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Merge https://github.com/FGMEMBERS/A320Family

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omega13a 2017-06-09 17:10:50 -07:00
commit bbd4788add
18 changed files with 2425 additions and 3508 deletions
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399
A319-100-CFM.xml
View file

@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
<flight_control name="none"/>
<aerodynamics>
<aerodynamics file="Systems/a319-aerodynamics.xml" />
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00090 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>

399
A319-100-IAE.xml
View file

@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
<flight_control name="none"/>
<aerodynamics>
<aerodynamics file="Systems/a319-aerodynamics.xml" />
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00090 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>

399
A320-200-CFM.xml
View file

@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
<flight_control name="none"/>
<aerodynamics>
<aerodynamics file="Systems/a320-aerodynamics.xml" />
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00090 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>

401
A320-200-IAE.xml
View file

@ -580,390 +580,21 @@ YAW MOI_________3950000______23089847_______24848934
<system file="fcs" />
<flight_control name="none"/>
<aerodynamics file="Systems/a320-aerodynamics.xml" />
<aerodynamics>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00090 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>

15
A320-main.xml
View file

@ -79,16 +79,19 @@
<autopilot n="3">
<path>Aircraft/A320Family/Systems/fmgc-b.xml</path>
</autopilot>
<autopilot n="4">
<autopilot n="4">
<path>Aircraft/A320Family/Systems/fmgc-roll-yaw.xml</path>
</autopilot>
<autopilot n="5">
<path>Aircraft/A320Family/Systems/fmgc-pitch.xml</path>
</autopilot>
<autopilot n="6">
<path>Aircraft/A320Family/Systems/custom-autothrust.xml</path>
</autopilot>
<autopilot n="5">
<autopilot n="7">
<path>Aircraft/A320Family/Systems/libraries.xml</path>
</autopilot>
<autopilot n="6">
<path>Aircraft/A320Family/Systems/fmgc-c.xml</path>
</autopilot>
<autopilot n="7">
<autopilot n="8">
<path>Systems/fl2070_sound.xml</path>
</autopilot>
<property-rule n="100">

399
A321-200-CFM.xml
View file

@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934
<flight_control name="none"/>
<aerodynamics>
<aerodynamics file="Systems/a321-aerodynamics.xml" />
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00090 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>

401
A321-200-IAE.xml
View file

@ -579,391 +579,22 @@ YAW MOI_________3950000______23089847_______24848934
<system file="fmgc" />
<system file="fcs" />
<flight_control name="none"/>
<flight_control name="none" />
<aerodynamics>
<aerodynamics file="Systems/a321-aerodynamics.xml" />
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00090 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00120 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
<external_reactions>
<force name="pushback" frame="BODY">
<location unit="IN">
<x>294</x>
<y>0</y>
<z>-149</z>
</location>
<direction>
<x>1</x>
<y>0</y>
<z>0</z>
</direction>
</force>
</external_reactions>
</fdm_config>

2
AircraftConfig/acconfig.nas
View file

@ -349,7 +349,7 @@ var takeoff = func {
setprop("/controls/flight/flap-pos", 2);
setprop("/controls/flight/flap-txt", "1+F");
libraries.flaptimer.start();
setprop("/controls/flight/elevator-trim", -0.15);
setprop("/controls/flight/elevator-trim", -0.07);
}
});
}

371
Systems/a319-aerodynamics.xml Normal file
View file

@ -0,0 +1,371 @@
<!-- A3XX Aerodynamics -->
<!-- Joshua Davidson (it0uchpods) -->
<aerodynamics>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>

371
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<!-- A3XX Aerodynamics -->
<!-- Joshua Davidson (it0uchpods) -->
<aerodynamics>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>

