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737-700-26.xml
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737-700-26.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="737-700" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Aeromatic v 3.3.10 </author>
<filecreationdate> 24 Apr 2018 </filecreationdate>
<version>$Revision: 1.80 $</version>
<description> Models a 737-700 with CFM56-7B26 engines. </description>
</fileheader>
<!--
File: 737-700.xml
Inputs:
name: 737-700
type: Multi-engine Passenger Jet Airliner, Transonic Jet Transport
stall speed: unspecified
max weight: 171028.61 lb
length: 110.24 ft
wing:
span: 112.60 ft
area: 1340.97 sq-ft
mean chord: 17.61 ft
aspect ratio: 9.45:1
taper ratio: 0.16:1
incidence: 2.00 degrees
dihedral: 6.00 degrees
sweep: 25.02 degrees
no. engines: 2
engine type: Turbine Engine
engine layout: wings
control type: Conventional with Yaw Damper
gear type: tricycle
steering type: steering
retractable?: yes
Outputs:
wing loading: 127.54 lb/sq-ft
- thickness ratio: 15.00%
payload: 40639.85 lbs
CL-alpha: 5.38 per radian
CL-0: 0.20
CL-max: 1.20
CD-0: 0.02
K: 0.04
Mcrit: 0.79
min. turn radius -nan ft
max. turn rate: -nan deg/s
-->
<metrics>
<wingarea unit="FT2"> 1340.97 </wingarea>
<wingspan unit="FT" > 112.60 </wingspan>
<wing_incidence unit="DEG"> 2.00 </wing_incidence>
<chord unit="FT" > 17.61 </chord>
<htailarea unit="FT2"> 352.84 </htailarea>
<htailarm unit="FT" > 49.57 </htailarm>
<vtailarea unit="FT2"> 284.60 </vtailarea>
<vtailarm unit="FT" > 45.08 </vtailarm>
<location name="AERORP" unit="IN">
<x> 728.05 </x>
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 92.60 </x>
<y> -30.00 </y>
<z> 70.00 </z>
</location>
<location name="VRP" unit="IN">
<x> 0.0 </x>
<y> 0.0 </y>
<z> 0.0 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 510715.75 </ixx>
<iyy unit="SLUG*FT2"> 1130968.00 </iyy>
<izz unit="SLUG*FT2"> 1692995.00 </izz>
<emptywt unit="LBS" > 83013.84 </emptywt>
<location name="CG" unit="IN">
<x> 728.05 </x>
<y> 0.00 </y>
<z> -33.07 </z>
</location>
<pointmass name="Payload">
<description> 40639.85 LBS should bring model up to entered max weight </description>
<weight unit="LBS"> 20319.92 </weight>
<location name="POINTMASS" unit="IN">
<x> 728.05 </x>
<y> 0.00 </y>
<z> -33.07 </z>
</location>
</pointmass>
</mass_balance>
<propulsion>
<engine file="CFM56-7B26">
<location unit="IN">
<x> 715.6 </x> <!-- value from simulator data -->
<y> -193.68 </y> <!-- value from simulator data -->
<z> -52.38 </z> <!-- BWL 155.72 -->
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> 0 </pitch>
<yaw> 1 </yaw>
</orient>
<feed>3</feed>
<thruster file="direct">
<location unit="IN">
<x> 715.6 </x> <!-- value from simulator data -->
<y> -193.68 </y> <!-- value from simulator data -->
<z> -52.38 </z> <!-- BWL 155.72 -->
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> 0 </pitch>
<yaw> 1 </yaw>
</orient>
</thruster>
</engine>
<engine file="CFM56-7B26">
<location unit="IN">
<x> 715.6 </x> <!-- value from simulator data -->
<y> 193.68 </y> <!-- value from simulator data -->
<z> -52.38 </z> <!-- BWL 155.72 -->
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> 0 </pitch>
<yaw> -1 </yaw>
</orient>
<feed>4</feed>
<thruster file="direct">
<location unit="IN">
<x> 715.6 </x> <!-- value from simulator data -->
<y> 193.68 </y> <!-- value from simulator data -->
