Merge branch 'master' of https://github.com/it0uchpods/IDG-A32X into Lower-ECAM
This commit is contained in:
Jonathan Redpath
commit
59accc88a5
35 changed files with 2370 additions and 639 deletions
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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|||
</ground_reactions>
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||||
|
||||
<propulsion>
|
||||
<engine file="cfm56_5a1">
|
||||
<engine file="cfm56_5a1_1">
|
||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
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||||
<y> -5.755 </y>
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||||
|
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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|||
</thruster>
|
||||
</engine>
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||||
|
||||
<engine file="cfm56_5a1">
|
||||
<engine file="cfm56_5a1_2">
|
||||
<location unit="M">
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||||
<x> 14.3962788 </x>
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||||
<y> 5.755 </y>
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||||
|
|
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|||
|
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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|||
</ground_reactions>
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||||
|
||||
<propulsion>
|
||||
<engine file="cfm56_5b4">
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||||
<engine file="cfm56_5b4_1">
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||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
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||||
<y> -5.755 </y>
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||||
|
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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|||
</thruster>
|
||||
</engine>
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||||
|
||||
<engine file="cfm56_5b4">
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||||
<engine file="cfm56_5b4_2">
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||||
<location unit="M">
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||||
<x> 14.3962788 </x>
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||||
<y> 5.755 </y>
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||||
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|
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|||
|
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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|||
</ground_reactions>
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||||
|
||||
<propulsion>
|
||||
<engine file="v2527_a5">
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||||
<engine file="v2527_a5_1">
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||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
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||||
<y> -5.755 </y>
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||||
|
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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|||
</thruster>
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||||
</engine>
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||||
|
||||
<engine file="v2527_a5">
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||||
<engine file="v2527_a5_2">
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||||
<location unit="M">
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||||
<x> 14.3962788 </x>
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||||
<y> 5.755 </y>
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||||
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|||
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@ -997,8 +997,20 @@
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|||
</mouse>
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||||
</mice>
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||||
<keyboard>
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||||
<key n="4">
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||||
<name>CTRL-d</name>
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||||
<desc>Autothrottle Disconnect</desc>
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||||
<binding>
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||||
<command>nasal</command>
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||||
<script>
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||||
if (getprop("/it-autoflight/output/athr") == 1) {
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setprop("/it-autoflight/input/athr", 0);
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||||
}
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||||
</script>
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||||
</binding>
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||||
</key>
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||||
<key n="24">
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||||
<name>Ctrl-X</name>
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<name>Ctrl-x</name>
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||||
<desc>Reset zoom to default</desc>
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||||
<binding>
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||||
<command>nasal</command>
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||||
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@ -1226,6 +1238,21 @@
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</script>
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</binding>
