Alert.msg</object-name>
|
||||
<condition>
|
||||
<and>
|
||||
<property>/instrumentation/kfc200/alt-alert</property>
|
||||
<greater-than>
|
||||
<property>systems/electrical/volts</property>
|
||||
<value>1</value>
|
||||
</greater-than>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>select</type>
|
||||
<object-name>Arm.msg</object-name>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/instrumentation/kfc200/vnav</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<greater-than>
|
||||
<property>systems/electrical/volts</property>
|
||||
<value>1</value>
|
||||
</greater-than>
|
||||
</and>
|
||||
</condition>
|
||||
</animation>
|
||||
|
||||
<!-- Altitude Select -->
|
||||
|
||||
<animation>
|
||||
<type>textranslate</type>
|
||||
<object-name>altmsg</object-name>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<factor>0.00001</factor>
|
||||
<step>10000</step>
|
||||
<axis>
|
||||
<x>0</x>
|
||||
<y>1</y>
|
||||
<z>0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>textranslate</type>
|
||||
<object-name>altmsg.001</object-name>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<factor>0.0001</factor>
|
||||
<step>1000</step>
|
||||
<axis>
|
||||
<x>0</x>
|
||||
<y>1</y>
|
||||
<z>0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>textranslate</type>
|
||||
<object-name>altmsg.002</object-name>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<factor>0.001</factor>
|
||||
<step>100</step>
|
||||
<axis>
|
||||
<x>0</x>
|
||||
<y>1</y>
|
||||
<z>0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>textranslate</type>
|
||||
<object-name>altmsg.003</object-name>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<factor>0.01</factor>
|
||||
<step>10</step>
|
||||
<axis>
|
||||
<x>0</x>
|
||||
<y>1</y>
|
||||
<z>0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>textranslate</type>
|
||||
<object-name>altmsg.004</object-name>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<factor>0.1</factor>
|
||||
<step>1</step>
|
||||
<axis>
|
||||
<x>0</x>
|
||||
<y>1</y>
|
||||
<z>0</z>
|
||||
</axis>
|
||||
</animation>
|
||||
|
||||
<!-- OSG animations
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>Alt.decrease</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>true</repeatable>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<step>-100</step>
|
||||
<min>0.0</min>
|
||||
<max>99999.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>Alt.decrease</object-name>
|
||||
<action>
|
||||
<button>1</button>
|
||||
<repeatable>true</repeatable>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<step>-1000</step>
|
||||
<min>0.0</min>
|
||||
<max>99999.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>Alt.increase</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>true</repeatable>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<step>100</step>
|
||||
<min>0.0</min>
|
||||
<max>99999.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>Alt.increase</object-name>
|
||||
<action>
|
||||
<button>1</button>
|
||||
<repeatable>true</repeatable>
|
||||
<binding>
|
||||
<command>property-adjust</command>
|
||||
<property>instrumentation/kfc200/alt-preset</property>
|
||||
<step>1000</step>
|
||||
<min>0.0</min>
|
||||
<max>99999.0</max>
|
||||
<wrap>false</wrap>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
|
||||
<animation>
|
||||
<type>pick</type>
|
||||
<object-name>Alt.arm</object-name>
|
||||
<action>
|
||||
<button>0</button>
|
||||
<repeatable>false</repeatable>
|
||||
<binding>
|
||||
<command>nasal</command>
|
||||
<script>
|
||||
if(getprop("instrumentation/kfc200/vnav")!= 1){
|
||||
setprop("instrumentation/kfc200/vnav",1);
|
||||
setprop("autopilot/settings/target-altitude-ft",getprop("instrumentation/kfc200/alt-preset"));
|
||||
}else{
|
||||
setprop("instrumentation/kfc200/vnav",0);
|
||||