<z> -52.38 </z> <!-- BWL 155.72 -->
</location>
<orient unit="DEG">
<roll> 0 </roll>
<pitch> 0 </pitch>
<yaw> -1 </yaw>
</orient>
</thruster>
</engine>
<tank type="FUEL"><!-- Left wing tank -->
<location unit="IN">
<x> 767.01 </x> <!-- based on trimsheet calculation. Correct value -->
<y> -350 </y>
<z> 26.58 </z>
</location>
<drain_location unit="IN">
<x> 703.09</x> <!-- based on trimsheet calculation. Correct value -->
<y> -200 </y>
<z> 10.91 </z>
</drain_location>
<capacity unit="LBS"> 8630 </capacity>
<contents unit="LBS"> 8630 </contents>
<temperature> 59.0 </temperature> <!-- Fuel temp in degrees F -->
</tank>
<tank type="FUEL"><!-- Right wing tank -->
<location unit="IN">
<x> 767.01 </x> <!-- based on trimsheet calculation. Correct value -->
<y> 350 </y>
<z> 26.58 </z>
</location>
<drain_location unit="IN">
<x> 703.09</x> <!-- based on trimsheet calculation. Correct value -->
<y> 200 </y>
<z> 10.91 </z>
</drain_location>
<capacity unit="LBS"> 8630 </capacity>
<contents unit="LBS"> 8630 </contents>
<temperature> 59.0 </temperature> <!-- Fuel temp in degrees F -->
</tank>
<tank type="FUEL"><!-- Center tank -->
<location unit="IN">
<x> 675.41 </x> <!-- based on trimsheet calculation. Correct value -->
<y> 0 </y>
<z> -19.54 </z>
</location>
<drain_location unit="IN">
<x> 675.46 </x> <!-- based on trimsheet calculation. Correct value -->
<y> 0 </y>
<z> -97.4 </z>
</drain_location>
<capacity unit="LBS"> 28803 </capacity>
<contents unit="LBS"> 9000 </contents>
<temperature> 59.0 </temperature> <!-- Fuel temp in degrees F -->
</tank>
<tank type="FUEL"><!-- Feed pipe for left engine -->
<location unit="IN">
<x> 700 </x>
<y>-193 </y>
<z> -40 </z>
</location>
<capacity unit="LBS"> 0.5 </capacity>
<contents unit="LBS"> 0.25 </contents>
</tank>
<tank type="FUEL"><!-- Feed pipe for right engine -->
<location unit="IN">
<x> 700 </x>
<y> 193 </y>
<z> -40 </z>
</location>
<capacity unit="LBS"> 0.5 </capacity>
<contents unit="LBS"> 0.25 </contents>
</tank>
</propulsion>
<ground_reactions>
<contact type="BOGEY" name="NOSE">
<location unit="IN">
<x> 171.97 </x>
<y> 0.00 </y>
<z> -158.74 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 51308.59 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 25654.29 </damping_coeff>
<max_steer unit="DEG"> 5.00 </max_steer>
<brake_group> NONE </brake_group>
<retractable> 1 </retractable>
</contact>
<contact type="BOGEY" name="LEFT_MAIN">
<location unit="IN">
<x> 757.18 </x>
<y> -121.61 </y>
<z> -158.74 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 171028.61 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 85514.30 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group> LEFT </brake_group>
<retractable> 1 </retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MAIN">
<location unit="IN">
<x> 757.18 </x>
<y> 121.61 </y>
<z> -158.74 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 171028.61 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 85514.30 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group> RIGHT </brake_group>
<retractable> 1 </retractable>
</contact>
<contact type="STRUCTURE" name="LEFT_WING">
<location unit="IN">
<x> 728.05 </x>
<y> -675.59 </y>
<z> -33.07 </z>
</location>
<static_friction> 1 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 171028.61 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 171028.61 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_WING">
