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dpculp
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A few generic systems.
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‎systems/BLC.xml

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<?xml version="1.0"?>
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<!-- This system determines the state of the Boundary Layer Control (BLC)
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system. The aerodynamic effects of BLC are set in the aircraft
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configuration file <aerodynamics> section, not here. In order for
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the switch to work properly the number of engine rpm tests should
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match the number of engines installed!
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-->
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<system name="BLC">
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<property>systems/BLC/active</property>
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<channel name="Boundary Layer Control">
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<switch name="systems/BLC/switch">
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<default value="0"/>
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<test logic="AND" value="1">
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fcs/flap-pos-norm gt 0.51
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propulsion/engine[0]/n2 gt 70.0
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propulsion/engine[1]/n2 gt 70.0
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</test>
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<output>systems/BLC/active</output>
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</switch>
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</channel>
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</system>

‎systems/FCS-pitch.xml

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<?xml version="1.0"?>
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<system name="FCS-pitch">
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<channel name="Pitch">
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<summer name="Pitch Trim Sum">
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<input>fcs/elevator-cmd-norm</input>
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<input>fcs/pitch-trim-cmd-norm</input>
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<clipto>
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<min> -1 </min>
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<max> 1 </max>
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</clipto>
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</summer>
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<aerosurface_scale name="Elevator Control">
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<input>fcs/pitch-trim-sum</input>
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<range>
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<min> -0.35 </min>
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<max> 0.30 </max>
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</range>
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<output>fcs/elevator-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="elevator normalized">
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<input>fcs/elevator-pos-rad</input>
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<domain>
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<min>-0.35</min>
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<max> 0.35</max>
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</domain>
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<range>
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<min>-1</min>
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<max> 1</max>
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</range>
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<output>fcs/elevator-pos-norm</output>
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</aerosurface_scale>
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</channel>
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</system>

‎systems/FCS-roll.xml

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<?xml version="1.0"?>
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<system name="FCS-roll">
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<channel name="Roll">
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<summer name="Roll Trim Sum">
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<input>fcs/aileron-cmd-norm</input>
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<input>fcs/roll-trim-cmd-norm</input>
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<clipto>
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<min> -1 </min>
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<max> 1 </max>
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</clipto>
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</summer>
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<aerosurface_scale name="Left Aileron Control">
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<input>fcs/roll-trim-sum</input>
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<range>
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<min> -0.35 </min>
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<max> 0.35 </max>
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</range>
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<output>fcs/left-aileron-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Right Aileron Control">
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<input>fcs/roll-trim-sum</input>
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<range>
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<min> -0.35 </min>
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<max> 0.35 </max>
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</range>
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<output>fcs/right-aileron-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="left aileron normalized">
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<input>fcs/left-aileron-pos-rad</input>
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<domain>
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<min>-0.35</min>
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<max> 0.35</max>
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</domain>
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<range>
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<min>-1</min>
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<max> 1</max>
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</range>
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<output>fcs/left-aileron-pos-norm</output>
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</aerosurface_scale>
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<aerosurface_scale name="right aileron normalized">
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<input>fcs/right-aileron-pos-rad</input>
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<domain>
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<min>-0.35</min>
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<max> 0.35</max>
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</domain>
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<range>
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<min>-1</min>
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<max> 1</max>
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</range>
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<output>fcs/right-aileron-pos-norm</output>
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</aerosurface_scale>
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</channel>
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</system>

‎systems/FCS-yaw.xml

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<?xml version="1.0"?>
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<system name="FCS-yaw">
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<channel name="Yaw">
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<summer name="Rudder Command Sum">
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<input>fcs/rudder-cmd-norm</input>
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<input>fcs/yaw-trim-cmd-norm</input>
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<limit>
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<min> -1.0 </min>
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<max> 1.0 </max>
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</limit>
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</summer>
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<scheduled_gain name="Yaw Damper Rate">
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<input>velocities/r-aero-rad_sec</input>
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<table>
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<independentVar lookup="row">velocities/ve-kts</independentVar>
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<tableData>
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30 0.00
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60 2.00
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</tableData>
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</table>
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</scheduled_gain>
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<scheduled_gain name="Yaw Damper Beta">
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<input>aero/beta-rad</input>
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<table>
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<independentVar lookup="row">velocities/ve-kts</independentVar>
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<tableData>
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30 0.00
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60 0.00
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</tableData>
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</table>
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</scheduled_gain>
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<summer name="Yaw Damper Sum">
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<input>fcs/yaw-damper-beta</input>
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<input>fcs/yaw-damper-rate</input>
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<limit>
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<min> -0.1 </min>
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<max> 0.1 </max>
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</limit>
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</summer>
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<scheduled_gain name="Yaw Damper Final">
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<input>fcs/yaw-damper-sum</input>
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<table>
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<independentVar lookup="row">velocities/ve-kts</independentVar>
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<tableData>
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30 0.0
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31 1.0
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</tableData>
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</table>
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</scheduled_gain>
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<summer name="Rudder Sum">
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<input>fcs/rudder-command-sum</input>
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<input>fcs/yaw-damper-final</input>
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<limit>
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<min> -1 </min>
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<max> 1 </max>
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</limit>
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</summer>
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<aerosurface_scale name="Rudder Control">
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<input>fcs/rudder-sum</input>
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<domain>
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<min>-1.0</min>
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<max> 1.0</max>
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</domain>
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<range>
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<min> -0.25 </min>
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<max> 0.25 </max>
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</range>
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<output>fcs/rudder-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="rudder normalized">
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<input>fcs/rudder-pos-rad</input>
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<domain>
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<min>-0.25</min>
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<max> 0.25</max>
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</domain>
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<range>
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<min>-1</min>
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<max> 1</max>
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</range>
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<output>fcs/rudder-pos-norm</output>
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</aerosurface_scale>
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</channel>
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</system>