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||||
</key>
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||||
<key n="68">
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<name>D</name>
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<desc>Autopilot Disconnect</desc>
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||||
<binding>
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||||
<command>nasal</command>
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||||
<script>
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||||
if (getprop("/it-autoflight/output/ap1") == 1) {
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||||
setprop("/it-autoflight/input/ap1", 0);
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||||
}
|
||||
if (getprop("/it-autoflight/output/ap2") == 1) {
|
||||
setprop("/it-autoflight/input/ap2", 0);
|
||||
}
|
||||
</script>
|
||||
</binding>
|
||||
</key>
|
||||
<key n="88">
|
||||
<name>X</name>
|
||||
<desc>Increase field of view</desc>
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||||
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|||
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
</ground_reactions>
|
||||
|
||||
<propulsion>
|
||||
<engine file="leap1a26">
|
||||
<engine file="leap1a26_1">
|
||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
|
||||
<y> -5.755 </y>
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||||
|
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
</thruster>
|
||||
</engine>
|
||||
|
||||
<engine file="leap1a26">
|
||||
<engine file="leap1a26_2">
|
||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
|
||||
<y> 5.755 </y>
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||||
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|
|||
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
</ground_reactions>
|
||||
|
||||
<propulsion>
|
||||
<engine file="pw1127g">
|
||||
<engine file="pw1127g_1">
|
||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
|
||||
<y> -5.755 </y>
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||||
|
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
|||
</thruster>
|
||||
</engine>
|
||||
|
||||
<engine file="pw1127g">
|
||||
<engine file="pw1127g_2">
|
||||
<location unit="M">
|
||||
<x> 14.3962788 </x>
|
||||
<y> 5.755 </y>
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||||
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@ -126,9 +126,9 @@ setlistener("/systems/acconfig/new-revision", func {
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});
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var mismatch_chk = func {
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if (num(string.replace(getprop("/sim/version/flightgear"),".","")) < 201730) {
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||||
if (num(string.replace(getprop("/sim/version/flightgear"),".","")) < 201810) {
|
||||
setprop("/systems/acconfig/mismatch-code", "0x121");
|
||||
setprop("/systems/acconfig/mismatch-reason", "FGFS version is too old! Please update FlightGear to at least 2017.3.0.");
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||||
setprop("/systems/acconfig/mismatch-reason", "FGFS version is too old! Please update FlightGear to at least 2018.1.0.");
|
||||
if (getprop("/systems/acconfig/out-of-date") != 1) {
|
||||
error_mismatch.open();
|
||||
}
|
||||
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@ -344,14 +344,14 @@ var taxi = func {
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|||
setprop("/controls/APU/master", 1);
|
||||
setprop("/controls/APU/start", 1);
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||||
var apu_rpm_chk = setlistener("/systems/apu/rpm", func {
|
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if (getprop("/systems/apu/rpm") >= 99) {
|
||||
if (getprop("/systems/apu/rpm") >= 98) {
|
||||
removelistener(apu_rpm_chk);
|
||||
taxi_b();
|
||||
}
|
||||
});
|
||||
}
|
||||
var taxi_b = func {
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||||
# Continue with engine start prep, and start engine 2.
|
||||
# Continue with engine start prep, and start engines.
|
||||
setprop("/controls/fuel/tank0pump1", 1);
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||||
setprop("/controls/fuel/tank0pump2", 1);
|
||||
setprop("/controls/fuel/tank1pump1", 1);
|
||||
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|
|||
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@ -96,6 +96,10 @@
|
|||
<halign>left</halign>
|
||||
<label>F2 - Engage/Increase Reverse Thrust</label>
|
||||
</text>
|
||||
<text>
|
||||
<halign>left</halign>
|
||||
<label>DEL - Toggle Reverse Thrust</label>
|
||||
</text>
|
||||
<text>
|
||||
<halign>left</halign>
|
||||
<label>E - Set Idle Thrust</label>
|
||||
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@ -104,10 +108,6 @@
|
|||
<halign>left</halign>
|
||||
<label>F - Set TOGA Thrust</label>
|
||||
</text>
|
||||
<text>
|
||||
<halign>left</halign>
|
||||
<label>DEL - Toggle Reverse Thrust</label>
|
||||
</text>
|
||||
<text>
|
||||
<halign>left</halign>
|
||||
<label>CTRL + B - Cycle Spoilers</label>
|
||||
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@ -116,6 +116,14 @@
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|||
<halign>left</halign>
|
||||
<label>SHIFT + B - Toggle Parking Brake</label>
|
||||
</text>
|
||||
<text>
|
||||
<halign>left</halign>
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||||
<label>CTRL + D - Disconnect Autothrottle</label>
|
||||
</text>
|
||||
<text>
|
||||
<halign>left</halign>
|
||||
<label>SHIFT + D - Disconnect Autopilot</label>
|
||||
</text>
|
||||
|
||||
</group>
|
||||
|
||||
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|
|||