<location unit="IN">
<x> 728.05 </x>
<y> 675.59 </y>
<z> -33.07 </z>
</location>
<static_friction> 1 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 171028.61 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 171028.61 </damping_coeff>
</contact>
</ground_reactions>
<system file="pushback"/>
<system file="fuel"/>
<system file="fmc"/>
<system file="hydraulics-jsb"/>
<flight_control name="FCS: 737">
<channel name="Pitch">
<summer name="Pitch Trim Sum Cmd">
<input>/controls/flight/elevator-sum</input>
<clipto>
<min>-1</min>
<max> 1</max>
</clipto>
</summer>
<kinematic name="Pitch Trim Sum">
<input>fcs/pitch-trim-sum-cmd</input>
<traverse>
<setting>
<position>-1</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>0.829</time> <!-- from report about Norwegian Air LN-DYM. Rate is 50 deg/sec -->
</setting>
</traverse>
<output>fcs/pitch-trim-sum</output>
</kinematic>
<aerosurface_scale name="Elevator Control">
<input>fcs/pitch-trim-sum</input>
<range>
<min>-0.336</min>
<max> 0.3875</max>
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Elevator Normalized">
<input>fcs/elevator-pos-rad</input>
<domain>
<min>-0.336</min>
<max> 0.3875</max>
</domain>
<range>
<min>-1</min>
<max> 1</max>
</range>
<output>fcs/elevator-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Roll">
<summer name="Roll Trim Sum">
<input>/controls/flight/aileron-sum</input>
<input>fcs/roll-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max> 1</max>
</clipto>
</summer>
<fcs_function name="Left Aileron Control">
<function>
<table>
<independentVar>fcs/roll-trim-sum</independentVar>
<tableData>
-1 -0.3577924967
-0.9195402299 -0.3271881482
-0.8620689655 -0.3028076439
-0.8045977011 -0.2784271396
-0.7471264368 -0.2540448899
-0.6896551724 -0.2296643856
-0.632183908 -0.2078407886
-0.5747126437 -0.1861428554
-0.5172413793 -0.1644445731
-0.4597701149 -0.1427468143
-0.4022988506 -0.1210490556
-0.3448275862 -0.0993512969
-0.2873563218 -0.0792398679
-0.2298850575 -0.0591930161
-0.1724137931 -0.0391461643
-0.1149425287 -0.0198375868
-0.0574712644 -0.000818809
0 0.0181999444
0.0574712644 0.035044117
0.1149425287 0.0518179528
0.1724137931 0.0685919632
0.2298850575 0.085421126
0.2873563218 0.1023026486
0.3448275862 0.1191841713
0.4022988506 0.1345229974
0.4597701149 0.1495581363
0.5172413793 0.1645932751
0.5747126437 0.1796275413
0.632183908 0.1946635528
0.6896551724 0.209697819
0.7471264368 0.2231124196
0.8045977011 0.2363751766
0.8620689655 0.2496361882
0.9195402299 0.2628989452
1 0.2705260341
</tableData>
</table>
</function>
<output>fcs/left-aileron-pos-rad</output>
</fcs_function>
<fcs_function name="Right Aileron Control">
<function>
<table>
<independentVar>fcs/roll-trim-sum</independentVar>
<tableData>
-1 0.2705260341
-0.9195402299 0.2628989452
-0.8620689655 0.2496361882
-0.8045977011 0.2363751766
-0.7471264368 0.2231124196
-0.6896551724 0.209697819
-0.632183908 0.1946635528
-0.5747126437 0.1796275413
-0.5172413793 0.1645932751
-0.4597701149 0.1495581363
-0.4022988506 0.1345229974
-0.3448275862 0.1191841713
-0.2873563218 0.1023026486
-0.2298850575 0.085421126
-0.1724137931 0.0685919632
-0.1149425287 0.0518179528
-0.0574712644 0.035044117
0 0.0181999444
0.0574712644 -0.000818809
0.1149425287 -0.0198375868
0.1724137931 -0.0391461643
0.2298850575 -0.0591930161
0.2873563218 -0.0792398679
