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Merge branch 'master' of git://gitorious.org/fg/fgdata

This commit is contained in:
unknown 2010-06-04 19:17:21 +02:00
commit 0b496c3708
140 changed files with 86209 additions and 120 deletions

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#disable cas when engines running- otherwise we are overflooded with error messages in the console
call_casdisable = func {
if ( getprop("/rotors/main/rpm")> 80.0)
{
setprop("/controls/flight/fcs/cas-enabled", 0);
} else {
setprop("/controls/flight/fcs/cas-enabled", 1.0);
}
#if (RUN2 ==1) {
# setprop("/controls/flight/fcs/cas-enabled", 0);
# } else {
# setprop("/controls/flight/fcs/cas-enabled", 1.0);
# }
settimer(call_casdisable, 0.2);
}
init = func {
settimer(call_casdisable, 0.0);
}
init();

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#
# Flight Control System by Tatsuhiro Nishioka
# $Id: fcs.nas,v 1.11 2008/08/28 02:41:04 tat Exp $
#
#This one simulates a 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, '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);

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#
# 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);

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@ -1,120 +1,118 @@
// -*- mode: C; -*- // -*- mode: C; -*-
// Licence: GPL v2 // Licence: GPL v2
// Author: Vivian Meazza. // Author: Vivian Meazza.
#version 120 #version 120
varying vec4 rawpos; varying vec4 rawpos;
varying vec4 ecPosition; varying vec4 ecPosition;
varying vec3 VNormal; varying vec3 VNormal;
varying vec3 Normal; varying vec3 Normal;
varying vec4 constantColor; varying vec4 constantColor;
varying vec3 vViewVec; varying vec3 vViewVec;
varying vec3 reflVec; varying vec3 reflVec;
varying vec4 Diffuse; varying vec4 Diffuse;
varying vec3 lightDir, halfVector; varying vec3 lightDir, halfVector;
varying float alpha, fogCoord; varying float alpha, fogCoord;
uniform samplerCube Environment; uniform samplerCube Environment;
uniform sampler2D Rainbow; uniform sampler2D Rainbow;
uniform sampler2D BaseTex; uniform sampler2D BaseTex;
uniform sampler2D Fresnel; uniform sampler2D Fresnel;
uniform sampler2D Map; uniform sampler2D Map;
uniform sampler3D Noise; uniform sampler3D Noise;
uniform float refl_correction; uniform float refl_correction;
uniform float rainbowiness; uniform float rainbowiness;
uniform float fresneliness; uniform float fresneliness;
uniform float noisiness; uniform float noisiness;
uniform float ambient_correction; uniform float ambient_correction;
uniform float reflect_map; uniform float reflect_map;
void main (void) void main (void)
{ {
if (!gl_FrontFacing) discard; vec3 n, halfV;
float NdotL, NdotHV;
vec3 n, halfV; vec4 color = constantColor;
float NdotL, NdotHV; vec4 specular = vec4(0.0);
vec4 color = constantColor; n = VNormal;
vec4 specular = vec4(0.0); NdotL = max(0.0, dot(n, lightDir));
n = VNormal;
NdotL = max(0.0, dot(n, lightDir)); // calculate the specular light
if (NdotL > 0.0) {
// calculate the specular light color += Diffuse * NdotL;
if (NdotL > 0.0) { halfV = normalize(halfVector);
color += Diffuse * NdotL; NdotHV = max(dot(n, halfV), 0.0);
halfV = normalize(halfVector); if (gl_FrontMaterial.shininess > 0.0)
NdotHV = max(dot(n, halfV), 0.0); specular.rgb = (gl_FrontMaterial.specular.rgb
if (gl_FrontMaterial.shininess > 0.0) * gl_LightSource[0].specular.rgb
specular.rgb = (gl_FrontMaterial.specular.rgb * pow(NdotHV, gl_FrontMaterial.shininess));
* gl_LightSource[0].specular.rgb }
* pow(NdotHV, gl_FrontMaterial.shininess));
} color.a = alpha;
color = clamp(color, 0.0, 1.0);
color.a = alpha; vec4 texel = texture2D(BaseTex, gl_TexCoord[0].st);
color = clamp(color, 0.0, 1.0); vec4 texelcolor = color * texel + specular;
vec4 texel = texture2D(BaseTex, gl_TexCoord[0].st);
vec4 texelcolor = color * texel + specular; // calculate the fog factor
float fogCoord = ecPosition.z;
// calculate the fog factor const float LOG2 = 1.442695;
float fogCoord = ecPosition.z; float fogFactor = exp2(-gl_Fog.density * gl_Fog.density * fogCoord * fogCoord * LOG2);
const float LOG2 = 1.442695; fogFactor = clamp(fogFactor, 0.0, 1.0);
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;
if(gl_Fog.density == 1.0)
fogFactor=1.0; vec3 normal = normalize(VNormal);
vec3 viewVec = normalize(vViewVec);
vec3 normal = normalize(VNormal);
vec3 viewVec = normalize(vViewVec); // Map a rainbowish color
float v = dot(viewVec, normal);
// Map a rainbowish color vec4 rainbow = texture2D(Rainbow, vec2(v, 0.0));
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 a fresnel effect
vec4 fresnel = texture2D(Fresnel, vec2(v, 0.0)); // map the refection of the environment
vec4 reflection = textureCube(Environment, reflVec);
// 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);
// set the user shininess offse float reflFactor = 0.0;
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
if(reflect_map > 0){ vec4 map = texture2D(Map, gl_TexCoord[0].st);
// map the shininess of the object with user input //float pam = (map.a * -2) + 1; //reverse map
vec4 map = texture2D(Map, gl_TexCoord[0].st); reflFactor = map.a + transparency_offset;
//float pam = (map.a * -2) + 1; //reverse map } else {
reflFactor = map.a + transparency_offset; // set the reflectivity proportional to shininess with user
} else { // input
// set the reflectivity proportional to shininess with user reflFactor = (gl_FrontMaterial.shininess / 128) + transparency_offset;
// input }
reflFactor = (gl_FrontMaterial.shininess / 128) + transparency_offset;
} reflFactor = clamp(reflFactor, 0.0, 1.0);
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);
// set ambient adjustment to remove bluiness with user input vec4 ambient_Correction = vec4(gl_LightSource[0].ambient.rg, gl_LightSource[0].ambient.b * 0.6, 0.5) * ambient_offset ;
float ambient_offset = clamp(ambient_correction, -1.0, 1.0); ambient_Correction = 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);
// 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);
// add fringing fresnel and rainbow effects and modulate by reflection vec4 reflfrescolor = mix(reflcolor, fresnel, fresneliness * v);
vec4 reflcolor = mix(reflection, rainbow, rainbowiness * v); vec4 noisecolor = mix(reflfrescolor, noisevec, noisiness);
vec4 reflfrescolor = mix(reflcolor, fresnel, fresneliness * v); vec4 raincolor = vec4(noisecolor.rgb, 1.0) * reflFactor;
vec4 noisecolor = mix(reflfrescolor, noisevec, noisiness);
vec4 raincolor = vec4(noisecolor.rgb, 1.0) * reflFactor; vec4 mixedcolor = mix(texel, raincolor, reflFactor);
vec4 mixedcolor = mix(texel, raincolor, reflFactor); // the final reflection
vec4 reflColor = color * mixedcolor + specular + ambient_Correction ;
// the final reflection reflColor = clamp(reflColor, 0.0, 1.0);
vec4 reflColor = color * mixedcolor + specular + ambient_Correction ;
reflColor = clamp(reflColor, 0.0, 1.0); gl_FragColor = mix(gl_Fog.color, reflColor, fogFactor);
}
gl_FragColor = mix(gl_Fog.color, reflColor, fogFactor);
}