371
Systems/a321-aerodynamics.xml Normal file
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<!-- A3XX Aerodynamics -->
<!-- Joshua Davidson (it0uchpods) -->
<aerodynamics>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.900
0.00 0.103
0.15 1.600
0.23 1.900
0.60 1.000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">fcs/flap-pos-norm</independentVar>
<tableData>
0.000 0.00000
0.290 0.00250
0.596 0.00700
0.645 0.01300
1.000 0.01700
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_slats">
<description>Delta Lift due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/slat-pos-deg</property>
<value> 0.01000 </value>
</product>
</function>
<function name="aero/force/Lift_speedbrake">
<description>Delta Lift due to speedbrake</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>-0.15</value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value>0.04</value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.260
-0.26 0.018
0.00 0.008
0.26 0.017
1.57 1.320
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.000
0.79 0.000
1.10 0.023
1.80 0.015
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
</product>
</function>
<function name="aero/force/Drag_slats">
<description>Drag due to slats</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.00080 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value>0.025</value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value>0.035</value>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.230
-0.26 0.050
0.00 0.000
0.26 0.050
1.57 1.230
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-norm</property></abs>
<value>0.035</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>-0.1</value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value>-0.95</value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>0.005</value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.20</value>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.003</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value>-0.6</value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.900
2.0 -0.900
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-140</value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-1</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value>0.12</value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value>-0.2</value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0</value>
</product>
</function>
</axis>
</aerodynamics>

7
Systems/fadec-cfm.xml
View file

@ -1,5 +1,8 @@
<?xml version="1.0" encoding="UTF-8"?>
<!-- A3XX CFM56 FADEC -->
<!-- Joshua Davidson -->
<PropertyList>
<filter>
@ -436,7 +439,7 @@
</equals>
<greater-than>
<property>/engines/engine[0]/n1</property>
<value>23</value>
<value>22</value>
</greater-than>
</and>
</condition>
@ -469,7 +472,7 @@
</equals>
<greater-than>
<property>/engines/engine[1]/n1</property>
<value>23</value>
<value>22</value>
</greater-than>
</and>
</condition>

9
Systems/fadec-iae.xml
View file

@ -1,5 +1,8 @@
<?xml version="1.0" encoding="UTF-8"?>
<!-- A3XX IAE V2500 FADEC -->
<!-- Joshua Davidson -->
<PropertyList>
<filter>
@ -702,7 +705,7 @@
</equals>
<greater-than>
<property>/engines/engine[0]/n1</property>
<value>23</value>
<value>22</value>
</greater-than>
</and>
</condition>
@ -735,7 +738,7 @@
</equals>
<greater-than>
<property>/engines/engine[1]/n1</property>
<value>23</value>
<value>22</value>
</greater-than>
</and>
</condition>
@ -755,4 +758,4 @@
<output>/engines/engine[1]/egt-actual</output>
</filter>
</PropertyList>
</PropertyList>

1175
Systems/fmgc-b.xml
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87
Systems/fmgc-c.xml
View file

@ -1,87 +0,0 @@
<?xml version="1.0" encoding="UTF-8"?>
<PropertyList>
<filter>
<name>FMGC MNG SPD</name>
<type>gain</type>
<gain>1</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input>
<expression>
<product>
<table>
<property>/instrumentation/altimeter/indicated-altitude-ft</property>
<entry><ind>10000</ind><dep>286</dep></entry>
<entry><ind>42000</ind><dep>249</dep></entry>
</table>
<table>
<property>/FMGC/internal/cost-index</property>
<entry><ind> 0</ind><dep>1.0</dep></entry>
<entry><ind>120</ind><dep>1.1</dep></entry>
</table>
</product>
</expression>
</input>
<output>/FMGC/internal/mng-alt-spd</output>
</filter>
<filter>
<name>FMGC MNG MACH</name>
<type>gain</type>
<gain>1</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input>
<expression>
<product>
<table>
<property>/instrumentation/altimeter/indicated-altitude-ft</property>
<entry><ind>26000</ind><dep>0.705</dep></entry>
<entry><ind>42000</ind><dep>0.815</dep></entry>
</table>
<table>
<property>/FMGC/internal/cost-index</property>
<entry><ind> 0</ind><dep>0.97</dep></entry>
<entry><ind>120</ind><dep>1.03</dep></entry>
</table>
</product>
</expression>
</input>
<output>/FMGC/internal/mng-alt-mach</output>
</filter>
<filter>
<name>FMGC Target IAS PFD</name>
<type>gain</type>
<gain>1</gain>
<update-interval-secs type="double">0.1</update-interval-secs>
<input>
<condition>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>0</value>
</equals>
</condition>
<property>/it-autoflight/input/spd-kts</property>
</input>
<input>
<condition>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>1</value>
</equals>
</condition>
<expression>
<product>
<div>
<property>/instrumentation/airspeed-indicator/indicated-speed-kt</property>
<property>/instrumentation/airspeed-indicator/indicated-mach</property>
</div>
<property>/it-autoflight/input/spd-mach</property>
</product>
</expression>
</input>
<output>/FMGC/internal/target-ias-pfd</output>
</filter>
</PropertyList>