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@ -396,7 +396,7 @@
|
|||
</checkbox>
|
||||
|
||||
<checkbox>
|
||||
<label>Skip ADIRS Alignment</label>
|
||||
<label>ADIRS Aligns Instantly</label>
|
||||
<halign>left</halign>
|
||||
<property>/controls/adirs/skip</property>
|
||||
<binding>
|
||||
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|
|
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@ -104,7 +104,9 @@
|
|||
<command>nasal</command>
|
||||
<script>
|
||||
if (getprop("/systems/acconfig/mismatch-code") == "0x000") {
|
||||
acconfig.welcome_dlg.open();
|
||||
if (getprop("/systems/acconfig/options/welcome-skip") != 1) {
|
||||
acconfig.welcome_dlg.open();
|
||||
}
|
||||
} else {
|
||||
acconfig.error_mismatch.open();
|
||||
}
|
||||
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|
|
|||
|
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@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5A1">
|
||||
|
||||
<milthrust> 25000 </milthrust>
|
||||
<bypassratio> 8.1 </bypassratio>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/cfm56_5a1_1.xml
Normal file
118
Engines/cfm56_5a1_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5A1">
|
||||
|
||||
<milthrust> 25000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/cfm56_5a1_2.xml
Normal file
118
Engines/cfm56_5a1_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5A1">
|
||||
|
||||
<milthrust> 25000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5B4">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<bypassratio> 8.1 </bypassratio>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/cfm56_5b4_1.xml
Normal file
118
Engines/cfm56_5b4_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5B4">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/cfm56_5b4_2.xml
Normal file
118
Engines/cfm56_5b4_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5B4">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="LEAP1A26">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<bypassratio> 8.1 </bypassratio>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/leap1a26_1.xml
Normal file
118
Engines/leap1a26_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="LEAP1A26">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/leap1a26_2.xml
Normal file
118
Engines/leap1a26_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="LEAP1A26">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="PW1127G">
|
||||
|
||||
<milthrust> 26345 </milthrust>
|
||||
<bypassratio> 8.1 </bypassratio>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/pw1127g_1.xml
Normal file
118
Engines/pw1127g_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="PW1127G">
|
||||
|
||||
<milthrust> 26345 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/pw1127g_2.xml
Normal file
118
Engines/pw1127g_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="PW1127G">
|
||||
|
||||
<milthrust> 26345 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="V2527_A5">
|
||||
|
||||
<milthrust> 26600 </milthrust>
|
||||
<bypassratio> 8.1 </bypassratio>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/v2527_a5_1.xml
Normal file
118
Engines/v2527_a5_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="V2527_A5">
|
||||
|
||||
<milthrust> 26600 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
118
Engines/v2527_a5_2.xml
Normal file
118
Engines/v2527_a5_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="V2527_A5">
|
||||
|
||||
<milthrust> 26600 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N1SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="N2SpoolDown">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
|
||||
<tableData>
|
||||
24 1.1
|
||||
28 2.9
|
||||
46 9.7
|
||||
68 15.4
|
||||
80 19.6
|
||||
94 21.4
|
||||
103 23.6
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="IdleThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
|
||||
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
|
||||
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
|
||||
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
|
||||
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
|
||||
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
<function name="MilThrust">
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
|
||||
<tableData>
|
||||
-10000 0 10000 20000 30000 40000 50000
|
||||
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
|
||||
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
|
||||
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
|
||||
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
|
||||
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
|
||||
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
|
||||
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
|
||||
1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
||||
</turbine_engine>
|
||||
|
|
@ -1,7 +1,7 @@
|
|||
# INSTALL
|
||||
## Prerequisites
|
||||
Have at least following versions installed:
|
||||
* FlightGear 2017.3.0 or newer
|
||||
* FlightGear 2018.1.0 or newer
|
||||
|
||||
## Install using ZIP Snapshot
|
||||
[Download](https://github.com/it0uchpods/IDG-A32X/archive/master.zip) the zip file.
|
||||
|
|
|
|||
|
|
@ -1,5 +1,5 @@
|
|||
<!-- Provide a general summary of the issue/question in the title above. -->
|
||||
<!-- Incase of a question, remove the format below, and write your question. -->
|
||||
<!-- Provide a general summary of the issue in the title above. -->
|
||||
<!-- Issues are for reporting bugs or problems only. If you have a feature request, please write in the forums. -->
|
||||
|
||||
### Expected Behavior
|
||||
<!-- Tell us what should happen. -->
|
||||
|
|
@ -16,4 +16,4 @@
|
|||
1.
|
||||
2.
|
||||
3.
|
||||
4.
|
||||
4.
