746 lines
17 KiB
XML
746 lines
17 KiB
XML
<!-- Airbus A320 FCS -->
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<!--
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##############################################
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# Copyright (c) Joshua Davidson (it0uchpods) #
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##############################################
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-->
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<system name="A320: FCS">
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<channel name="Surface Droop">
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<fcs_function name="hydraulics/aileron-droop">
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<function>
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<table>
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<independentVar lookup="row">/velocities/airspeed-kt</independentVar>
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<tableData>
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62 0.5
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116 0.0
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</tableData>
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</table>
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</function>
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</fcs_function>
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<pure_gain name="hydraulics/aileron-droop-neg">
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<input>hydraulics/aileron-droop</input>
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<gain>-1.0</gain>
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</pure_gain>
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<fcs_function name="hydraulics/elevator-droop">
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<function>
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<table>
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<independentVar lookup="row">/velocities/airspeed-kt</independentVar>
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<tableData>
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72 0.5
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121 0.0
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</tableData>
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</table>
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</function>
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</fcs_function>
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</channel>
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<channel name="Aileron Common">
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<summer name="hydraulics/roll-fbw-summer">
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<input>/controls/flight/roll-fbw</input>
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<input>/controls/flight/aileron-trim</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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</channel>
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<channel name="Aileron L">
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<fcs_function name="hydraulics/aileron-l/extended">
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<function>
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<product>
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<sum>
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<property>/controls/flight/speedbrake-norm</property>
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<max>
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<product>
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<property>hydraulics/roll-fbw-summer</property>
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<value>-1</value>
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</product>
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<value>0</value>
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</max>
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</sum>
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<value>-0.5</value>
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</product>
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</function>
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</fcs_function>
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<fcs_function name="hydraulics/aileron-l/retracted">
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<function>
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<sum>
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<product>
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<property>hydraulics/roll-fbw-summer</property>
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<value>0.5</value>
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</product>
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<table>
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<independentVar lookup="row">/fdm/jsbsim/fcs/flap-pos-deg</independentVar>
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<tableData>
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1 0.00
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5 0.13
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</tableData>
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</table>
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</sum>
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</function>
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</fcs_function>
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<switch name="hydraulics/aileron-l/pressure-switch-or">
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<default value="0"/>
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<test logic="OR" value="1">
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/systems/hydraulic/green-psi GE 1500
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/systems/hydraulic/blue-psi GE 1500
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</test>
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</switch>
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<switch name="hydraulics/aileron-l/switch">
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<default value="hydraulics/aileron-droop"/>
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<test logic="AND" value="hydraulics/aileron-l/extended">
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hydraulics/aileron-l/pressure-switch-or EQ 1
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/controls/flight/speedbrake-norm EQ 1
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/gear/gear[1]/wow EQ 1
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/gear/gear[2]/wow EQ 1
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/systems/failures/aileron-left EQ 0
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</test>
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<test logic="AND" value="hydraulics/aileron-l/retracted">
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hydraulics/aileron-l/pressure-switch-or EQ 1
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/systems/failures/aileron-left EQ 0
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</test>
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<clipto>
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<min>-0.5</min>
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<max>0.5</max>
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</clipto>
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</switch>
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<kinematic name="hydraulics/aileron-l/final">
