fly/IDG-A32X
Archived
1
0
Fork 0
Code Issues Pull requests Projects Releases Wiki Activity

Merge branch 'master' into Lower-ECAM

Browse source
This commit is contained in:
Joshua Davidson 2018-06-05 15:55:18 -04:00
commit 3e1fdbdbb6
36 changed files with 2394 additions and 641 deletions
Show stats Download patch file Download diff file Expand all files Collapse all files

4
A320-100-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions> </ground_reactions>
<propulsion> <propulsion>
<engine file="cfm56_5a1"> <engine file="cfm56_5a1_1">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> -5.755 </y> <y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster> </thruster>
</engine> </engine>
<engine file="cfm56_5a1"> <engine file="cfm56_5a1_2">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> 5.755 </y> <y> 5.755 </y>

4
A320-200-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions> </ground_reactions>
<propulsion> <propulsion>
<engine file="cfm56_5b4"> <engine file="cfm56_5b4_1">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> -5.755 </y> <y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster> </thruster>
</engine> </engine>
<engine file="cfm56_5b4"> <engine file="cfm56_5b4_2">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> 5.755 </y> <y> 5.755 </y>

4
A320-200-IAE.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions> </ground_reactions>
<propulsion> <propulsion>
<engine file="v2527_a5"> <engine file="v2527_a5_1">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> -5.755 </y> <y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster> </thruster>
</engine> </engine>
<engine file="v2527_a5"> <engine file="v2527_a5_2">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> 5.755 </y> <y> 5.755 </y>

31
A320-main.xml
View file

@ -355,6 +355,8 @@
<z-offset-min-m type="float">30.0</z-offset-min-m> <z-offset-min-m type="float">30.0</z-offset-min-m>
<z-offset-max-m type="float">300.0</z-offset-max-m> <z-offset-max-m type="float">300.0</z-offset-max-m>
</current-view> </current-view>
<minimum-fg-version>2018.1.0</minimum-fg-version>
</sim> </sim>
<consumables> <consumables>
@ -997,8 +999,20 @@
</mouse> </mouse>
</mice> </mice>
<keyboard> <keyboard>
<key n="4">
<name>CTRL-d</name>
<desc>Autothrottle Disconnect</desc>
<binding>
<command>nasal</command>
<script>
if (getprop("/it-autoflight/output/athr") == 1) {
setprop("/it-autoflight/input/athr", 0);
}
</script>
</binding>
</key>
<key n="24"> <key n="24">
<name>Ctrl-X</name> <name>Ctrl-x</name>
<desc>Reset zoom to default</desc> <desc>Reset zoom to default</desc>
<binding> <binding>
<command>nasal</command> <command>nasal</command>
@ -1226,6 +1240,21 @@
</script> </script>
</binding> </binding>
</key> </key>
<key n="68">
<name>D</name>
<desc>Autopilot Disconnect</desc>
<binding>
<command>nasal</command>
<script>
if (getprop("/it-autoflight/output/ap1") == 1) {
setprop("/it-autoflight/input/ap1", 0);
}
if (getprop("/it-autoflight/output/ap2") == 1) {
setprop("/it-autoflight/input/ap2", 0);
}
</script>
</binding>
</key>
<key n="88"> <key n="88">
<name>X</name> <name>X</name>
<desc>Increase field of view</desc> <desc>Increase field of view</desc>

4
A320neo-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions> </ground_reactions>
<propulsion> <propulsion>
<engine file="leap1a26"> <engine file="leap1a26_1">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> -5.755 </y> <y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster> </thruster>
</engine> </engine>
<engine file="leap1a26"> <engine file="leap1a26_2">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> 5.755 </y> <y> 5.755 </y>

4
A320neo-PW.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions> </ground_reactions>
<propulsion> <propulsion>
<engine file="pw1127g"> <engine file="pw1127g_1">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> -5.755 </y> <y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster> </thruster>
</engine> </engine>
<engine file="pw1127g"> <engine file="pw1127g_2">
<location unit="M"> <location unit="M">
<x> 14.3962788 </x> <x> 14.3962788 </x>
<y> 5.755 </y> <y> 5.755 </y>

8
AircraftConfig/acconfig.nas
View file

@ -126,9 +126,9 @@ setlistener("/systems/acconfig/new-revision", func {
}); });
var mismatch_chk = func { var mismatch_chk = func {
if (num(string.replace(getprop("/sim/version/flightgear"),".","")) < 201730) { if (num(string.replace(getprop("/sim/version/flightgear"),".","")) < 201810) {
setprop("/systems/acconfig/mismatch-code", "0x121"); 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."); 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) { if (getprop("/systems/acconfig/out-of-date") != 1) {
error_mismatch.open(); error_mismatch.open();
} }
@ -344,14 +344,14 @@ var taxi = func {
setprop("/controls/APU/master", 1); setprop("/controls/APU/master", 1);
setprop("/controls/APU/start", 1); setprop("/controls/APU/start", 1);
var apu_rpm_chk = setlistener("/systems/apu/rpm", func { var apu_rpm_chk = setlistener("/systems/apu/rpm", func {
if (getprop("/systems/apu/rpm") >= 99) { if (getprop("/systems/apu/rpm") >= 98) {
removelistener(apu_rpm_chk); removelistener(apu_rpm_chk);
taxi_b(); taxi_b();
} }
}); });
} }
var taxi_b = func { var taxi_b = func {
# Continue with engine start prep, and start engine 2. # Continue with engine start prep, and start engines.
setprop("/controls/fuel/tank0pump1", 1); setprop("/controls/fuel/tank0pump1", 1);
setprop("/controls/fuel/tank0pump2", 1); setprop("/controls/fuel/tank0pump2", 1);
setprop("/controls/fuel/tank1pump1", 1); setprop("/controls/fuel/tank1pump1", 1);