694
Systems/fmgc-pitch.xml Normal file
View file

@ -0,0 +1,694 @@
<?xml version="1.0"?>
<!-- IT-AUTOFLIGHT -->
<PropertyList>
<!-- =============================================================== -->
<!-- Vertical Modes -->
<!-- =============================================================== -->
<filter>
<name>ALTITUDE CAPTURE/HOLD</name>
<debug>false</debug>
<type>gain</type>
<input>
<property>/it-autoflight/internal/altitude-5-sec-ahead</property>
</input>
<reference>
<property>/it-autoflight/internal/alt</property>
</reference>
<gain>-8</gain>
<output>
<property>/it-autoflight/internal/target-fpm</property>
</output>
<min>
<property>/it-autoflight/internal/min-vs</property>
</min>
<max>
<property>/it-autoflight/internal/max-vs</property>
</max>
</filter>
<pid-controller>
<name>FPA HOLD</name>
<debug>false</debug>
<enable>
<condition>
<and>
<equals>
<property>/it-autoflight/output/vert</property>
<value>5</value>
</equals>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/fpa</property>
</input>
<reference>
<property>/it-autoflight/input/fpa</property>
</reference>
<output>
<property>/it-autoflight/internal/target-pitch-deg</property>
</output>
<config>
<Kp>
<property>/it-autoflight/config/cmd/fpa</property>
</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>1.0</Ti>
<Td>0.00001</Td>
<u_min>
<value>-10</value>
</u_min>
<u_max>
<value>30</value>
</u_max>
</config>
</pid-controller>
<pid-controller>
<name>FLCH SPEED BY PITCH</name>
<debug>false</debug>
<enable>
<condition>
<or>
<equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>7</value>
</equals>
</or>
</condition>
</enable>
<input>
<condition>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>0</value>
</equals>
</condition>
<property>/it-autoflight/internal/lookahead-15-sec-airspeed-kt</property>
</input>
<input>
<condition>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>1</value>
</equals>
</condition>
<property>/it-autoflight/internal/lookahead-15-sec-mach</property>
<scale>500.0</scale>
</input>
<reference>
<condition>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>0</value>
</equals>
</condition>
<property>/it-autoflight/internal/flch-kts</property>
</reference>
<reference>
<condition>
<equals>
<property>/it-autoflight/input/kts-mach</property>
<value>1</value>
</equals>
</condition>
<property>/it-autoflight/internal/flch-mach</property>
<scale>500.0</scale>
</reference>
<output>
<property>/it-autoflight/internal/target-fpm-b</property>
</output>
<config>
<Kp>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</equals>
</condition>
<value>-50</value>
</Kp>
<Kp>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>7</value>
</equals>
</condition>
<value>-60</value>
</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>2.5</Ti>
<Td>0.001</Td>
<u_min>
<condition>
<equals>
<property>/it-autoflight/output/thr-mode</property>
<value>2</value>
</equals>
</condition>
<value>150</value>
</u_min>
<u_min>
<condition>
<equals>
<property>/it-autoflight/output/thr-mode</property>
<value>1</value>
</equals>
</condition>
<value>-6000</value>
</u_min>
<u_max>
<condition>
<and>
<equals>
<property>/it-autoflight/output/thr-mode</property>
<value>2</value>
</equals>
<and>
<equals>
<property>/gear/gear[1]/wow</property>
<value>0</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>0</value>
</equals>
</and>
</and>
</condition>
<value>10000</value>
</u_max>
<u_max>
<condition>
<and>
<equals>
<property>/it-autoflight/output/thr-mode</property>
<value>2</value>
</equals>