0.3448275862 -0.0993512969
0.4022988506 -0.1210490556
0.4597701149 -0.1427468143
0.5172413793 -0.1644445731
0.5747126437 -0.1861428554
0.632183908 -0.2078407886
0.6896551724 -0.2296643856
0.7471264368 -0.2540448899
0.8045977011 -0.2784271396
0.8620689655 -0.3028076439
0.9195402299 -0.3271881482
1 -0.3577924967
</tableData>
</table>
</function>
<output>fcs/right-aileron-pos-rad</output>
</fcs_function>
<aerosurface_scale name="Left aileron Normalized">
<input>fcs/left-aileron-pos-rad</input>
<domain>
<min>-0.3577924967</min>
<max> 0.2705260341</max>
</domain>
<range>
<min>-1</min>
<max> 1</max>
</range>
<output>fcs/left-aileron-pos-norm</output>
</aerosurface_scale>
<aerosurface_scale name="Right aileron Normalized">
<input>fcs/right-aileron-pos-rad</input>
<domain>
<min>-0.3577924967</min>
<max> 0.2705260341</max>
</domain>
<range>
<min>-1</min>
<max> 1</max>
</range>
<output>fcs/right-aileron-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Yaw">
<summer name="Rudder Command Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max> 1</max>
</clipto>
</summer>
<!--Yaw damper-->
<washout_filter name="yaw-wf">
<input>velocities/r-aero-rad_sec</input>
<c1>4</c1>
</washout_filter>
<pure_gain name="Yaw Damper">
<input>fcs/yaw-wf</input>
<gain>5</gain>
</pure_gain>
<!--Slip stabilizer-->
<switch name="accelerations/Ny-switched">
<default value="0.0"/>
<test logic="AND" value="accelerations/Ny">
aero/h_b-mac-ft GE 1
/b737/controls/flight/yaw-damper NE 0
</test>
</switch>
<pid name="fcs/yaw-slip">
<input>accelerations/Ny-switched</input>
<kp> -0.1 </kp>
<ki> 0.05 </ki>
<kd> 0.0 </kd>
<clipto>
<min>-0.12</min>
<max>0.12</max>
</clipto>
<!--<output>fcs/yaw-slip-out</output> possible for debug -->
</pid>
<summer name="Yaw Damper Sum">
<input>fcs/yaw-damper</input>
<input>fcs/yaw-slip</input>
<clipto>
<min>-0.12</min>
<max> 0.12</max>
</clipto>
</summer>
<switch name="Yaw Damper Final">
<default value="0.0"/>
<test value="fcs/yaw-damper-sum">
/b737/controls/flight/yaw-damper ne 0
</test>
</switch>
<summer name="Rudder Sum Cmd">
<input>fcs/rudder-command-sum</input>
<input>fcs/yaw-damper-final</input>
<clipto>
<min>-1</min>
<max> 1</max>
</clipto>
</summer>
<kinematic name="Rudder Sum">
<input>fcs/rudder-sum-cmd</input>
<traverse>
<setting>
<position>-1</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>0.909</time> <!-- from reports about problems with jammed rudder -->
</setting>
</traverse>
<output>fcs/rudder-sum</output>
</kinematic>
<aerosurface_scale name="Rudder Control"> <!-- -30...+30 degrees range -->
<input>fcs/rudder-sum</input>
<range>
<min>-0.523</min>
<max> 0.523</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
<aerosurface_scale name="Rudder Normalized">
<input>fcs/rudder-pos-rad</input>
<domain>
<min>-0.523</min>
<max> 0.523</max>
</domain>
<range>
<min>-1</min>
<max> 1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale>
</channel>
<channel name="Flaps">
<kinematic name="Flaps Control">
<input>fcs/flap-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>0.125</position>
<time>13</time>
</setting>
<setting>
<position>0.25</position>
<time>3</time>
</setting>
<setting>
<position>0.375</position>
<time>4</time>
</setting>
<setting>
<position>0.5</position>
<time>2</time>
</setting>
<setting>
<position>0.625</position>
<time>3</time>
</setting>
<setting>
<position>0.75</position>