‎systems/NWS.xml

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<?xml version="1.0"?>
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<system name="NWS">
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<property>systems/NWS/engaged</property>
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<channel name="Nose Wheel Steering">
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<scheduled_gain name="systems/NWS/steer-cmd">
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<input>fcs/rudder-cmd-norm</input>
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<table>
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<independentVar lookup="row">systems/NWS/engaged</independentVar>
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<tableData>
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0 -0.1
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1 -1.0
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</tableData>
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</table>
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<output>fcs/steer-cmd-norm</output>
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</scheduled_gain>
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</channel>
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</system>

‎systems/catapult.xml

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<?xml version="1.0"?>
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<system name="catapult">
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<channel name="Catapult">
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<switch name="systems/catapult/cat-cmd-norm">
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<default value="0"/>
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<test logic="AND" value="0">
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systems/catapult/cat-pos-norm gt 0.999
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</test>
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<test logic="AND" value="1">
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systems/catapult/cat-launch-cmd == 1
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</test>
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<output>systems/catapult/cat-launch-cmd</output>
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</switch>
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<kinematic name="systems/catapult/cat-timer">
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<input>systems/catapult/cat-cmd-norm</input>
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<traverse>
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<setting>
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<position>0.0</position>
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<time>0.0</time>
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</setting>
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<setting>
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<position>1.0</position>
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<time>2.7</time>
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</setting>
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</traverse>
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<output>systems/catapult/cat-pos-norm</output>
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</kinematic>
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<pure_gain name="systems/catapult/cat-force">
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<input>inertia/weight-lbs</input>
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<gain>2.0</gain>
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</pure_gain>
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<switch name="systems/catapult/cat-final">
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<default value="0"/>
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<test logic="AND" value="systems/catapult/cat-force">
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systems/catapult/cat-launch-cmd == 1
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systems/catapult/cat-pos-norm lt 0.999
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systems/catapult/cat-pos-norm gt 0.0
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</test>
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<output>external_reactions/catapult/magnitude</output>
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</switch>
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</channel>
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</system>

‎systems/flaps.xml

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<?xml version="1.0"?>
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<system name="flaps">
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<channel name="Flaps">
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<kinematic name="Flaps Control">
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<input>fcs/flap-cmd-norm</input>
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<traverse>
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<setting>
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<position> 0 </position>
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<time> 0 </time>
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</setting>
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<setting>
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<position> 0.5</position>
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<time> 4 </time>
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</setting>
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<setting>
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<position> 1</position>
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<time> 5 </time>
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</setting>
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</traverse>
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<output>fcs/flap-pos-norm</output>
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</kinematic>
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</channel>
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</system>

‎systems/gear.xml

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<?xml version="1.0"?>
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<system name="gear">
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<channel name="Landing Gear">
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<kinematic name="Gear Control">
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<input>gear/gear-cmd-norm</input>
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<traverse>
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<setting>
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<position> 0 </position>
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<time> 0 </time>
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</setting>
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<setting>
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<position> 1 </position>
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<time> 5 </time>
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</setting>
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</traverse>
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<output>gear/gear-pos-norm</output>
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</kinematic>
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</channel>
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</system>

‎systems/holdback.xml

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<?xml version="1.0"?>
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<system name="holdback">
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<channel name="Holdback_Launchbar">
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<summer name="systems/holdback/total_thrust">
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<input>propulsion/engine/thrust</input>
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<input>propulsion/engine[1]/thrust</input>
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</summer>
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<switch name="systems/holdback/switch">
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<default value="0"/>
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<test logic="AND" value="systems/holdback/total_thrust">
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systems/holdback/holdback-cmd == 1
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</test>
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<output>external_reactions/holdback/magnitude</output>
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</switch>
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</channel>
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</system>

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