<or>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
<value>1000</value>
</u_max>
<u_max>
<condition>
<equals>
<property>/it-autoflight/output/thr-mode</property>
<value>1</value>
</equals>
</condition>
<value>-150</value>
</u_max>
</config>
</pid-controller>
<filter>
<name>AUTOLAND FPM</name>
<type>gain</type>
<gain>1</gain>
<update-interval-secs type="double">0.05</update-interval-secs>
<input>
<expression>
<table>
<property>/position/gear-agl-ft</property>
<entry><ind>100</ind><dep>-600</dep></entry>
<entry><ind> 50</ind><dep>-500</dep></entry>
<entry><ind> 40</ind><dep>-400</dep></entry>
<entry><ind> 30</ind><dep>-300</dep></entry>
<entry><ind> 20</ind><dep>-200</dep></entry>
<entry><ind> 10</ind><dep>-150</dep></entry>
<entry><ind> 5</ind><dep>-100</dep></entry>
</table>
</expression>
</input>
<output>/it-autoflight/internal/target-fpm-c</output>
</filter>
<pid-controller>
<name>FPM HOLD</name>
<debug>false</debug>
<enable>
<condition>
<and>
<or>
<equals>
<property>/it-autoflight/output/vert</property>
<value>0</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>2</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>6</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>7</value>
</equals>
</or>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/vert-speed-fpm</property>
<scale>0.16667</scale>
</input>
<reference>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>0</value>
</equals>
</condition>
<property>/it-autoflight/internal/target-fpm</property>
<scale>0.16667</scale>
</reference>
<reference>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>1</value>
</equals>
</condition>
<property>/it-autoflight/internal/vs</property>
<scale>0.16667</scale>
</reference>
<reference>
<condition>
<or>
<equals>
<property>/it-autoflight/output/vert</property>
<value>4</value>
</equals>
<equals>
<property>/it-autoflight/output/vert</property>
<value>7</value>
</equals>
</or>
</condition>
<property>/it-autoflight/internal/target-fpm-b</property>
<scale>0.16667</scale>
</reference>
<reference>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>6</value>
</equals>
</condition>
<property>/it-autoflight/internal/target-fpm-c</property>
<scale>0.16667</scale>
</reference>
<reference>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>2</value>
</equals>
</condition>
<property>/it-autoflight/internal/nav1-rate-of-climb-fpm</property>
<scale>0.16667</scale>
</reference>
<output>
<property>/it-autoflight/internal/target-pitch-deg</property>
</output>
<config>
<Kp>
<condition>
<not-equals>
<property>/it-autoflight/output/vert</property>
<value>6</value>
</not-equals>
</condition>
<property>/it-autoflight/config/cmd/vs</property>
</Kp>
<Kp>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>6</value>
</equals>
</condition>
<property>/it-autoflight/config/autoland/kp-pitch</property>
</Kp>
<Ti>7.0</Ti>
<Td>0.0001</Td>
<u_min>
<condition>
<not-equals>
<property>/it-autoflight/output/vert</property>
<value>6</value>
</not-equals>
</condition>
<value>-10</value>
</u_min>
<u_min>
<condition>
<equals>
<property>/it-autoflight/output/vert</property>
<value>6</value>
</equals>
</condition>
<value>0</value>
</u_min>
<u_max>
<condition>
<and>
<equals>
<property>/gear/gear[1]/wow</property>
<value>0</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>0</value>
</equals>
</and>
</condition>
<value>30</value>
</u_max>
<u_max>
<condition>
<or>
<equals>
<property>/gear/gear[1]/wow</property>
<value>1</value>
</equals>
<equals>
<property>/gear/gear[2]/wow</property>
<value>1</value>
</equals>