<time>2</time>
</setting>
<setting>
<position>0.875</position>
<time>5</time>
</setting>
<setting>
<position>1</position>
<time>5</time>
</setting>
</traverse>
<output>fcs/flap-pos-norm</output>
</kinematic>
</channel>
<channel name="Landing Gear">
<kinematic name="Gear Control">
<input>gear/gear-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>5</time>
</setting>
</traverse>
<output>gear/gear-pos-norm</output>
</kinematic>
</channel>
<channel name="Flight Spoilers">
<!-- operated by the speedbrake handle and roll control -->
<fcs_function name="Outboard spoiler command low">
<function>
<table>
<independentVar>fcs/roll-trim-sum</independentVar>
<tableData>
-0.966 -33.0184
-0.954 -32.5422
-0.839 -25.816
-0.69 -17.9607
-0.483 -10.0735
-0.23 -3.08542
-0.172 -0.734767
-0.161 -0.262478
-0.149 0
0.149 0
0.161 0.262478
0.172 0.734767
0.23 3.08542
0.483 10.0735
0.69 17.9607
0.839 25.816
0.954 32.5422
0.966 33.0184
</tableData>
</table>
</function>
<output>fcs/spoilers-outb-cmd-low</output>
</fcs_function>
<fcs_function name="Outboard spoiler command high">
<function>
<table>
<independentVar>fcs/roll-trim-sum</independentVar>
<tableData>
-0.908 -33.0184
-0.897 -33
-0.885 -32.7384
-0.874 -32.3305
-0.828 -29.3878
-0.69 -21.2068
-0.494 -12.3579
-0.322 -6.87439
-0.207 -3.93022
-0.126 -0
0.126 0
0.207 3.93022
0.322 6.87439
0.494 12.3579
0.69 21.2068
0.828 29.3878
0.874 32.3305
0.885 32.7384
0.897 33
0.908 33.0184
</tableData>
</table>
</function>
<output>fcs/spoilers-outb-cmd-high</output>
</fcs_function>
<pure_gain name="fcs/spoilers-outb-rollpos">
<input>fcs/spoilers-outb-rollpos</input>
<gain>1</gain>
<clipto>
<min>fcs/spoilers-outb-cmd-low</min>
<max>fcs/spoilers-outb-cmd-high</max>
</clipto>
<output>fcs/spoilers-outb-rollpos</output>
</pure_gain>
<fcs_function name="fcs/spoilers-23-pos">
<function>
<sum>
<product>
<property>fcs/spoilers-outb-rollpos</property>
<value>-1</value>
</product>
<table>
<independentVar>/controls/flight/speedbrake-output</independentVar>
<tableData>
0 0
0.65 25
1 33
</tableData>
</table>
</sum>
</function>
<clipto>
<min>0</min>
<max>33</max>
</clipto>
<output>fcs/spoilers-23-pos</output>
</fcs_function>
<fcs_function name="fcs/spoilers-1011-pos">
<function>
<sum>
<product>
<property>fcs/spoilers-outb-rollpos</property>
<value>1</value>
</product>
<table>
<independentVar>/controls/flight/speedbrake-output</independentVar>
<tableData>
0 0
0.65 25
1 33
</tableData>
</table>
</sum>
</function>
<clipto>
<min>0</min>
<max>33</max>
</clipto>
<output>fcs/spoilers-1011-pos</output>
</fcs_function>
<fcs_function name="Inboard spoiler command low">
<function>
<table>
<independentVar>fcs/roll-trim-sum</independentVar>
<tableData>
-0.931 -38.0876
-0.851 -32.9198
-0.759 -27.2137
-0.667 -21.8692
-0.253 -7.35186
-0.172 -4.15259
-0.115 0
0.115 0
0.172 4.15259
0.253 7.35186
0.667 21.8692
0.759 27.2137
0.851 32.9198
0.931 38.0876
</tableData>
</table>
</function>
<output>fcs/spoilers-inbd-cmd-low</output>
</fcs_function>
<fcs_function name="Inboard spoiler command high">
<function>
<table>
<independentVar>fcs/roll-trim-sum</independentVar>
<tableData>
-0.874 -38.0876
-0.839 -37.0523
-0.759 -31.2959
-0.678 -25.9222
-0.575 -20.416
-0.46 -15.5011
-0.345 -11.8071
-0.207 -7.50588
-0.161 -5.15716
-0.08 0
0.08 0
0.161 5.15716
0.207 7.50588
0.345 11.8071
0.46 15.5011
0.575 20.416
0.678 25.9222
0.759 31.2959
