Flap and Slat separation
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JWocky
parent
2becd9ade9
commit
88f47ebcbb
1 changed files with 131 additions and 77 deletions
208
A320-200-IAE.xml
208
A320-200-IAE.xml
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@ -411,7 +411,7 @@ YAW MOI_________3950000______23089847_______24848934
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<engine file="v2527_a5">
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<location unit="IN">
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<x> 630.0683 </x>
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<x> 620.0683 </x>
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<y> -226.575 </y>
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<z> -45.567 </z>
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</location>
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@ -425,7 +425,7 @@ YAW MOI_________3950000______23089847_______24848934
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<feed>2</feed>
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<thruster file="direct">
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<location unit="IN">
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<x> 642.4820 </x>
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<x> 640.4820 </x>
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<y> -226.575 </y>
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<z> -45.567 </z>
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</location>
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@ -439,7 +439,7 @@ YAW MOI_________3950000______23089847_______24848934
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<engine file="v2527_a5">
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<location unit="IN">
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<x> 630.00683 </x>
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<x> 620.00683 </x>
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<y> 226.575 </y>
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<z> -45.567 </z>
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</location>
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@ -453,7 +453,7 @@ YAW MOI_________3950000______23089847_______24848934
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<feed>4</feed>
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<thruster file="direct">
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<location unit="IN">
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<x> 642.4820 </x>
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<x> 640.4820 </x>
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<y> 226.575 </y>
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<z> -45.567 </z>
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</location>
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@ -472,7 +472,7 @@ YAW MOI_________3950000______23089847_______24848934
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<y> -574.4148 </y>
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<z> 3.1080 </z>
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</location>
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<capacity unit="LBS"> 0 </capacity><!-- need review -->
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<capacity unit="LBS"> 150 </capacity><!-- need review -->
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<contents unit="LBS"> 0 </contents>
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<priority>4</priority>
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@ -550,7 +550,7 @@ YAW MOI_________3950000______23089847_______24848934
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<y> 574.4148 </y>
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<z> 3.1080 </z>
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</location>
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<capacity unit="LBS"> 0 </capacity><!-- need review -->
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<capacity unit="LBS"> 150 </capacity><!-- need review -->
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<contents unit="LBS"> 0 </contents>
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<priority>4</priority>
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<type>JET-A1</type>
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@ -803,79 +803,113 @@ YAW MOI_________3950000______23089847_______24848934
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</channel>
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<channel name="Flaps">
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<channel name="Flaps">
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<kinematic name="Flaps Control">
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<input>fcs/flap-cmd-norm</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>40</position>
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<time>40</time>
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</setting>
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</traverse>
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<output>fcs/flap-pos-deg</output>
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</kinematic>
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<kinematic name="Flaps Control">
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<input>/controls/flight/flaps</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>40</position>
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<time>40</time>
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</setting>
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</traverse>
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<output>fcs/flap-pos-deg</output>
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</kinematic>
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<aerosurface_scale name="Flap position normalized">
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<input>fcs/flap-pos-deg</input>
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<domain>
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<min>0</min>
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<max>40</max>
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</domain>
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<range>
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<min>0</min>
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<max>1</max>
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</range>
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<output>fcs/flap-pos-norm</output>
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</aerosurface_scale>
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<aerosurface_scale name="Flap position normalized">
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<input>fcs/flap-pos-deg</input>
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<domain>
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<min>0</min>
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<max>40</max>
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</domain>
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<range>
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<min>0</min>
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<max>1</max>
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</range>
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<output>fcs/flap-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Slats">
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<kinematic name="Slats Control">
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<input>/controls/flight/slats</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>40</position>
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<time>40</time>
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</setting>
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</traverse>
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<output>fcs/slat-pos-deg</output>
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</kinematic>
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<aerosurface_scale name="Slat position normalized">
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<input>fcs/slat-pos-deg</input>
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<domain>
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<min>0</min>
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<max>27</max>
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</domain>
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<range>
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<min>0</min>
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<max>1</max>
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</range>
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<output>fcs/slat-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Landing Gear">
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<kinematic name="Gear Control">
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<input>gear/gear-cmd-norm</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>1</position>
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<time>10</time>
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</setting>
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</traverse>
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<output>gear/gear-pos-norm</output>
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</kinematic>
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<kinematic name="Gear Control">
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<input>gear/gear-cmd-norm</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>1</position>
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<time>10</time>
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</setting>
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</traverse>
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<output>gear/gear-pos-norm</output>
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</kinematic>
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</channel>
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<channel name="Speedbrake">
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<kinematic name="Speedbrake">
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<input>fcs/speedbrake-cmd-norm</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>1</position>
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<time>2</time>
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</setting>
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</traverse>
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<output>fcs/speedbrake-pos-norm</output>
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</kinematic>
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<kinematic name="Speedbrake">
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<input>fcs/speedbrake-cmd-norm</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>1</position>
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<time>2</time>
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</setting>
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</traverse>
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<output>fcs/speedbrake-pos-norm</output>
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</kinematic>
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</channel>
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<channel name="Tiller">
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<channel name="Tiller">
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<switch name="/controls/gear/tiller-disabled">
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<default value="0"/>
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<test logic="AND" value="1">
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/controls/gear/tiller-enabled == 0
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</test>
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</switch>
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<default value="0"/>
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<test logic="AND" value="1">
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/controls/gear/tiller-enabled == 0
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</test>
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</switch>
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<fcs_function name="Nose Wheel Steering 0">
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<function name="fcs/steer-nose-deg[0]">
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@ -930,10 +964,10 @@ YAW MOI_________3950000______23089847_______24848934
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<table>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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-0.20 -0.880
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0.00 0.450
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0.23 1.500
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0.60 0.900
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-0.20 -0.780
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0.00 0.375
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0.23 1.300
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0.60 0.700
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</tableData>
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</table>
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</product>
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@ -945,7 +979,17 @@ YAW MOI_________3950000______23089847_______24848934
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
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<value> 0.03500 </value>
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<value> 0.02000 </value>
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</product>
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</function>
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<function name="aero/force/Lift_slats">
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<description>Delta Lift due to slats</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
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<value> 0.01800 </value>
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</product>
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</function>
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@ -965,7 +1009,7 @@ YAW MOI_________3950000______23089847_______24848934
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/elevator-pos-rad</property>
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<value>0.25</value>
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<value>0.15</value>
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</product>
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</function>
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@ -983,7 +1027,7 @@ YAW MOI_________3950000______23089847_______24848934
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<tableData>
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-1.57 1.300
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-0.26 0.021
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0.00 0.015
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0.00 0.012
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0.26 0.021
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1.57 1.300
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</tableData>
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@ -1024,7 +1068,17 @@ YAW MOI_________3950000______23089847_______24848934
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
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<value> 0.00197 </value>
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<value> 0.00150 </value>
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</product>
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</function>
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<function name="aero/force/Drag_slats">
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<description>Drag due to slats</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/flap-pos-deg</property>
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<value> 0.00150 </value>
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</product>
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</function>
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@ -1034,7 +1088,7 @@ YAW MOI_________3950000______23089847_______24848934
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>gear/gear-pos-norm</property>
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<value>0.025</value>
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<value>0.020</value>
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</product>
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</function>
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@ -1072,7 +1126,7 @@ YAW MOI_________3950000______23089847_______24848934
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<abs><property>fcs/elevator-pos-norm</property></abs>
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<value>0.04</value>
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<value>0.045</value>
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</product>
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</function>
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