</or>
</condition>
<value>10</value>
</u_max>
</config>
</pid-controller>
<filter>
<name>PITCH DEG SYNC</name>
<debug>false</debug>
<type>gain</type>
<gain>1</gain>
<enable>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</not-equals>
</and>
</condition>
</enable>
<input>/orientation/pitch-deg</input>
<output>/it-autoflight/internal/target-pitch-deg</output>
<min>-15</min>
<max>30</max>
</filter>
<pid-controller>
<name>IT-CONTROLLER: PITCH</name>
<debug>false</debug>
<enable>
<condition>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</condition>
</enable>
<input>
<property>/orientation/pitch-deg</property>
</input>
<reference>
<property>/it-autoflight/internal/target-pitch-deg</property>
</reference>
<output>
<property>/it-autoflight/internal/elevator-cmd</property>
</output>
<config>
<Kp>
<property>/it-autoflight/config/pitch/kp</property>
</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>
<property>/it-autoflight/config/pitch/ti</property>
</Ti>
<Td>
<property>/it-autoflight/config/pitch/td</property>
</Td>
<u_min>
<property>/it-autoflight/config/pitch/umin</property>
</u_min>
<u_max>
<property>/it-autoflight/config/pitch/umax</property>
</u_max>
</config>
</pid-controller>
<filter>
<name>IT-CONTROLLER: PITCH CMD</name>
<debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<enable>
<condition>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/elevator-cmd</property>
</input>
<output>/controls/flight/elevator</output>
<type>noise-spike</type>
<max-rate-of-change>0.4</max-rate-of-change>
</filter>
<!-- =============================================================== -->
<!-- Autotrim -->
<!-- =============================================================== -->
<pid-controller>
<name>AP PITCH HELPER PLUS</name>
<debug>false</debug>
<enable>
<condition>
<and>
<greater-than>
<property>/it-autoflight/internal/elevator-cmd</property>
<value>0.01</value>
</greater-than>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>
<value>0</value>
</input>
<reference>
<value>1</value>
</reference>
<output>
<property>/it-autoflight/internal/elevator-trim-cmd</property>
</output>
<config>
<Kp>0.08</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>10</Ti>
<Td>0.00001</Td>
<u_min>-1.00</u_min>
<u_max>1.00</u_max>
</config>
</pid-controller>
<pid-controller>
<name>AP PITCH HELPER MINUS</name>
<debug>false</debug>
<enable>
<condition>
<and>
<less-than>
<property>/it-autoflight/internal/elevator-cmd</property>
<value>-0.01</value>
</less-than>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>
<value>0</value>
</input>
<reference>
<value>1</value>
</reference>
<output>
<property>/it-autoflight/internal/elevator-trim-cmd</property>
</output>
<config>
<Kp>-0.08</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>10</Ti>
<Td>0.00001</Td>
<u_min>-1.00</u_min>
<u_max>1.00</u_max>
</config>
</pid-controller>
<filter>
<name>IT-CONTROLLER: PITCH TRIM CMD</name>
<debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<enable>
<condition>
<and>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
<or>
<greater-than>
<property>/it-autoflight/internal/elevator-cmd</property>
<value>0.01</value>
</greater-than>
<less-than>
<property>/it-autoflight/internal/elevator-cmd</property>
<value>-0.01</value>
</less-than>
</or>
</and>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/elevator-trim-cmd</property>
</input>
<output>/controls/flight/elevator-trim</output>
<type>noise-spike</type>
<max-rate-of-change>0.01</max-rate-of-change>
</filter>
</PropertyList>