16
AircraftConfig/help.xml
View file

@ -96,6 +96,10 @@
<halign>left</halign> <halign>left</halign>
<label>F2 - Engage/Increase Reverse Thrust</label> <label>F2 - Engage/Increase Reverse Thrust</label>
</text> </text>
<text>
<halign>left</halign>
<label>DEL - Toggle Reverse Thrust</label>
</text>
<text> <text>
<halign>left</halign> <halign>left</halign>
<label>E - Set Idle Thrust</label> <label>E - Set Idle Thrust</label>
@ -104,10 +108,6 @@
<halign>left</halign> <halign>left</halign>
<label>F - Set TOGA Thrust</label> <label>F - Set TOGA Thrust</label>
</text> </text>
<text>
<halign>left</halign>
<label>DEL - Toggle Reverse Thrust</label>
</text>
<text> <text>
<halign>left</halign> <halign>left</halign>
<label>CTRL + B - Cycle Spoilers</label> <label>CTRL + B - Cycle Spoilers</label>
@ -116,6 +116,14 @@
<halign>left</halign> <halign>left</halign>
<label>SHIFT + B - Toggle Parking Brake</label> <label>SHIFT + B - Toggle Parking Brake</label>
</text> </text>
<text>
<halign>left</halign>
<label>CTRL + D - Disconnect Autothrottle</label>
</text>
<text>
<halign>left</halign>
<label>SHIFT + D - Disconnect Autopilot</label>
</text>
</group> </group>

2
AircraftConfig/main.xml
View file

@ -396,7 +396,7 @@
</checkbox> </checkbox>
<checkbox> <checkbox>
<label>Skip ADIRS Alignment</label> <label>ADIRS Aligns Instantly</label>
<halign>left</halign> <halign>left</halign>
<property>/controls/adirs/skip</property> <property>/controls/adirs/skip</property>
<binding> <binding>

4
AircraftConfig/update.xml
View file

@ -104,7 +104,9 @@
<command>nasal</command> <command>nasal</command>
<script> <script>
if (getprop("/systems/acconfig/mismatch-code") == "0x000") { if (getprop("/systems/acconfig/mismatch-code") == "0x000") {
acconfig.welcome_dlg.open(); if (getprop("/systems/acconfig/options/welcome-skip") != 1) {
acconfig.welcome_dlg.open();
}
} else { } else {
acconfig.error_mismatch.open(); acconfig.error_mismatch.open();
} }

59
Engines/cfm56_5a1.xml
View file

@ -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
View 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
View 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>

59
Engines/cfm56_5b4.xml
View file

@ -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
View 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
View 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>

59
Engines/leap1a26.xml
View file

@ -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
View 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
View 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>

59
Engines/pw1127g.xml
View file

@ -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
View 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
View 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>

59
Engines/v2527_a5.xml
View file

@ -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
View 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
View 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>

2
INSTALL.md
View file

@ -1,7 +1,7 @@
# INSTALL # INSTALL
## Prerequisites ## Prerequisites
Have at least following versions installed: Have at least following versions installed:
* FlightGear 2017.3.0 or newer * FlightGear 2018.1.0 or newer
## Install using ZIP Snapshot ## Install using ZIP Snapshot
[Download](https://github.com/it0uchpods/IDG-A32X/archive/master.zip) the zip file. [Download](https://github.com/it0uchpods/IDG-A32X/archive/master.zip) the zip file.

6
ISSUE_TEMPLATE.md
View file

@ -1,5 +1,5 @@
<!-- Provide a general summary of the issue/question in the title above. --> <!-- Provide a general summary of the issue in the title above. -->
<!-- Incase of a question, remove the format below, and write your question. --> <!-- Issues are for reporting bugs or problems only. If you have a feature request, please write in the forums. -->
### Expected Behavior ### Expected Behavior
<!-- Tell us what should happen. --> <!-- Tell us what should happen. -->
@ -16,4 +16,4 @@
1. 1.
2. 2.
3. 3.
4. 4.