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||||
|
|
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||||
-0.01286 -0.12505 -0.02817
|
||||
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|
||||
-0.01017 -0.12355 -0.02817
|
||||
-0.00919 -0.123 -0.02704
|
||||
-0.01081 -0.11532 -0.02262
|
||||
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|
||||
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|
||||
-0.01518 -0.11776 -0.01973
|
||||
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|
||||
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|
||||
-0.02022 -0.12057 -0.0255
|
||||
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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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|
||||
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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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|
||||
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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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|
||||
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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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|
||||
-0.02276 -0.11 -0.0255
|
||||
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|
||||
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|
||||
-0.02028 -0.10862 -0.02835
|
||||
-0.01903 -0.10792 -0.02797
|
||||
-0.01812 -0.10742 -0.02692
|
||||
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|
||||
-0.01905 -0.10535 -0.02545
|
||||
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|
||||
-0.02148 -0.1067 -0.02267
|
||||
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|
||||
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|
||||
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|
||||
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|
||||
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|
||||
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|
||||
-0.02027 -0.10603 -0.02786
|
||||
-0.01938 -0.10553 -0.02685
|
||||
-0.00735 -0.13178 -0.02549
|
||||
-0.01996 -0.10284 -0.02351
|
||||
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|
||||
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|
||||
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|
||||
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|
||||
-0.02556 -0.10596 -0.02351
|
||||
-0.02599 -0.1062 -0.02536
|
||||
-0.02556 -0.10596 -0.02721
|
||||
-0.02437 -0.1053 -0.02856
|
||||
-0.02276 -0.1044 -0.02906
|
||||
-0.02114 -0.1035 -0.02856
|
||||
-0.01996 -0.10284 -0.02721
|
||||
-0.02026 -0.10024 -0.0183
|
||||
-0.02737 -0.1042 -0.0183
|
||||
-0.02382 -0.10222 -0.01721
|
||||
-0.01953 -0.09978 -0.02124
|
||||
-0.02997 -0.10564 -0.02128
|
||||
-0.01953 -0.09977 -0.02529
|
||||
-0.03092 -0.10618 -0.02535
|
||||
-0.01952 -0.09981 -0.02953
|
||||
-0.02997 -0.10564 -0.02941
|
||||
-0.02026 -0.10024 -0.03239
|
||||
-0.02737 -0.1042 -0.03239
|
||||
-0.02382 -0.10222 -0.03348
|
||||
-0.03403 -0.10787 -0.03363
|
||||
-0.01949 -0.09977 -0.01706
|
||||
-0.03403 -0.10787 -0.01706
|
||||
-0.01949 -0.09977 -0.03363
|
||||
-0.02008 -0.09871 -0.01706
|
||||
-0.03462 -0.10682 -0.01706
|
||||
-0.02008 -0.09871 -0.03363
|
||||
-0.03462 -0.10682 -0.03363
|
||||
-0.02089 -0.09783 -0.03335
|
||||
-0.03495 -0.10566 -0.01734
|
||||
-0.02089 -0.09783 -0.01734
|
||||
-0.03495 -0.10566 -0.03335
|
||||
numsurf 166
|
||||
SURF 0X10
|
||||
mat 7
|
||||
|
|
@ -380945,6 +380945,13 @@ refs 4
|
|||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
164 0.634061 0.764246
|
||||
162 0.50671 0.764246
|
||||
166 0.512828 0.762086
|
||||
168 0.627943 0.762086
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
109 0.723479 0.793684
|
||||
119 0.720759 0.792297
|
||||
131 0.710471 0.792616
|
||||
|
|
@ -381213,73 +381220,66 @@ refs 4
|
|||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
164 0.626892 0.764246
|
||||
162 0.504196 0.764246
|
||||
166 0.510314 0.762086
|
||||
168 0.620774 0.762086
|
||||
157 0.634061 0.760429
|
||||
159 0.50671 0.760429
|
||||
162 0.50671 0.764246
|
||||
164 0.634061 0.764246
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
157 0.626892 0.760429
|
||||
159 0.504196 0.760429
|
||||