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<input>hydraulics/aileron-l/switch</input>
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<traverse>
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<setting>
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<position>-1.0</position>
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<time>1.1</time>
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</setting>
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<setting>
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<position>1.0</position>
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<time>1.1</time>
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</setting>
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</traverse>
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<output>/controls/flight/aileron-left</output>
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</kinematic>
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</channel>
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<channel name="Aileron R">
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<fcs_function name="hydraulics/aileron-r/extended">
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<function>
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<product>
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<sum>
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<property>/controls/flight/speedbrake-norm</property>
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<max>
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<property>hydraulics/roll-fbw-summer</property>
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<value>0</value>
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</max>
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</sum>
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<value>0.5</value>
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</product>
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</function>
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</fcs_function>
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<fcs_function name="hydraulics/aileron-r/retracted">
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<function>
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<sum>
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<product>
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<property>hydraulics/roll-fbw-summer</property>
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<value>0.5</value>
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</product>
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<table>
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<independentVar lookup="row">/fdm/jsbsim/fcs/flap-pos-deg</independentVar>
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<tableData>
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1 0.00
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5 -0.13
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</tableData>
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</table>
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</sum>
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</function>
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</fcs_function>
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<switch name="hydraulics/aileron-r/pressure-switch-or">
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<default value="0"/>
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<test logic="OR" value="1">
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/systems/hydraulic/green-psi GE 1500
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/systems/hydraulic/blue-psi GE 1500
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</test>
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</switch>
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<switch name="hydraulics/aileron-r/switch">
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<default value="hydraulics/aileron-droop-neg"/>
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<test logic="AND" value="hydraulics/aileron-r/extended">
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hydraulics/aileron-r/pressure-switch-or EQ 1
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/controls/flight/speedbrake-norm EQ 1
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/gear/gear[1]/wow EQ 1
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/gear/gear[2]/wow EQ 1
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/systems/failures/aileron-right EQ 0
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</test>
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<test logic="AND" value="hydraulics/aileron-r/retracted">
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hydraulics/aileron-r/pressure-switch-or EQ 1
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/systems/failures/aileron-right EQ 0
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</test>
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<clipto>
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<min>-0.5</min>
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<max>0.5</max>
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</clipto>
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</switch>
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<kinematic name="hydraulics/aileron-r/final">
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<input>hydraulics/aileron-r/switch</input>
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<traverse>
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<setting>
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<position>-1.0</position>
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<time>1.1</time>
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</setting>
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<setting>
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<position>1.0</position>
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<time>1.1</time>
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</setting>
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</traverse>
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<output>/controls/flight/aileron-right</output>
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</kinematic>
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</channel>
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<channel name="Roll">
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<fcs_function name="hydraulics/roll-control">
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<function>
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<product>
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<sum>
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<product>
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<sum>
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<property>hydraulics/aileron-l/final</property>
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<property>hydraulics/aileron-r/final</property>
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</sum>
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<value>1.75</value>
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</product>
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<product>
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<sum>
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<product>
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<property>/controls/flight/spoiler-l-sum</property>
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<value>-1.0</value>
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</product>