}
|
||||
</script>
|
||||
</binding>
|
||||
</action>
|
||||
</animation>
|
||||
-->
|
||||
|
||||
</PropertyList>
|
||||
219
instrumentation/kfc200/kfc-200.nas
Normal file
219
instrumentation/kfc200/kfc-200.nas
Normal file
|
|
@ -0,0 +1,219 @@
|
|||
#### Bendix-King KFC-200 Flight Director ####
|
||||
|
||||
#Buttons
|
||||
# HDG ...heading hold
|
||||
# FD ..... flightdirector on/off
|
||||
# ALT ....altitude arm
|
||||
# NAV ...VOR / LOC arm
|
||||
# BC ....LOC back course
|
||||
# APPR ... LOC / GS arm
|
||||
|
||||
#### lnav ####
|
||||
# 0 = wingleveler
|
||||
# 1 = heading hold
|
||||
# 2 = NAV arm
|
||||
# 3 = NAV cap
|
||||
# 4 = APPR arm
|
||||
# 5 = APPR cap
|
||||
|
||||
#### vnav ####
|
||||
# 0 = pitch hold
|
||||
# 1 = ALT arm
|
||||
# 2 = ALT cap
|
||||
# 3 = GS arm
|
||||
# 4 = GS cap
|
||||
|
||||
var L_list=["wing-leveler","dg-heading-hold","dg-heading-hold","nav1-hold","dg-heading-hold","nav1-hold","dg-heading-hold","nav1-hold"];
|
||||
|
||||
var V_list=["pitch-hold","pitch-hold","altitude-hold","pitch-hold","gs1-hold"];
|
||||
|
||||
var fdprop = props.globals.getNode("/instrumentation/kfc200",1);
|
||||
var lnav = 0;
|
||||
var vnav = 0;
|
||||
var current_alt=0.0;
|
||||
var alt_select = 0.0;
|
||||
var DH = 0;
|
||||
|
||||
var HASGS = "/instrumentation/nav/has-gs";
|
||||
var NAVLOC = "/instrumentation/nav/nav-loc";
|
||||
var NAVDST = "/instrumentation/nav/nav-dist";
|
||||
var NAVRNG = "/instrumentation/nav/in-range";
|
||||
var HDEFL = "/instrumentation/nav/heading-needle-deflection";
|
||||
var GSDEFL = "/instrumentation/nav/gs-needle-deflection";
|
||||
var BC = "/instrumentation/nav/back-course-btn";
|
||||
|
||||
var HDG = props.globals.getNode("/autopilot/locks/heading",1);
|
||||
var ALT = props.globals.getNode("/autopilot/locks/altitude",1);
|
||||
var SPD = props.globals.getNode("/autopilot/locks/speed",1);
|
||||
var SRVC = 0;
|
||||
|
||||
setlistener("/sim/signals/fdm-initialized", func {
|
||||
fdprop.getNode("serviceable",1).setBoolValue(1);
|
||||
fdprop.getNode("armed",1).setBoolValue(0);
|
||||
fdprop.getNode("cpld",1).setBoolValue(0);
|
||||
fdprop.getNode("pitch-trim",1).setIntValue(0);
|
||||
fdprop.getNode("alt-trim",1).setIntValue(0);
|
||||
fdprop.getNode("fd-on",1).setBoolValue(0);
|
||||
fdprop.getNode("gs-arm",1).setBoolValue(0);
|
||||
fdprop.getNode("lnav",1).setValue(0);
|
||||
fdprop.getNode("vnav",1).setValue(0);
|
||||
fdprop.getNode("alt-preset",1).setDoubleValue(0.0);
|
||||
fdprop.getNode("alt-alert",1).setBoolValue(0);
|
||||
fdprop.getNode("dh-alert",1).setBoolValue(0);
|
||||
DH = getprop("/autopilot/route-manager/min-lock-altitude-agl-ft");
|
||||
alt_select = 0;
|
||||
ALT.setValue(V_list[vnav]);
|
||||
HDG.setValue(L_list[lnav]);
|
||||
settimer(update,5);
|
||||
print("KFC-200 ... Check");
|
||||
});
|
||||
|
||||
setlistener("/instrumentation/kfc200/fd-on", func(fd){
|
||||
var fdON = fd.getBoolValue();
|
||||
clear_ap();
|
||||
},0,0);
|
||||
|
||||
setlistener("/autopilot/locks/passive-mode", func(ap){
|
||||
if(!ap.getBoolValue()){
|
||||
setprop("autopilot/settings/target-pitch-deg",getprop("/orientation/pitch-deg"));
|
||||
}
|
||||
},0,0);
|
||||
|
||||
setlistener("/instrumentation/kfc200/serviceable", func(srv){
|
||||
if(srv.getBoolValue()){SRVC=1;
|
||||
}else{
|
||||
SRVC=0;
|
||||
}
|
||||
},0,0);
|
||||
|
||||
setlistener("/autopilot/settings/target-altitude-ft",func(at){
|
||||
alt_select = at.getValue();
|
||||
},0,0);
|
||||
|
||||
setlistener("/autopilot/route-manager/min-lock-altitude-agl-ft",func(dh){
|
||||
DH = dh.getValue();
|
||||
},0,0);
|
||||
|
||||
setlistener("/instrumentation/kfc200/lnav",func(ln){
|
||||
if(SRVC == 0)return;
|
||||
lnav = ln.getValue();
|
||||
|
||||
if(lnav == 4){
|
||||
if(!getprop(NAVLOC)){
|
||||
lnav=2;
|
||||
setprop("/instrumentation/kfc200/lnav",lnav);