162 0.504196 0.764246
|
||||
164 0.626892 0.764246
|
||||
157 0.515068 0.876908
|
||||
164 0.515068 0.880725
|
||||
163 0.515068 0.762765
|
||||
160 0.515068 0.758942
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
157 0.511508 0.876457
|
||||
164 0.507637 0.876457
|
||||
163 0.507634 0.764239
|
||||
160 0.511509 0.764238
|
||||
161 0.511738 0.762765
|
||||
162 0.511738 0.880725
|
||||
159 0.511738 0.876908
|
||||
158 0.511738 0.758942
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
161 0.508386 0.765279
|
||||
162 0.508386 0.883239
|
||||
159 0.508386 0.879422
|
||||
158 0.508386 0.761456
|
||||
165 0.49663 0.515047
|
||||
168 0.49663 0.621305
|
||||
166 0.381514 0.621305
|
||||
167 0.381514 0.515047
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
165 0.491231 0.515047
|
||||
168 0.491231 0.618645
|
||||
166 0.380771 0.618645
|
||||
167 0.380771 0.515047
|
||||
157 0.232288 0.59531
|
||||
160 0.232288 0.528131
|
||||
158 0.159764 0.528131
|
||||
159 0.159764 0.59531
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
157 0.228416 0.594634
|
||||
160 0.228416 0.530919
|
||||
158 0.162147 0.530919
|
||||
159 0.162147 0.594634
|
||||
161 0.508613 0.857564
|
||||
163 0.508613 0.753809
|
||||
165 0.511589 0.758982
|
||||
167 0.511589 0.85239
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
161 0.50774 0.856869
|
||||
163 0.50774 0.75693
|
||||
165 0.511416 0.761914
|
||||
167 0.511416 0.851886
|
||||
163 0.515068 0.762765
|
||||
164 0.515068 0.880725
|
||||
168 0.50895 0.878565
|
||||
165 0.50895 0.772307
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
163 0.512741 0.758852
|
||||
164 0.512741 0.876812
|
||||
168 0.506623 0.874652
|
||||
165 0.506623 0.768394
|
||||
166 0.517856 0.878565
|
||||
162 0.511738 0.880725
|
||||
161 0.511738 0.762765
|
||||
167 0.517856 0.772307
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
166 0.514504 0.881079
|
||||
162 0.508386 0.883239
|
||||
161 0.508386 0.765279
|
||||
167 0.514504 0.774821
|
||||
SURF 0X10
|
||||
mat 7
|
||||
refs 4
|
||||
158 0.506267 0.856869
|
||||
160 0.506267 0.75693
|
||||
163 0.50774 0.75693
|
||||
161 0.50774 0.856869
|
||||
158 0.506093 0.857564
|
||||
160 0.506093 0.753809
|
||||
163 0.508613 0.753809
|
||||
161 0.508613 0.857564
|
||||
kids 0
|
||||
OBJECT poly
|
||||
name "Rcutoff.axis"
|
||||
|
|
|
|||
Binary file not shown.
|
Before Width: | Height: | Size: 1.3 MiB After Width: | Height: | Size: 1.3 MiB |
|
|
@ -30,7 +30,7 @@ var new = func(layer) {
|
|||
m.addVisibilityListener();
|
||||
var driver = opt_member(m.layer.options, 'route_driver');
|
||||
if(driver == nil){
|
||||
driver = RouteDriver.new();
|
||||
driver = A3XXRouteDriver.new();
|
||||
}
|
||||
var driver_listeners = driver.getListeners();
|
||||
foreach(var listener; driver_listeners){
|
||||
|
|
|
|||
|
|
@ -180,8 +180,8 @@
|
|||
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 -1.20 0.00
|
||||
0.9 -0.07 0.00
|
||||
0.2 5.01 0.00
|
||||
0.9 1.05 0.00
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -194,8 +194,8 @@
|
|||
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
|
||||
<tableData>
|
||||
0 1
|
||||
0.2 -0.25 0.00
|
||||
0.9 -0.19 0.00
|
||||
0.2 1.03 0.00
|
||||
0.9 0.79 0.00
|
||||
</tableData>
|
||||
</table>
|
||||
</function>
|
||||
|
|
@ -1113,13 +1113,13 @@
|
|||
<input>fbw/yaw/r-r_s-s</input>
|
||||
<gain>fbw/yaw/yd-p-gain</gain>
|
||||
<clipto>
|
||||
<min>-0.2</min>
|
||||
<max>0.2</max>
|
||||
<min>-0.1</min>
|
||||
<max>0.1</max>
|
||||
</clipto>
|
||||
</pure_gain>
|
||||
|
||||
<switch name="fbw/yaw/slip-skid">
|
||||
<default value="/instrumentation/slip-skid-ball/indicated-slip-skid"/>
|
||||
<default value="aero/beta-rad"/>
|
||||
<test logic="OR" value="0">
|
||||
position/wow eq 1
|
||||
fbw/yaw/rudder-nul gt 0
|
||||
|
|
|
|||
|
|
@ -262,6 +262,430 @@
|
|||
<output>/engines/engine[1]/n1-actual-cmd</output>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED 1</name>
|
||||
<type>noise-spike</type>
|
||||
<input>/controls/engines/throttle-cmd-pid</input>
|
||||
<output>/controls/engines/engine[0]/throttle-cmd</output>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<greater-than-equals>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</greater-than-equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</or>
|
||||
</condition>
|