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<property>/controls/flight/spoiler-r-sum</property>
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</sum>
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<value>0.25</value>
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</product>
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</sum>
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<value>0.444444</value>
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</product>
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</function>
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<clipto>
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<min>-1.0</min>
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<max>1.0</max>
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</clipto>
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</fcs_function>
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<aerosurface_scale name="fcs/roll-pos-rad">
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<input>hydraulics/roll-control</input>
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<range>
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<min>-0.436332</min>
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<max>0.436332</max>
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</range>
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</aerosurface_scale>
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</channel>
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<channel name="Elevator Common">
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<aerosurface_scale name="hydraulics/elevator-fbw-scale">
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<input>/controls/flight/elevator-fbw</input>
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<range>
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<min>-0.6666666666666666666666666666666</min>
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<max>1.0</max>
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</range>
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</aerosurface_scale>
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<switch name="hydraulics/elevator-fbw-switch">
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<default value="hydraulics/elevator-fbw-scale"/>
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<test value="/controls/flight/elevator-fbw">
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/velocities/groundspeed-kt LT 75
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</test>
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</switch>
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<pure_gain name="hydraulics/elevator-fbw-gain">
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<input>hydraulics/elevator-fbw-switch</input>
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<gain>0.5</gain>
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</pure_gain>
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</channel>
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<channel name="Elevator L">
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<switch name="hydraulics/elevator-l/pressure-switch-or">
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<default value="0"/>
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<test logic="OR" value="1">
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/systems/hydraulic/green-psi GE 1500
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/systems/hydraulic/blue-psi GE 1500
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</test>
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</switch>
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<switch name="hydraulics/elevator-l/switch">
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<default value="hydraulics/elevator-droop"/>
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<test logic="AND" value="hydraulics/elevator-fbw-gain">
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hydraulics/elevator-l/pressure-switch-or EQ 1
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/systems/failures/elevator-left EQ 0
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</test>
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<clipto>
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<min>-0.5</min>
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<max>0.5</max>
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</clipto>
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</switch>
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<kinematic name="hydraulics/elevator-l/final">
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<input>hydraulics/elevator-l/switch</input>
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<traverse>
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<setting>
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<position>-1.0</position>
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<time>1.1</time>
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</setting>
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<setting>
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<position>1.0</position>
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<time>1.1</time>
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</setting>
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</traverse>
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<output>/controls/flight/elevator-left</output>
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</kinematic>
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</channel>
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<channel name="Elevator R">
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<switch name="hydraulics/elevator-r/pressure-switch-or">
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<default value="0"/>
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<test logic="OR" value="1">
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/systems/hydraulic/yellow-psi GE 1500
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/systems/hydraulic/blue-psi GE 1500
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</test>
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</switch>
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<switch name="hydraulics/elevator-r/switch">
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<default value="hydraulics/elevator-droop"/>
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<test logic="AND" value="hydraulics/elevator-fbw-gain">
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hydraulics/elevator-r/pressure-switch-or EQ 1
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/systems/failures/elevator-right EQ 0
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</test>
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<clipto>
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<min>-0.5</min>
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<max>0.5</max>
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</clipto>
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</switch>
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<kinematic name="hydraulics/elevator-r/final">
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<input>hydraulics/elevator-r/switch</input>
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<traverse>
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<setting>
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<position>-1.0</position>
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<time>1.1</time>
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</setting>
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<setting>