532
Models/FlightDeck/res/fd_complete.ac
View file

@ -161418,13 +161418,13 @@ numsurf 2
SURF 0X12 SURF 0X12
mat 1 mat 1
refs 2 refs 2
2 0 0 0 0 0
3 0 0 1 0 0
SURF 0X12 SURF 0X12
mat 1 mat 1
refs 2 refs 2
0 0 0 2 0 0
1 0 0 3 0 0
kids 0 kids 0
OBJECT poly OBJECT poly
name "iesi" name "iesi"
@ -163905,55 +163905,55 @@ numvert 169
-0.02028 -0.10862 0.02178 -0.02028 -0.10862 0.02178
-0.01903 -0.10792 0.02216 -0.01903 -0.10792 0.02216
-0.01812 -0.10742 0.02321 -0.01812 -0.10742 0.02321
-0.02078 -0.10273 0.02607 -0.01938 -0.10553 0.02607
-0.02045 -0.10255 0.02468 -0.01905 -0.10535 0.02468
-0.02167 -0.10323 0.02709 -0.02027 -0.10603 0.02709
-0.02288 -0.1039 0.02746 -0.02148 -0.1067 0.02746
-0.0241 -0.10458 0.02709 -0.0227 -0.10738 0.02709
-0.02499 -0.10508 0.02607 -0.02359 -0.10788 0.02607
-0.02531 -0.10526 0.02468 -0.02391 -0.10806 0.02468
-0.02499 -0.10508 0.02328 -0.02359 -0.10788 0.02328
-0.0241 -0.10458 0.02227 -0.0227 -0.10738 0.02227
-0.02288 -0.1039 0.02189 -0.02148 -0.1067 0.02189
-0.02167 -0.10323 0.02227 -0.02027 -0.10603 0.02227
-0.02078 -0.10273 0.02328 -0.01938 -0.10553 0.02328
-0.00735 -0.13178 0.02464 -0.00735 -0.13178 0.02464
-0.02136 -0.10004 0.02662 -0.01996 -0.10284 0.02662
-0.02093 -0.0998 0.02477 -0.01953 -0.1026 0.02477
-0.02254 -0.1007 0.02798 -0.02114 -0.1035 0.02798
-0.02416 -0.1016 0.02847 -0.02276 -0.1044 0.02847
-0.02577 -0.1025 0.02798 -0.02437 -0.1053 0.02798
-0.02696 -0.10316 0.02662 -0.02556 -0.10596 0.02662
-0.02739 -0.1034 0.02477 -0.02599 -0.1062 0.02477
-0.02696 -0.10316 0.02292 -0.02556 -0.10596 0.02292
-0.02577 -0.1025 0.02157 -0.02437 -0.1053 0.02157
-0.02416 -0.1016 0.02107 -0.02276 -0.1044 0.02107
-0.02254 -0.1007 0.02157 -0.02114 -0.1035 0.02157
-0.02136 -0.10004 0.02292 -0.01996 -0.10284 0.02292
-0.02166 -0.09744 0.03183 -0.02026 -0.10024 0.03183
-0.02877 -0.1014 0.03183 -0.02737 -0.1042 0.03183
-0.02522 -0.09942 0.03292 -0.02382 -0.10222 0.03292
-0.02093 -0.09698 0.02889 -0.01953 -0.09978 0.02889
-0.03137 -0.10284 0.02885 -0.02997 -0.10564 0.02885
-0.02093 -0.09697 0.02484 -0.01953 -0.09977 0.02484
-0.03232 -0.10338 0.02478 -0.03092 -0.10618 0.02478
-0.02092 -0.09701 0.0206 -0.01952 -0.09981 0.0206
-0.03137 -0.10284 0.02072 -0.02997 -0.10564 0.02072
-0.02166 -0.09744 0.01774 -0.02026 -0.10024 0.01774
-0.02877 -0.1014 0.01774 -0.02737 -0.1042 0.01774
-0.02522 -0.09942 0.01665 -0.02382 -0.10222 0.01665
-0.03543 -0.10507 0.0165 -0.03403 -0.10787 0.0165
-0.02089 -0.09697 0.03307 -0.01949 -0.09977 0.03307
-0.03543 -0.10507 0.03307 -0.03403 -0.10787 0.03307
-0.02089 -0.09697 0.0165 -0.01949 -0.09977 0.0165
-0.02148 -0.09591 0.03307 -0.02008 -0.09871 0.03307
-0.03602 -0.10402 0.03307 -0.03462 -0.10682 0.03307
-0.02148 -0.09591 0.0165 -0.02008 -0.09871 0.0165
-0.03602 -0.10402 0.0165 -0.03462 -0.10682 0.0165
-0.02229 -0.09503 0.01678 -0.02089 -0.09783 0.01678
-0.03635 -0.10286 0.03279 -0.03495 -0.10566 0.03279
-0.02229 -0.09503 0.03279 -0.02089 -0.09783 0.03279
-0.03635 -0.10286 0.01678 -0.03495 -0.10566 0.01678
numsurf 166 numsurf 166
SURF 0X10 SURF 0X10
mat 7 mat 7
@ -379954,181 +379954,181 @@ refs 2
kids 0 kids 0
OBJECT poly OBJECT poly
name "Rcutoff" name "Rcutoff"
data 12 data 16
Rcutoff.mesh Lcutoff.mesh.000
crease 45.0 crease 45.0
texture "ped_xtra.png" texture "ped_xtra.png"
texrep 1 1 texrep 1 1
numvert 169 numvert 169
-0.00556 -0.13002 -0.02535 -0.00556 -0.13002 -0.02549
-0.00436 -0.12575 -0.02215 -0.00436 -0.12575 -0.02229
-0.00584 -0.13018 -0.02414 -0.00584 -0.13018 -0.02428
-0.00361 -0.12533 -0.02535 -0.00361 -0.12533 -0.02549
-0.00662 -0.13061 -0.02326 -0.00662 -0.13061 -0.02339
-0.00641 -0.12689 -0.01981 -0.00641 -0.12689 -0.01994
-0.00767 -0.1312 -0.02293 -0.00767 -0.1312 -0.02307