||||
<value>1000</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.3</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>1000</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED LIMIT 1</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>/controls/engines/engine[0]/throttle-cmd</input>
|
||||
<output>/controls/engines/engine[0]/throttle-cmd-feed</output>
|
||||
<min>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/mode/thr</property>
|
||||
<value>RETARD</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>0.0</value>
|
||||
</min>
|
||||
<min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</min>
|
||||
<max>
|
||||
<property>/controls/engines/engine[0]/throttle-man</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED 2</name>
|
||||
<type>noise-spike</type>
|
||||
<input>/controls/engines/throttle-cmd-pid</input>
|
||||
<output>/controls/engines/engine[1]/throttle-cmd</output>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<greater-than-equals>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</greater-than-equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</or>
|
||||
</condition>
|
||||
<value>1000</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.3</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>1000</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED LIMIT 2</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>/controls/engines/engine[1]/throttle-cmd</input>
|
||||
<output>/controls/engines/engine[1]/throttle-cmd-feed</output>
|
||||
<min>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/mode/thr</property>
|
||||
<value>RETARD</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>0.0</value>
|
||||
</min>
|
||||
<min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</min>
|
||||
<max>
|
||||
<property>/controls/engines/engine[1]/throttle-man</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>Throttle 1</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -435,7 +859,7 @@
|
|||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
<property>/controls/engines/engine[0]/throttle-cmd</property>
|
||||
<property>/controls/engines/engine[0]/throttle-cmd-feed</property>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/engine[0]/throttle-fdm</property>
|
||||
|
|
@ -615,7 +1039,7 @@
|
|||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
<property>/controls/engines/engine[1]/throttle-cmd</property>
|
||||
<property>/controls/engines/engine[1]/throttle-cmd-feed</property>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/engine[1]/throttle-fdm</property>
|
||||
|
|
|
|||
|
|
@ -643,6 +643,430 @@
|
|||
<output>/engines/engine[1]/n1-actual-cmd</output>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED 1</name>
|
||||
<type>noise-spike</type>
|
||||
<input>/controls/engines/throttle-cmd-pid</input>
|
||||
<output>/controls/engines/engine[0]/throttle-cmd</output>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<greater-than-equals>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</greater-than-equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</or>
|
||||
</condition>
|
||||
<value>1000</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.3</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[0]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state1</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>1000</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED LIMIT 1</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>/controls/engines/engine[0]/throttle-cmd</input>
|
||||
<output>/controls/engines/engine[0]/throttle-cmd-feed</output>
|
||||
<min>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/mode/thr</property>
|
||||
<value>RETARD</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>0.0</value>
|
||||
</min>
|
||||
<min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</min>
|
||||
<max>
|
||||
<property>/controls/engines/engine[0]/throttle-man</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED 2</name>
|
||||
<type>noise-spike</type>
|
||||
<input>/controls/engines/throttle-cmd-pid</input>
|
||||
<output>/controls/engines/engine[1]/throttle-cmd</output>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<greater-than-equals>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</greater-than-equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>IDLE</value>