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<position>1.0</position>
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<time>1.1</time>
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</setting>
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</traverse>
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<output>/controls/flight/elevator-right</output>
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</kinematic>
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</channel>
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<channel name="Pitch">
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<fcs_function name="hydraulics/pitch-control">
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<function>
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<sum>
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<property>hydraulics/elevator-l/final</property>
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<property>hydraulics/elevator-r/final</property>
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</sum>
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</function>
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<clipto>
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<min>-1.0</min>
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<max>1.0</max>
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</clipto>
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</fcs_function>
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<aerosurface_scale name="fcs/pitch-pos-rad">
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<input>hydraulics/pitch-control</input>
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<range>
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<min>-0.523599</min>
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<max>0.296706</max>
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</range>
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</aerosurface_scale>
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<scheduled_gain name="fcs/pitch-pos-geared">
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<input>fcs/pitch-pos-rad</input>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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0 43000
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0.0 1.00 0.850
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0.9 0.02 0.750
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</tableData>
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</table>
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</scheduled_gain>
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</channel>
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<channel name="Pitch Trim">
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<aerosurface_scale name="fcs/pitch-trim-cmd-deg">
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<input>/controls/flight/elevator-trim</input>
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<domain>
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<min>-1.00</min>
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<max>0.32</max>
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</domain>
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<range>
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<min>-12.5</min>
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<max>4.0</max>
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</range>
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</aerosurface_scale>
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<aerosurface_scale name="fcs/pitch-trim-pos-rad">
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<input>/controls/flight/elevator-trim-fdm</input>
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<domain>
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<min>-1.00</min>
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<max>0.32</max>
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</domain>
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<range>
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<min>-0.2181662</min>
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<max>0.0698132</max>
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</range>
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</aerosurface_scale>
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<aerosurface_scale name="fcs/pitch-trim-pos-deg">
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<input>/controls/flight/elevator-trim-fdm</input>
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<domain>
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<min>-1.00</min>
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<max>0.32</max>
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</domain>
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<range>
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<min>-12.5</min>
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<max>4.0</max>
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</range>
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</aerosurface_scale>
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<scheduled_gain name="fcs/pitch-trim-pos-geared">
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<input>fcs/pitch-trim-pos-rad</input>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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0 43000
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0.0 1.00 0.850
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0.9 0.02 0.750
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</tableData>
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</table>
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</scheduled_gain>
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</channel>
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<channel name="FADEC">
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<lag_filter name="fcs/throttle1">
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<input>/controls/engines/engine[0]/throttle-output</input>
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<c1>0.95</c1>
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<output>fcs/throttle-cmd-norm</output>
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<output>fcs/throttle-pos-norm</output>
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</lag_filter>
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<lag_filter name="fcs/throttle2">
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<input>/controls/engines/engine[1]/throttle-output</input>
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<c1>0.95</c1>
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<output>fcs/throttle-cmd-norm[1]</output>
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<output>fcs/throttle-pos-norm[1]</output>
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</lag_filter>
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<lag_filter name="fcs/n1-actual1">
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<input>/engines/engine[0]/n1</input>
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<c1>2.25</c1>
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<output>/engines/engine[0]/n1-actual</output>
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<output>/engines/engine[3]/n1</output>
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</lag_filter>
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<lag_filter name="fcs/n1-actual2">
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<input>/engines/engine[1]/n1</input>
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<c1>2.25</c1>
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<output>/engines/engine[1]/n1-actual</output>