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<?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>
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Maintainer: Torsten Dreyer
-->
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<property alias="../../params/power-btn"/>
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<axis>
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<?xml version="1.0" ?>
<!--
$Id: hsi-bk-hi.xml,v 1.1 2007/06/03 14:58:44 mfranz Exp $
This is the Bendix/King KI252 HSI 3d instrument.
Maintainer: Torsten Dreyer
$Log: hsi-bk-hi.xml,v $
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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<!--
<factor>0.022420</factor>
-->
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<!-- fixme: whould be nicer to have a rotation bound to spin -->
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View file

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KA 285 Mode Annunciator Panel
Syd Adams
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View file

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View file

@ -0,0 +1,198 @@
<?xml version="1.0"?>
<!--
KFC-200 FlightDirector / Autopilot Controller
Syd Adams
-->
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<animation>
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<object-name>FDbase</object-name>
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</animation>
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<type>pick</type>
<object-name>Pitch.down</object-name>
<condition>
<not-equals>
<property>/autopilot/locks/altitude</property>
<value></value>
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<action>
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<repeatable>true</repeatable>
<interval-sec>0.1</interval-sec>
<binding>
<command>property-adjust</command>
<property>/autopilot/settings/target-pitch-deg</property>
<step>-0.05</step>
<min>-15.0</min>
<max>15.0</max>
<wrap>false</wrap>
</binding>
</action>
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<condition>
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<repeatable>true</repeatable>
<interval-sec>0.1</interval-sec>
<binding>
<command>property-adjust</command>
<property>/autopilot/settings/target-pitch-deg</property>
<step>0.05</step>
<min>-15.0</min>
<max>15.0</max>
<wrap>false</wrap>
</binding>
</action>
</animation>
<animation>
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<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");}
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</binding>
</action>
</animation>
<animation>
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<object-name>FD.btn</object-name>
<action>
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<binding>
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<property>/instrumentation/kfc200/fd-on</property>
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</action>
</animation>
<animation>
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<object-name>ALT.btn</object-name>
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if(getprop("/instrumentation/kfc200/fdmodeV") != "alt-arm"){
setprop("/instrumentation/kfc200/fdmodeV","alt-arm");}
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if(getprop("/instrumentation/kfc200/fdmode") != "nav-arm"){
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</action>
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if(getprop("/instrumentation/kfc200/fdmode") != "bc"){
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</action>
</animation>
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<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>
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<repeatable>false</repeatable>
<binding>
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<property>/autopilot/locks/passive-mode</property>
</binding>
</action>
</animation>
-->
<animation>
<type>rotate</type>
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<axis>
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<center>
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<y-m>0.046</y-m>
<z-m>0.002</z-m>
</center>
</animation>
</PropertyList>

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@ -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>

View 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);
}

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