|
||||
</equals>
|
||||
</or>
|
||||
</and>
|
||||
</or>
|
||||
</condition>
|
||||
<value>1000</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.3</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/it-autoflight/output/athr</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<or>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/lim-flex</property>
|
||||
<value>0</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MCT</value>
|
||||
</equals>
|
||||
</and>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/systems/thrust/eng-out</property>
|
||||
<value>1</value>
|
||||
</equals>
|
||||
<less-than>
|
||||
<property>/controls/engines/engine[1]/throttle-pos</property>
|
||||
<value>0.83</value>
|
||||
</less-than>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN THR</value>
|
||||
</equals>
|
||||
</and>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>CL</value>
|
||||
</equals>
|
||||
<equals>
|
||||
<property>/systems/thrust/state2</property>
|
||||
<value>MAN</value>
|
||||
</equals>
|
||||
</or>
|
||||
<not-equals>
|
||||
<property>/it-autoflight/output/thr-mode</property>
|
||||
<value>0</value>
|
||||
</not-equals>
|
||||
</and>
|
||||
</condition>
|
||||
<value>0.05</value>
|
||||
</max-rate-of-change>
|
||||
<max-rate-of-change>1000</max-rate-of-change>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>A/THR FEED LIMIT 2</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>/controls/engines/engine[1]/throttle-cmd</input>
|
||||
<output>/controls/engines/engine[1]/throttle-cmd-feed</output>
|
||||
<min>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/mode/thr</property>
|
||||
<value>RETARD</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>0.0</value>
|
||||
</min>
|
||||
<min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</min>
|
||||
<max>
|
||||
<property>/controls/engines/engine[1]/throttle-man</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>Throttle 1</name>
|
||||
<debug>false</debug>
|
||||
|
|
@ -816,7 +1240,7 @@
|
|||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
<property>/controls/engines/engine[0]/throttle-cmd</property>
|
||||
<property>/controls/engines/engine[0]/throttle-cmd-feed</property>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/engine[0]/throttle-fdm</property>
|
||||
|
|
@ -996,7 +1420,7 @@
|
|||
</or>
|
||||
</and>
|
||||
</condition>
|
||||
<property>/controls/engines/engine[1]/throttle-cmd</property>
|
||||
<property>/controls/engines/engine[1]/throttle-cmd-feed</property>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/engine[1]/throttle-fdm</property>
|
||||
|
|
|
|||
|
|
@ -523,17 +523,8 @@
|
|||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/it-autoflight/mode/thr</property>
|
||||
<value>RETARD</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<value>0.0</value>
|
||||
</input>
|
||||
<input>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
|
|
@ -643,7 +634,7 @@
|
|||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<property>/controls/engines/throttle-pid-max</property>
|
||||
<value>1.0</value>
|
||||
</input>
|
||||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
|
|
@ -750,36 +741,6 @@
|
|||
<output>
|
||||
<property>/controls/engines/throttle-cmd-pid</property>
|
||||
</output>
|
||||
<min>
|
||||
<property>/controls/engines/idle-limit</property>
|
||||
</min>
|
||||
<max>
|
||||
<property>/controls/engines/throttle-pid-max</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
<!-- Engine 1 -->
|
||||
<filter>
|
||||
<name>Thrust Filter 1</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>/controls/engines/throttle-cmd-pid</input>
|
||||
<output>/controls/engines/engine[0]/throttle-cmd</output>
|
||||
<max>
|
||||
<property>/controls/engines/engine[0]/throttle-man</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
<!-- Engine 2 -->
|
||||
<filter>
|
||||
<name>Thrust Filter 2</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>/controls/engines/throttle-cmd-pid</input>
|
||||
<output>/controls/engines/engine[1]/throttle-cmd</output>
|
||||
<max>
|
||||
<property>/controls/engines/engine[1]/throttle-man</property>
|
||||
</max>
|
||||
</filter>
|
||||
|
||||
</PropertyList>
|
||||
|
|
|
|||
|
|
@ -1 +1 @@
|
|||
4412
|
||||
4504
|
||||
Reference in a new issue