-0.00921 -0.12845 -0.01895 -0.00921 -0.12845 -0.01909
-0.012 -0.13001 -0.01981 -0.012 -0.13001 -0.01994
-0.00873 -0.13179 -0.02326 -0.00873 -0.13179 -0.02339
-0.01405 -0.13115 -0.02215 -0.01405 -0.13115 -0.02229
-0.0095 -0.13222 -0.02414 -0.0095 -0.13222 -0.02428
-0.0148 -0.13157 -0.02535 -0.0148 -0.13157 -0.02549
-0.00979 -0.13237 -0.02535 -0.00979 -0.13237 -0.02549
-0.0095 -0.13222 -0.02656 -0.0095 -0.13222 -0.0267
-0.01405 -0.13115 -0.02856 -0.01405 -0.13115 -0.02869
-0.00873 -0.13179 -0.02745 -0.00873 -0.13179 -0.02759
-0.012 -0.13001 -0.0309 -0.012 -0.13001 -0.03104
-0.00767 -0.1312 -0.02777 -0.00767 -0.1312 -0.02791
-0.00921 -0.12845 -0.03176 -0.00921 -0.12845 -0.0319
-0.00641 -0.12689 -0.0309 -0.00641 -0.12689 -0.03104
-0.00662 -0.13061 -0.02745 -0.00662 -0.13061 -0.02759
-0.00436 -0.12575 -0.02856 -0.00436 -0.12575 -0.02869
-0.00584 -0.13018 -0.02656 -0.00584 -0.13018 -0.0267
-0.00779 -0.12295 -0.0231 -0.00779 -0.12295 -0.02323
-0.00726 -0.12265 -0.02536 -0.00726 -0.12265 -0.0255
-0.00923 -0.12375 -0.02144 -0.00923 -0.12375 -0.02158
-0.01121 -0.12485 -0.02084 -0.01121 -0.12485 -0.02097
-0.01318 -0.12596 -0.02144 -0.01318 -0.12596 -0.02158
-0.01463 -0.12676 -0.0231 -0.01463 -0.12676 -0.02323
-0.01516 -0.12706 -0.02536 -0.01516 -0.12706 -0.0255
-0.01463 -0.12676 -0.02762 -0.01463 -0.12676 -0.02776
-0.01318 -0.12596 -0.02927 -0.01318 -0.12596 -0.02941
-0.01121 -0.12485 -0.02988 -0.01121 -0.12485 -0.03002
-0.00923 -0.12375 -0.02927 -0.00923 -0.12375 -0.02941
-0.00779 -0.12295 -0.02762 -0.00779 -0.12295 -0.02776
-0.00919 -0.123 -0.02383 -0.00919 -0.123 -0.02397
-0.00883 -0.1228 -0.02537 -0.00883 -0.1228 -0.02551
-0.01017 -0.12355 -0.02271 -0.01017 -0.12355 -0.02284
-0.01152 -0.1243 -0.02229 -0.01152 -0.1243 -0.02243
-0.01286 -0.12505 -0.02271 -0.01286 -0.12505 -0.02284
-0.01384 -0.1256 -0.02383 -0.01384 -0.1256 -0.02397
-0.0142 -0.1258 -0.02537 -0.0142 -0.1258 -0.02551
-0.01384 -0.1256 -0.02691 -0.01384 -0.1256 -0.02704
-0.01286 -0.12505 -0.02803 -0.01286 -0.12505 -0.02817
-0.01152 -0.1243 -0.02844 -0.01152 -0.1243 -0.02858
-0.01017 -0.12355 -0.02803 -0.01017 -0.12355 -0.02817
-0.00919 -0.123 -0.02691 -0.00919 -0.123 -0.02704
-0.01081 -0.11532 -0.02248 -0.01081 -0.11532 -0.02262
-0.01013 -0.11495 -0.02536 -0.01013 -0.11495 -0.0255
-0.01265 -0.11635 -0.02036 -0.01265 -0.11635 -0.0205
-0.01518 -0.11776 -0.01959 -0.01518 -0.11776 -0.01973
-0.0177 -0.11916 -0.02036 -0.0177 -0.11916 -0.0205
-0.01954 -0.12019 -0.02248 -0.01954 -0.12019 -0.02262
-0.02022 -0.12057 -0.02536 -0.02022 -0.12057 -0.0255
-0.01954 -0.12019 -0.02825 -0.01954 -0.12019 -0.02839
-0.0177 -0.11916 -0.03037 -0.0177 -0.11916 -0.0305
-0.01518 -0.11776 -0.03114 -0.01518 -0.11776 -0.03128
-0.01265 -0.11635 -0.03037 -0.01265 -0.11635 -0.0305
-0.01081 -0.11532 -0.02825 -0.01081 -0.11532 -0.02839
-0.01119 -0.11361 -0.02219 -0.01119 -0.11361 -0.02233
-0.01045 -0.1132 -0.02537 -0.01045 -0.1132 -0.0255
-0.01322 -0.11474 -0.01987 -0.01322 -0.11475 -0.02
-0.01599 -0.11629 -0.01902 -0.01599 -0.11629 -0.01915
-0.01877 -0.11784 -0.01987 -0.01877 -0.11784 -0.02
-0.0208 -0.11897 -0.02219 -0.0208 -0.11897 -0.02233
-0.02154 -0.11938 -0.02537 -0.02154 -0.11938 -0.0255
-0.0208 -0.11897 -0.02854 -0.0208 -0.11897 -0.02868
-0.01877 -0.11784 -0.03086 -0.01877 -0.11784 -0.031
-0.01599 -0.11629 -0.03171 -0.01599 -0.11629 -0.03185
-0.01322 -0.11474 -0.03086 -0.01322 -0.11475 -0.031
-0.01119 -0.11361 -0.02854 -0.01119 -0.11361 -0.02868
-0.01438 -0.10821 -0.02228 -0.01438 -0.10821 -0.02242
-0.01366 -0.10781 -0.02536 -0.01366 -0.10781 -0.0255
-0.01635 -0.10931 -0.02003 -0.01635 -0.10931 -0.02016
-0.01905 -0.11081 -0.0192 -0.01905 -0.11081 -0.01934
-0.02174 -0.11231 -0.02003 -0.02174 -0.11231 -0.02016