|
||||
}else{
|
||||
if(getprop(HASGS)){
|
||||
if(!getprop(BC)){
|
||||
setprop("/instrumentation/kfc200/gs-arm",1);
|
||||
}
|
||||
}
|
||||
}
|
||||
}
|
||||
HDG.setValue(L_list[lnav]);
|
||||
},0,0);
|
||||
|
||||
setlistener("/instrumentation/kfc200/vnav", func(vn){
|
||||
if(SRVC == 0)return;
|
||||
vnav = vn.getValue();
|
||||
ALT.setValue(V_list[vnav]);
|
||||
},0,0);
|
||||
|
||||
var clear_ap = func {
|
||||
setprop("/autopilot/settings/target-pitch-deg",getprop("/orientation/pitch-deg"));
|
||||
vnav = 0;
|
||||
lnav=0;
|
||||
setprop("/instrumentation/kfc200/lnav",lnav);
|
||||
setprop("/instrumentation/kfc200/vnav",vnav);
|
||||
HDG.setValue(L_list[lnav]);
|
||||
ALT.setValue(V_list[vnav]);
|
||||
}
|
||||
|
||||
#### PITCH TRIM = 1 degree per second ####
|
||||
var pitch_trim = func {
|
||||
var temp_pitch = getprop("autopilot/settings/target-pitch-deg");
|
||||
var FR =getprop("sim/frame-rate");
|
||||
if(FR > 0){
|
||||
var trim = (1/FR) * arg[0];
|
||||
setprop("autopilot/settings/target-pitch-deg",temp_pitch + trim);
|
||||
}
|
||||
}
|
||||
|
||||
#### ALTITUDE TRIM = 600 fpm ####
|
||||
var alt_trim = func {
|
||||
var temp_alt = getprop("autopilot/settings/target-altitude-ft");
|
||||
var FR =getprop("sim/frame-rate");
|
||||
if(FR > 0){
|
||||
var trim = (10/FR) * arg[0];
|
||||
setprop("autopilot/settings/target-altitude-ft",temp_alt + trim);
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
|
||||
|
||||
var update_nav = func {
|
||||
if(SRVC == 1){
|
||||
var inrange= getprop(NAVRNG);
|
||||
|
||||
if(inrange){
|
||||
|
||||
if(lnav == 2 or lnav == 4){
|
||||
setprop("instrumentation/kfc200/armed",1);
|
||||
setprop("instrumentation/kfc200/cpld",0);
|
||||
var DF = getprop(HDEFL);
|
||||
if(DF > -9 and DF < 9){
|
||||
setprop("/instrumentation/kfc200/lnav",lnav + 1);
|
||||
setprop("instrumentation/kfc200/armed",0);
|
||||
setprop("instrumentation/kfc200/cpld",1);
|
||||
}
|
||||
}
|
||||
|
||||
if(lnav ==5){
|
||||
if(getprop("instrumentation/kfc200/gs-arm")){
|
||||
if(getprop("instrumentation/nav/gs-distance") < 25000){
|
||||
var GS1 = getprop(GSDEFL);
|
||||
if( GS1< 1.0 and GS1 > -1.0){vnav = 4;
|
||||
setprop("/instrumentation/kfc200/vnav",vnav);
|
||||
}
|
||||
}
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
if(vnav == 1){
|
||||
var offset = get_altoffset();
|
||||
if(offset > -990 and offset < 990){
|
||||
setprop("/instrumentation/kfc200/vnav",vnav + 1);
|
||||
}
|
||||
}
|
||||
|
||||
}
|
||||
}
|
||||
|
||||
var get_altoffset = func(){
|
||||
current_alt = getprop("/instrumentation/altimeter/pressure-alt-ft");
|
||||
var offset = (current_alt - alt_select);
|
||||
var alert =0;
|
||||
if(offset > -1000 and offset < -1000){
|
||||
if(offset < -300 and offset > 300)alert = 1;
|
||||
}
|
||||
fdprop.getNode("alt-alert").setBoolValue(alert);
|
||||
return(offset);
|
||||
}
|
||||
|
||||
var update = func {
|
||||
var PT = getprop("instrumentation/kfc200/pitch-trim");
|
||||
var AT = getprop("instrumentation/kfc200/alt-trim");
|
||||
if(PT !=0)pitch_trim(PT);
|
||||
if(AT!=0)alt_trim(AT);
|
||||
if(getprop("/position/altitude-agl-ft") < DH){
|
||||
props.globals.getNode("/autopilot/locks/passive-mode").setBoolValue(1);
|
||||
setprop("instrumentation/kfc200/dh-alert",1);
|
||||
}else{
|
||||
setprop("instrumentation/kfc200/dh-alert",0);
|
||||
}
|
||||
update_nav();
|
||||
settimer(update, 0);
|
||||
}
|
||||
|
||||
2116
instrumentation/kfc200/kfc200.ac
Normal file
2116
instrumentation/kfc200/kfc200.ac
Normal file
File diff suppressed because it is too large
Load diff
BIN
instrumentation/kfc200/kfc200.rgb
Normal file
BIN
instrumentation/kfc200/kfc200.rgb
Normal file
Binary file not shown.
Some files were not shown because too many files have changed in this diff Show more
Loading…
Reference in a new issue