0.839 37.0523
0.874 38.0876
</tableData>
</table>
</function>
<output>fcs/spoilers-inbd-cmd-high</output>
</fcs_function>
<pure_gain name="fcs/spoilers-inbd-rollpos">
<input>fcs/spoilers-inbd-rollpos</input>
<gain>1</gain>
<clipto>
<min>fcs/spoilers-inbd-cmd-low</min>
<max>fcs/spoilers-inbd-cmd-high</max>
</clipto>
<output>fcs/spoilers-inbd-rollpos</output>
</pure_gain>
<fcs_function name="fcs/spoilers-45-pos">
<function>
<sum>
<product>
<property>fcs/spoilers-inbd-rollpos</property>
<value>-1</value>
</product>
<table>
<independentVar>/controls/flight/speedbrake-output</independentVar>
<tableData>
0 0
0.65 32
1 38
</tableData>
</table>
</sum>
</function>
<clipto>
<min>0</min>
<max>38</max>
</clipto>
<output>fcs/spoilers-45-pos</output>
</fcs_function>
<fcs_function name="fcs/spoilers-89-pos">
<function>
<sum>
<product>
<property>fcs/spoilers-inbd-rollpos</property>
<value>1</value>
</product>
<table>
<independentVar>/controls/flight/speedbrake-output</independentVar>
<tableData>
0 0
0.65 32
1 38
</tableData>
</table>
</sum>
</function>
<clipto>
<min>0</min>
<max>38</max>
</clipto>
<output>fcs/spoilers-89-pos</output>
</fcs_function>
<kinematic name="Flight Spoilers Control">
<input>/controls/flight/speedbrake-output</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>0.6</time>
</setting>
</traverse>
<output>fcs/speedbrake-pos-norm</output>
</kinematic>
</channel>
<channel name="Ground Spoilers">
<kinematic name="Ground Spoilers Control">
<input>fcs/spoiler-cmd-norm</input>
<traverse>
<setting>
<position>0</position>
<time>0</time>
</setting>
<setting>
<position>1</position>
<time>0.6</time>
</setting>
</traverse>
<output>fcs/spoiler-pos-norm</output>
</kinematic>
</channel>
<channel name="Stabilizer">
<pure_gain name="fcs/stabilizer/trim-rate-per-tick">
<input>fcs/stabilizer/trim-rate</input>
<gain>simulation/dt</gain>
</pure_gain>
<summer name="fcs/stabilizer/errorfree-stab-error">
<input> fcs/stabilizer/stab-target </input>
<input>-fcs/stabilizer-pos-unit </input>
<clipto>
<min>-fcs/stabilizer/trim-rate-per-tick</min>
<max> fcs/stabilizer/trim-rate-per-tick</max>
</clipto>
<output>fcs/stabilizer/stab-error</output>
</summer>
<summer name="fcs/stabilizer/stabilizer-pos-unit">
<input> fcs/stabilizer-pos-unit </input>
<input> fcs/stabilizer/stab-error </input>
<output>fcs/stabilizer-pos-unit</output>
</summer>
<fcs_function name="fcs/stab">
<function>
<product>
<sum>
<property>fcs/stabilizer-pos-unit</property>
<value>-4</value>
</sum>
<value>-1</value>
</product>
</function>
</fcs_function>
</channel>
<channel name="Autobrake">
<switch name="fcs/autobrake/errorfree-target-decel-fps_sec2-filtered">
<default value="fcs/autobrake/target-decel-fps_sec2"/>
<test value="12">
velocities/u-fps LE 134
fcs/autobrake/target-decel-fps_sec2 == 14
</test>
<output>fcs/autobrake/target-decel-fps_sec2-filtered</output>
</switch>
<summer name="fcs/autobrake/time-work">
<input> sim-time-sec </input>
<input>-fcs/autobrake/start-time-sec </input>
</summer>
<pure_gain name="fcs/autobrake/target-decel-15sec">
<input>fcs/autobrake/time-work</input>
<gain>2</gain>
</pure_gain>
<fcs_function name="fcs/autobrake/target-decel-25sec">
<function>
<sum>
<product>
<property>fcs/autobrake/time-work</property>
<sum>
<property>fcs/autobrake/target-decel-fps_sec2-filtered</property>
<value>-3</value>
</sum>
</product>
<sum>
<value>3</value>