-0.02371 -0.11341 -0.02228 -0.02371 -0.11341 -0.02242
-0.02443 -0.11381 -0.02536 -0.02443 -0.11381 -0.0255
-0.02371 -0.11341 -0.02845 -0.02371 -0.11341 -0.02858
-0.02174 -0.11231 -0.0307 -0.02174 -0.11231 -0.03084
-0.01905 -0.11081 -0.03153 -0.01905 -0.11081 -0.03167
-0.01635 -0.10931 -0.0307 -0.01635 -0.10931 -0.03084
-0.01438 -0.10821 -0.02845 -0.01438 -0.10821 -0.02858
-0.01484 -0.108 -0.02245 -0.01484 -0.10801 -0.02259
-0.01416 -0.10762 -0.02536 -0.01416 -0.10763 -0.0255
-0.0167 -0.10904 -0.02032 -0.0167 -0.10904 -0.02046
-0.01924 -0.11046 -0.01954 -0.01924 -0.11046 -0.01968
-0.02178 -0.11188 -0.02032 -0.02178 -0.11188 -0.02046
-0.02365 -0.11291 -0.02245 -0.02365 -0.11292 -0.02259
-0.02433 -0.11329 -0.02536 -0.02433 -0.1133 -0.0255
-0.02365 -0.11291 -0.02828 -0.02365 -0.11292 -0.02841
-0.02178 -0.11188 -0.03041 -0.02178 -0.11188 -0.03054
-0.01924 -0.11046 -0.03119 -0.01924 -0.11046 -0.03132
-0.0167 -0.10904 -0.03041 -0.0167 -0.10904 -0.03054
-0.01484 -0.108 -0.02828 -0.01484 -0.10801 -0.02841
-0.01681 -0.10808 -0.02346 -0.01681 -0.10808 -0.0236
-0.01636 -0.10783 -0.02536 -0.01636 -0.10783 -0.0255
-0.01802 -0.10876 -0.02207 -0.01802 -0.10876 -0.02221
-0.01968 -0.10968 -0.02156 -0.01968 -0.10969 -0.0217
-0.02134 -0.11061 -0.02207 -0.02134 -0.11061 -0.02221
-0.02256 -0.11129 -0.02346 -0.02256 -0.11129 -0.0236
-0.023 -0.11154 -0.02536 -0.023 -0.11154 -0.0255
-0.02256 -0.11129 -0.02727 -0.02256 -0.11129 -0.0274
-0.02134 -0.11061 -0.02866 -0.02134 -0.11061 -0.0288
-0.01968 -0.10968 -0.02917 -0.01968 -0.10969 -0.0293
-0.01802 -0.10876 -0.02866 -0.01802 -0.10876 -0.0288
-0.01681 -0.10808 -0.02727 -0.01681 -0.10808 -0.0274
-0.01812 -0.10742 -0.02394 -0.01812 -0.10742 -0.02408
-0.01779 -0.10723 -0.02536 -0.01779 -0.10723 -0.0255
-0.01904 -0.10792 -0.0229 -0.01903 -0.10792 -0.02304
-0.02028 -0.10862 -0.02252 -0.02028 -0.10862 -0.02265
-0.02152 -0.10931 -0.0229 -0.02152 -0.10931 -0.02304
-0.02243 -0.10982 -0.02394 -0.02243 -0.10982 -0.02408
-0.02276 -0.11 -0.02536 -0.02276 -0.11 -0.0255
-0.02243 -0.10982 -0.02679 -0.02243 -0.10982 -0.02692
-0.02152 -0.10931 -0.02783 -0.02152 -0.10931 -0.02797
-0.02028 -0.10862 -0.02821 -0.02028 -0.10862 -0.02835
-0.01904 -0.10792 -0.02783 -0.01903 -0.10792 -0.02797
-0.01812 -0.10742 -0.02679 -0.01812 -0.10742 -0.02692
-0.02078 -0.10273 -0.02392 -0.01938 -0.10553 -0.02406
-0.02045 -0.10255 -0.02532 -0.01905 -0.10535 -0.02545
-0.02167 -0.10322 -0.0229 -0.02027 -0.10603 -0.02304
-0.02288 -0.1039 -0.02253 -0.02148 -0.1067 -0.02267
-0.0241 -0.10458 -0.0229 -0.0227 -0.10738 -0.02304
-0.02499 -0.10508 -0.02392 -0.02359 -0.10788 -0.02406
-0.02531 -0.10526 -0.02532 -0.02391 -0.10806 -0.02545
-0.02499 -0.10508 -0.02671 -0.02359 -0.10788 -0.02685
-0.0241 -0.10458 -0.02773 -0.0227 -0.10738 -0.02786
-0.02288 -0.1039 -0.0281 -0.02148 -0.1067 -0.02824
-0.02167 -0.10322 -0.02773 -0.02027 -0.10603 -0.02786
-0.02078 -0.10273 -0.02671 -0.01938 -0.10553 -0.02685
-0.00735 -0.13178 -0.02535 -0.00735 -0.13178 -0.02549
-0.02136 -0.10004 -0.02337 -0.01996 -0.10284 -0.02351
-0.02093 -0.0998 -0.02522 -0.01953 -0.1026 -0.02536
-0.02254 -0.1007 -0.02202 -0.02114 -0.1035 -0.02215
-0.02416 -0.1016 -0.02152 -0.02276 -0.1044 -0.02166
-0.02577 -0.1025 -0.02202 -0.02437 -0.1053 -0.02215
-0.02696 -0.10316 -0.02337 -0.02556 -0.10596 -0.02351
-0.02739 -0.1034 -0.02522 -0.02599 -0.1062 -0.02536
-0.02696 -0.10316 -0.02707 -0.02556 -0.10596 -0.02721
-0.02577 -0.1025 -0.02842 -0.02437 -0.1053 -0.02856
-0.02416 -0.1016 -0.02892 -0.02276 -0.1044 -0.02906
-0.02254 -0.1007 -0.02842 -0.02114 -0.1035 -0.02856
-0.02136 -0.10004 -0.02707 -0.01996 -0.10284 -0.02721
-0.02166 -0.09744 -0.01817 -0.02026 -0.10024 -0.0183
-0.02877 -0.10139 -0.01817 -0.02737 -0.1042 -0.0183