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<output>/engines/engine[4]/n1</output>
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</lag_filter>
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<lag_filter name="fcs/n2-actual1">
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<input>/engines/engine[0]/n2</input>
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<c1>2.25</c1>
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<output>/engines/engine[0]/n2-actual</output>
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<output>/engines/engine[3]/n2</output>
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</lag_filter>
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<lag_filter name="fcs/n2-actual2">
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<input>/engines/engine[1]/n2</input>
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<c1>2.25</c1>
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<output>/engines/engine[1]/n2-actual</output>
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<output>/engines/engine[4]/n2</output>
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</lag_filter>
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</channel>
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<channel name="Rudder">
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<switch name="hydraulics/rudder/pressure-switch-or">
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<default value="0"/>
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<test logic="OR" value="1">
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/systems/hydraulic/green-psi GE 1500
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/systems/hydraulic/blue-psi GE 1500
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/systems/hydraulic/yellow-psi GE 1500
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</test>
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</switch>
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<summer name="hydraulics/rudder/summer">
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<input>/controls/flight/rudder-fbw</input>
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<input>/controls/flight/rudder-trim</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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<switch name="hydraulics/rudder/switch">
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<default value="0"/>
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<test logic="AND" value="hydraulics/rudder/summer">
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hydraulics/rudder/pressure-switch-or EQ 1
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/systems/failures/rudder EQ 0
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</test>
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<clipto>
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<min>-1.0</min>
|
|
<max>1.0</max>
|
|
</clipto>
|
|
</switch>
|
|
|
|
<kinematic name="hydraulics/rudder/final">
|
|
<input>hydraulics/rudder/switch</input>
|
|
<traverse>
|
|
<setting>
|
|
<position>-1.0</position>
|
|
<time>1.1</time>
|
|
</setting>
|
|
<setting>
|
|
<position>1.0</position>
|
|
<time>1.1</time>
|
|
</setting>
|
|
</traverse>
|
|
<output>/controls/flight/rudder-fdm</output>
|
|
</kinematic>
|
|
|
|
</channel>
|
|
|
|
<channel name="Yaw">
|
|
|
|
<pure_gain name="hydraulics/rudder/gain">
|
|
<input>hydraulics/rudder/final</input>
|
|
<gain>-1.0</gain>
|
|
</pure_gain>
|
|
|
|
<scheduled_gain name="fcs/yaw-damper-rate">
|
|
<input>velocities/r-aero-rad_sec</input>
|
|
<table>
|
|
<independentVar lookup="row">velocities/ve-kts</independentVar>
|
|
<tableData>
|
|
30 0.00
|
|
60 2.00
|
|
</tableData>
|
|
</table>
|
|
<clipto>
|
|
<min>-0.05</min>
|
|
<max>0.05</max>
|
|
</clipto>
|
|
</scheduled_gain>
|
|
|
|
<scheduled_gain name="fcs/yaw-damper-final">
|
|
<input>fcs/yaw-damper-rate</input>
|
|
<table>
|
|
<independentVar lookup="row">velocities/ve-kts</independentVar>
|
|
<tableData>
|
|
30 0.0
|
|
31 1.0
|
|
</tableData>
|
|
</table>
|
|
</scheduled_gain>
|
|
|
|
<switch name="fcs/yaw-damper-switch">
|
|
<default value="0"/>
|
|
<test logic="AND" value="fcs/yaw-damper-final">
|
|
/it-fbw/law == 0
|
|
/gear/gear[1]/wow EQ 0
|
|
/gear/gear[2]/wow EQ 0
|
|
</test>
|
|
<test logic="AND" value="fcs/yaw-damper-final">
|
|
/it-fbw/law == 1
|
|
/gear/gear[1]/wow EQ 0
|
|
/gear/gear[2]/wow EQ 0
|
|
</test>
|
|
</switch>
|
|
|
|
<summer name="fcs/yaw-sum">
|
|
<input>hydraulics/rudder/gain</input>
|
|
<input>fcs/yaw-damper-switch</input>
|
|
<clipto>
|
|
<min>-1</min>
|
|
<max>1</max>
|
|
</clipto>
|
|
</summer>
|
|
|
|
<aerosurface_scale name="rubbish/rudder-pos-rad">
|
|
<input>fcs/yaw-sum</input>
|
|
<range>
|
|
<min>-0.436332</min>
|
|
<max>0.436332</max>
|
|
</range>
|
|
<output>fcs/rudder-pos-rad</output>
|
|
</aerosurface_scale>
|
|
|
|
<aerosurface_scale name="rubbish/rudder-pos-norm">
|
|
<input>fcs/rudder-pos-rad</input>
|
|
<domain>
|
|
<min>-0.436332</min>
|
|
<max>0.436332</max>
|
|
</domain>
|
|
<range>
|
|
<min>-1</min>
|
|
<max>1</max>
|
|
</range>
|
|
<output>fcs/rudder-pos-norm</output>
|
|
</aerosurface_scale>
|
|
|
|
</channel>
|
|
|
|
<channel name="Flaps">
|
|
|
|
<kinematic name="rubbish/flap-pos-deg">
|
|
<input>/controls/flight/flaps</input>
|
|
<traverse>
|
|
<setting>
|
|
<position>0</position>
|
|
<time>0</time>
|
|
</setting>
|
|
<setting>
|
|
<position>35</position>
|
|
<time>30</time>
|
|
</setting>
|
|
</traverse>
|
|
<output>fcs/flap-pos-deg</output>
|
|
</kinematic>
|
|
|
|
<aerosurface_scale name="rubbish/flap-pos-norm">
|
|
<input>fcs/flap-pos-deg</input>
|
|
<domain>
|
|
<min>0</min>
|
|
<max>35</max>
|
|
</domain>
|
|
<range>
|
|
<min>0</min>
|
|
<max>1</max>
|
|
</range>
|
|
<output>fcs/flap-pos-norm</output>
|
|
</aerosurface_scale>
|
|
|
|
</channel>
|
|
|
|
<channel name="Slats">
|
|
|
|
<kinematic name="rubbish/slat-pos-deg">
|
|
<input>/controls/flight/slats</input>
|
|
<traverse>
|
|
<setting>
|
|
<position>0</position>
|
|
<time>0</time>
|
|
</setting>
|
|
<setting>
|
|
<position>27</position>
|
|
<time>20</time>
|
|
</setting>
|
|
</traverse>
|
|
<output>fcs/slat-pos-deg</output>
|
|
</kinematic>
|
|
|
|
<aerosurface_scale name="rubbish/slat-pos-norm">
|
|
<input>fcs/slat-pos-deg</input>
|
|
<domain>
|
|
<min>0</min>
|
|
<max>27</max>
|
|
</domain>
|
|
<range>
|
|
<min>0</min>
|
|
<max>1</max>
|
|
</range>
|
|
<output>fcs/slat-pos-norm</output>
|
|
</aerosurface_scale>
|
|
|
|
</channel>
|
|
|
|
<channel name="Landing Gear">
|
|
|
|
<kinematic name="rubbish/gear-pos-norm">
|
|
<input>gear/gear-cmd-norm</input>
|
|
<traverse>
|
|
<setting>
|
|
<position>0</position>
|
|
<time>0</time>
|
|
</setting>
|
|
<setting>
|
|
<position>1</position>
|
|
<time>10</time>
|
|
</setting>
|
|
</traverse>
|
|
<output>gear/gear-pos-norm</output>
|
|
</kinematic>
|
|
|
|
</channel>
|
|
|
|
<channel name="Speedbrake">
|
|
|
|
<pure_gain name="rubbish/speedbrake-pos-norm">
|
|
<input>/controls/flight/speedbrake-output</input>
|
|
<gain>1.0</gain>
|
|
<output>fcs/speedbrake-pos-norm</output>
|
|
</pure_gain>
|
|
|
|
</channel>
|
|
|
|
<channel name="Tiller">
|
|
|
|
<fcs_function name="fcs/steer-nose-deg[0]">
|
|
<function>
|
|
<table>
|
|
<independentVar lookup="row">/velocities/groundspeed-kt</independentVar>
|
|
<independentVar lookup="column">/controls/flight/rudder</independentVar>
|
|
<tableData>
|
|
-1 0 1
|
|
30.000 -70.0 0 70.0
|
|
30.001 -10.0 0 10.0
|
|
</tableData>
|
|
</table>
|
|
</function>
|
|
</fcs_function>
|
|
|
|
<actuator name="fcs/steer-deg">
|
|
<input>fcs/steer-nose-deg[0]</input>
|
|
<rate_limit>70</rate_limit>
|
|
<output>fcs/steer-pos-deg[0]</output>
|
|
</actuator>
|
|
|
|
</channel>
|
|
|
|
</system>
|