411
Systems/fmgc-roll-yaw.xml Normal file
View file

@ -0,0 +1,411 @@
<?xml version="1.0"?>
<!-- IT-AUTOFLIGHT -->
<PropertyList>
<!-- =============================================================== -->
<!-- Lateral Modes -->
<!-- =============================================================== -->
<pi-simple-controller>
<name>ROLL CONTROLLER: HDG/LNAV</name>
<debug>false</debug>
<enable>
<condition>
<and>
<or>
<equals>
<property>/it-autoflight/output/lat</property>
<value>0</value>
</equals>
<equals>
<property>/it-autoflight/output/lat</property>
<value>1</value>
</equals>
</or>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/heading-error-deg</property>
<scale>
<property>/it-autoflight/config/cmd/roll-scale</property>
</scale>
</input>
<reference>
<value>0</value>
</reference>
<output>
<property>/it-autoflight/internal/target-roll-deg</property>
</output>
<config>
<Kp>
<property>/it-autoflight/config/cmd/roll-kp</property>
</Kp>
<Ki>0.0</Ki>
<min>
<condition>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>1</value>
</not-equals>
</condition>
<property>/it-autoflight/input/bank-limit</property>
<scale>-1</scale>
</min>
<min>
<condition>
<equals>
<property>/it-autoflight/output/lat</property>
<value>1</value>
</equals>
</condition>
<value>-25</value>
</min>
<max>
<condition>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>1</value>
</not-equals>
</condition>
<property>/it-autoflight/input/bank-limit</property>
</max>
<max>
<condition>
<equals>
<property>/it-autoflight/output/lat</property>
<value>1</value>
</equals>
</condition>
<value>25</value>
</max>
</config>
</pi-simple-controller>
<pid-controller>
<name>VORLOC TRK</name>
<debug>false</debug>
<enable>
<condition>
<and>
<equals>
<property>/it-autoflight/output/lat</property>
<value>2</value>
</equals>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</equals>
</or>
</and>
</condition>
</enable>
<input>
<condition>
<equals>
<property>/it-autoflight/settings/use-backcourse</property>
<value>0</value>
</equals>
</condition>
<property>/it-autoflight/internal/nav-heading-error-deg</property>
</input>
<input>
<condition>
<equals>
<property>/it-autoflight/settings/use-backcourse</property>
<value>1</value>
</equals>
</condition>
<property>/it-autoflight/internal/nav-bc-heading-error-deg</property>
</input>
<reference>
<value>0.0</value>
</reference>
<output>
<property>/it-autoflight/internal/target-roll-deg</property>
</output>
<config>
<Kp>
<property>/it-autoflight/config/cmd/vorloc</property>
</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>10.0</Ti>
<Td>0.00001</Td>
<u_min>-25</u_min>
<u_max>25</u_max>
</config>
</pid-controller>
<filter>
<name>ROLL DEG SYNC</name>
<debug>false</debug>
<type>gain</type>
<gain>1</gain>
<enable>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd1</property>
<value>1</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/fd2</property>
<value>1</value>
</not-equals>
</and>
</condition>
</enable>
<input>/orientation/roll-deg</input>
<output>/it-autoflight/internal/target-roll-deg</output>
<min>-25</min>
<max>25</max>
</filter>
<filter>
<name>IT-CONTROLLER: TARGET ROLL CMD</name>
<debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<input>
<property>/it-autoflight/internal/target-roll-deg</property>
</input>
<output>/it-autoflight/internal/target-roll</output>
<type>noise-spike</type>
<max-rate-of-change>6</max-rate-of-change>
</filter>
<pid-controller>
<name>IT-CONTROLLER: ROLL</name>
<debug>false</debug>
<enable>
<condition>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</condition>
</enable>
<input>
<property>/orientation/roll-deg</property>
</input>
<reference>
<condition>