-0.02522 -0.09941 -0.01708 -0.02382 -0.10222 -0.01721
-0.02093 -0.09698 -0.02111 -0.01953 -0.09978 -0.02124
-0.03137 -0.10284 -0.02114 -0.02997 -0.10564 -0.02128
-0.02093 -0.09697 -0.02515 -0.01953 -0.09977 -0.02529
-0.03232 -0.10337 -0.02521 -0.03092 -0.10618 -0.02535
-0.02092 -0.09701 -0.02939 -0.01952 -0.09981 -0.02953
-0.03137 -0.10284 -0.02927 -0.02997 -0.10564 -0.02941
-0.02166 -0.09744 -0.03225 -0.02026 -0.10024 -0.03239
-0.02877 -0.10139 -0.03225 -0.02737 -0.1042 -0.03239
-0.02522 -0.09941 -0.03334 -0.02382 -0.10222 -0.03348
-0.03543 -0.10507 -0.03368 -0.03403 -0.10787 -0.03363
-0.02089 -0.09697 -0.01711 -0.01949 -0.09977 -0.01706
-0.03543 -0.10507 -0.01711 -0.03403 -0.10787 -0.01706
-0.02089 -0.09697 -0.03368 -0.01949 -0.09977 -0.03363
-0.02148 -0.09591 -0.01711 -0.02008 -0.09871 -0.01706
-0.03602 -0.10402 -0.01711 -0.03462 -0.10682 -0.01706
-0.02148 -0.09591 -0.03368 -0.02008 -0.09871 -0.03363
-0.03602 -0.10402 -0.03368 -0.03462 -0.10682 -0.03363
-0.02233 -0.09505 -0.03335 -0.02089 -0.09783 -0.03335
-0.03631 -0.10284 -0.01744 -0.03495 -0.10566 -0.01734
-0.02233 -0.09505 -0.01744 -0.02089 -0.09783 -0.01734
-0.03631 -0.10284 -0.03335 -0.03495 -0.10566 -0.03335
numsurf 166 numsurf 166
SURF 0X10 SURF 0X10
mat 7 mat 7
@ -380945,6 +380945,13 @@ refs 4
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 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 109 0.723479 0.793684
119 0.720759 0.792297 119 0.720759 0.792297
131 0.710471 0.792616 131 0.710471 0.792616
@ -381213,73 +381220,66 @@ refs 4
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
164 0.626892 0.764246 157 0.634061 0.760429
162 0.504196 0.764246 159 0.50671 0.760429
166 0.510314 0.762086 162 0.50671 0.764246
168 0.620774 0.762086 164 0.634061 0.764246
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
157 0.626892 0.760429 157 0.515068 0.876908
159 0.504196 0.760429 164 0.515068 0.880725
162 0.504196 0.764246 163 0.515068 0.762765
164 0.626892 0.764246 160 0.515068 0.758942
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
157 0.511508 0.876457 161 0.511738 0.762765
164 0.507637 0.876457 162 0.511738 0.880725
163 0.507634 0.764239 159 0.511738 0.876908
160 0.511509 0.764238 158 0.511738 0.758942
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
161 0.508386 0.765279 165 0.49663 0.515047
162 0.508386 0.883239 168 0.49663 0.621305
159 0.508386 0.879422 166 0.381514 0.621305
158 0.508386 0.761456 167 0.381514 0.515047
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
165 0.491231 0.515047 157 0.232288 0.59531
168 0.491231 0.618645 160 0.232288 0.528131
166 0.380771 0.618645 158 0.159764 0.528131
167 0.380771 0.515047 159 0.159764 0.59531
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
157 0.228416 0.594634 161 0.508613 0.857564
160 0.228416 0.530919 163 0.508613 0.753809
158 0.162147 0.530919 165 0.511589 0.758982
159 0.162147 0.594634 167 0.511589 0.85239
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
161 0.50774 0.856869 163 0.515068 0.762765
163 0.50774 0.75693 164 0.515068 0.880725
165 0.511416 0.761914 168 0.50895 0.878565
167 0.511416 0.851886 165 0.50895 0.772307
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
163 0.512741 0.758852 166 0.517856 0.878565
164 0.512741 0.876812 162 0.511738 0.880725
168 0.506623 0.874652 161 0.511738 0.762765
165 0.506623 0.768394 167 0.517856 0.772307
SURF 0X10 SURF 0X10
mat 7 mat 7
refs 4 refs 4
166 0.514504 0.881079 158 0.506093 0.857564
162 0.508386 0.883239 160 0.506093 0.753809
161 0.508386 0.765279 163 0.508613 0.753809
167 0.514504 0.774821 161 0.508613 0.857564
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
kids 0 kids 0
OBJECT poly OBJECT poly
name "Rcutoff.axis" name "Rcutoff.axis"

BIN
Models/FlightDeck/res/ohpanel2-tex.png
View file

Binary file not shown.
Side by side Swipe Overlay

Before

Width:  |  Height:  |  Size: 1.3 MiB

After

Width:  |  Height:  |  Size: 1.3 MiB

2
Models/Instruments/ND/canvas/map/RTE.lcontroller
View file

@ -30,7 +30,7 @@ var new = func(layer) {
m.addVisibilityListener(); m.addVisibilityListener();
var driver = opt_member(m.layer.options, 'route_driver'); var driver = opt_member(m.layer.options, 'route_driver');
if(driver == nil){ if(driver == nil){
driver = RouteDriver.new(); driver = A3XXRouteDriver.new();
} }
var driver_listeners = driver.getListeners(); var driver_listeners = driver.getListeners();
foreach(var listener; driver_listeners){ foreach(var listener; driver_listeners){

10
Nasal/it-fbw.nas
View file

@ -226,7 +226,15 @@ var update_loop = func {
var fbw_loop = func { var fbw_loop = func {
var ail = getprop("/controls/flight/aileron"); var ail = getprop("/controls/flight/aileron");
if (ail > 0.4 or ail < -0.4) { if (ail > 0.4 and getprop("/orientation/roll-deg") >= -33.5) {
setprop("/it-fbw/roll-lim", "67");
if (getprop("/it-fbw/roll-back") == 1 and getprop("/orientation/roll-deg") <= 33.5 and getprop("/orientation/roll-deg") >= -33.5) {
setprop("/it-fbw/roll-back", 0);
}
if (getprop("/it-fbw/roll-back") == 0 and (getprop("/orientation/roll-deg") > 33.5 or getprop("/orientation/roll-deg") < -33.5)) {
setprop("/it-fbw/roll-back", 1);
}
} else if (ail < -0.4 and getprop("/orientation/roll-deg") <= 33.5) {
setprop("/it-fbw/roll-lim", "67"); setprop("/it-fbw/roll-lim", "67");
if (getprop("/it-fbw/roll-back") == 1 and getprop("/orientation/roll-deg") <= 33.5 and getprop("/orientation/roll-deg") >= -33.5) { if (getprop("/it-fbw/roll-back") == 1 and getprop("/orientation/roll-deg") <= 33.5 and getprop("/orientation/roll-deg") >= -33.5) {
setprop("/it-fbw/roll-back", 0); setprop("/it-fbw/roll-back", 0);