<and>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</not-equals>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>5</value>
</not-equals>
</and>
</condition>
<property>/it-autoflight/internal/target-roll</property>
</reference>
<reference>
<condition>
<or>
<equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</equals>
<equals>
<property>/it-autoflight/output/lat</property>
<value>5</value>
</equals>
</or>
</condition>
<value>0</value>
</reference>
<output>
<property>/it-autoflight/internal/aileron-cmd</property>
</output>
<config>
<Kp>
<condition>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>2</value>
</not-equals>
</condition>
<property>/it-autoflight/config/roll/kp</property>
</Kp>
<Kp>
<condition>
<equals>
<property>/it-autoflight/output/lat</property>
<value>2</value>
</equals>
</condition>
<property>/it-autoflight/config/roll/kp-vloc</property>
</Kp>
<beta>1.0</beta>
<alpha>0.1</alpha>
<gamma>0.0</gamma>
<Ti>
<property>/it-autoflight/config/roll/ti</property>
</Ti>
<Td>
<property>/it-autoflight/config/roll/td</property>
</Td>
<u_min>
<property>/it-autoflight/config/roll/umin</property>
</u_min>
<u_max>
<property>/it-autoflight/config/roll/umax</property>
</u_max>
</config>
</pid-controller>
<filter>
<name>IT-CONTROLLER: ROLL CMD</name>
<debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<enable>
<condition>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/aileron-cmd</property>
</input>
<output>/controls/flight/aileron</output>
<type>noise-spike</type>
<max-rate-of-change>0.5</max-rate-of-change>
</filter>
<!-- =============================================================== -->
<!-- Yaw Control -->
<!-- =============================================================== -->
<pi-simple-controller>
<name>RUDDER VORLOC TRK</name>
<debug>false</debug>
<enable>
<condition>
<equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</equals>
</condition>
</enable>
<input>
<property>/it-autoflight/internal/nav-heading-error-deg</property>
</input>
<reference>
<value>0</value>
</reference>
<output>/it-autoflight/internal/rudder-cmd</output>
<config>
<Kp>
<property>/it-autoflight/config/autoland/kp-rudder</property>
</Kp>
<Ki>0</Ki>
</config>
<min>-0.25</min>
<max>0.25</max>
</pi-simple-controller>
<filter>
<name>IT-CONTROLLER: RUDDER CMD</name>
<debug>false</debug>
<feedback-if-disabled>true</feedback-if-disabled>
<initialize-to>output</initialize-to>
<enable>
<condition>
<or>
<equals>
<property>/it-autoflight/output/ap1</property>
<value>1</value>
</equals>
<equals>
<property>/it-autoflight/output/ap2</property>
<value>1</value>
</equals>
</or>
</condition>
</enable>
<input>
<condition>
<not-equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</not-equals>
</condition>
<value>0</value>
</input>
<input>
<condition>
<equals>
<property>/it-autoflight/output/lat</property>
<value>4</value>
</equals>
</condition>
<property>/it-autoflight/internal/rudder-cmd</property>
</input>
<output>/controls/flight/rudder</output>
<type>noise-spike</type>
<max-rate-of-change>0.20</max-rate-of-change>
</filter>
</PropertyList>

22
Systems/it-fbw.xml
View file

@ -1,4 +1,4 @@
<!-- Airbus A3XX FBW System by Joshua Davidson (it0uchpods) and Richard Harrison (richard) -->
<!-- Airbus A3XX FBW System by Joshua Davidson (it0uchpods) -->
<system name="it-fbw">
<property value="0">/it-fbw/law</property>
@ -100,19 +100,19 @@
<table>
<independentVar lookup="row">/controls/flight/elevator-input</independentVar>
<tableData>
-1.0 0.0750
-0.7 0.0530
-0.5 0.0220
-0.3 0.0110
-0.15 0.0040
-1.0 0.0755
-0.7 0.0535
-0.5 0.0225
-0.3 0.0115
-0.15 0.0045
-0.05 0.0007
0.00 0.0000
0.05 -0.0007
0.15 -0.0040
0.3 -0.0110
0.5 -0.0220
0.7 -0.0530
1.0 -0.0750
0.15 -0.0045
0.3 -0.0115
0.5 -0.0225
0.7 -0.0535
1.0 -0.0755
</tableData>
</table>
</sum>