28
Systems/a320-fcs.xml
View file

@ -180,8 +180,8 @@
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar> <independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 -1.20 0.00 0.2 5.01 0.00
0.9 -0.07 0.00 0.9 1.05 0.00
</tableData> </tableData>
</table> </table>
</function> </function>
@ -194,8 +194,8 @@
<independentVar lookup="column">fbw/yaw/gain-switch</independentVar> <independentVar lookup="column">fbw/yaw/gain-switch</independentVar>
<tableData> <tableData>
0 1 0 1
0.2 -0.25 0.00 0.2 1.03 0.00
0.9 -0.19 0.00 0.9 0.79 0.00
</tableData> </tableData>
</table> </table>
</function> </function>
@ -329,7 +329,7 @@
</function> </function>
</fcs_function> </fcs_function>
<fcs_function name="fbw/roll/r-r-rb"> <fcs_function name="fbw/roll/r-r-rb-f">
<function> <function>
<table> <table>
<independentVar lookup="row">attitude/roll-rad</independentVar> <independentVar lookup="row">attitude/roll-rad</independentVar>
@ -345,6 +345,18 @@
</function> </function>
</fcs_function> </fcs_function>
<switch name="fbw/roll/r-r-rb">
<default value="fbw/roll/r-r-rb-f"/>
<test logic="AND" value="fbw/roll/r-r-33">
attitude/roll-rad lt 0
fbw/roll/r-r-33 ge fbw/roll/r-r-rb-f
</test>
<test logic="AND" value="fbw/roll/r-r-33">
attitude/roll-rad gt 0
fbw/roll/r-r-33 le fbw/roll/r-r-rb-f
</test>
</switch>
<fcs_function name="fbw/roll/r-r-os-nrb"> <fcs_function name="fbw/roll/r-r-os-nrb">
<function> <function>
<sum> <sum>
@ -1113,13 +1125,13 @@
<input>fbw/yaw/r-r_s-s</input> <input>fbw/yaw/r-r_s-s</input>
<gain>fbw/yaw/yd-p-gain</gain> <gain>fbw/yaw/yd-p-gain</gain>
<clipto> <clipto>
<min>-0.2</min> <min>-0.1</min>
<max>0.2</max> <max>0.1</max>
</clipto> </clipto>
</pure_gain> </pure_gain>
<switch name="fbw/yaw/slip-skid"> <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"> <test logic="OR" value="0">
position/wow eq 1 position/wow eq 1
fbw/yaw/rudder-nul gt 0 fbw/yaw/rudder-nul gt 0

428
Systems/fadec-cfm.xml
View file

@ -262,6 +262,430 @@
<output>/engines/engine[1]/n1-actual-cmd</output> <output>/engines/engine[1]/n1-actual-cmd</output>
</filter> </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> <filter>
<name>Throttle 1</name> <name>Throttle 1</name>
<debug>false</debug> <debug>false</debug>
@ -435,7 +859,7 @@
</or> </or>
</and> </and>
</condition> </condition>
<property>/controls/engines/engine[0]/throttle-cmd</property> <property>/controls/engines/engine[0]/throttle-cmd-feed</property>
</input> </input>
<output> <output>
<property>/controls/engines/engine[0]/throttle-fdm</property> <property>/controls/engines/engine[0]/throttle-fdm</property>
@ -615,7 +1039,7 @@
</or> </or>
</and> </and>
</condition> </condition>
<property>/controls/engines/engine[1]/throttle-cmd</property> <property>/controls/engines/engine[1]/throttle-cmd-feed</property>
</input> </input>
<output> <output>
<property>/controls/engines/engine[1]/throttle-fdm</property> <property>/controls/engines/engine[1]/throttle-fdm</property>

428
Systems/fadec-iae.xml
View file

@ -643,6 +643,430 @@
<output>/engines/engine[1]/n1-actual-cmd</output> <output>/engines/engine[1]/n1-actual-cmd</output>
</filter> </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> <filter>
<name>Throttle 1</name> <name>Throttle 1</name>
<debug>false</debug> <debug>false</debug>
@ -816,7 +1240,7 @@
</or> </or>
</and> </and>
</condition> </condition>
<property>/controls/engines/engine[0]/throttle-cmd</property> <property>/controls/engines/engine[0]/throttle-cmd-feed</property>
</input> </input>
<output> <output>
<property>/controls/engines/engine[0]/throttle-fdm</property> <property>/controls/engines/engine[0]/throttle-fdm</property>
@ -996,7 +1420,7 @@
</or> </or>
</and> </and>
</condition> </condition>
<property>/controls/engines/engine[1]/throttle-cmd</property> <property>/controls/engines/engine[1]/throttle-cmd-feed</property>
</input> </input>
<output> <output>
<property>/controls/engines/engine[1]/throttle-fdm</property> <property>/controls/engines/engine[1]/throttle-fdm</property>

41
Systems/fmgc-thrust.xml
View file

@ -523,17 +523,8 @@
</condition> </condition>
</enable> </enable>
<input> <input>
<condition>
<equals>
<property>/it-autoflight/mode/thr</property>
<value>RETARD</value>
</equals>
</condition>
<value>0.0</value> <value>0.0</value>
</input> </input>
<input>
<property>/controls/engines/idle-limit</property>
</input>
<output> <output>
<property>/controls/engines/throttle-cmd-pid</property> <property>/controls/engines/throttle-cmd-pid</property>
</output> </output>
@ -643,7 +634,7 @@
</condition> </condition>
</enable> </enable>
<input> <input>
<property>/controls/engines/throttle-pid-max</property> <value>1.0</value>
</input> </input>
<output> <output>
<property>/controls/engines/throttle-cmd-pid</property> <property>/controls/engines/throttle-cmd-pid</property>
@ -750,36 +741,6 @@
<output> <output>
<property>/controls/engines/throttle-cmd-pid</property> <property>/controls/engines/throttle-cmd-pid</property>
</output> </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> </filter>
</PropertyList> </PropertyList>

2
revision.txt
View file

@ -1 +1 @@
4412 4504