ca3963d865
The other stuff isn't really an update but something I did for a bit of a laugh. The idea ocurred to me after animating the folding wings on the seahawk and seeing that the aileron and flap axis still worked...
73 lines
1.8 KiB
XML
Executable file
73 lines
1.8 KiB
XML
Executable file
<?xml version="1.0"?>
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<!--
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************************************************************************
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Hawker Sea Hawk pair simulation config.
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2003-01-09 Lee Elliott leee-fgfs@spatial.freeserve.co.uk
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************************************************************************
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-->
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<PropertyList>
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<sim>
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<flight-model>yasim</flight-model>
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<aero>seahawkpair-yasim</aero>
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<fuel-fraction>1.0</fuel-fraction>
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<sound>
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<audible>true</audible>
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<path>Aircraft/a4/a4-sound.xml</path>
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</sound>
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<panel>
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<path>Aircraft/c310/c310-vfr-panel.xml</path>
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</panel>
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<panel_2>
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<path>Aircraft/c310/c310-mini-panel.xml</path>
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</panel_2>
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<hud>
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<path>Huds/Default/default.xml</path>
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<visibility>true</visibility>
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</hud>
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<model>
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<path>Aircraft/seahawk/seahawkpair-model.xml</path>
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</model>
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<view n="1">
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<config>
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<z-offset-m type="double" archive="y">-80.0</z-offset-m>
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</config>
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</view>
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</sim>
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<autopilot>
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<config>
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<min-climb-speed-kt type="float">100.0</min-climb-speed-kt>
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<best-climb-speed-kt type="float">550.0</best-climb-speed-kt>
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<target-climb-rate-fpm type="float">6000.0</target-climb-rate-fpm>
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<target-descent-rate-fpm type="float">6000.0</target-descent-rate-fpm>
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<elevator-adj-factor type="float">300.0</elevator-adj-factor>
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<integral-contribution type="float">0.005</integral-contribution>
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<max-aileron type="float">0.5</max-aileron>
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<max-roll-deg type="float">60.0</max-roll-deg>
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<roll-out-deg type="float">8</roll-out-deg>
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<roll-out-smooth-deg type="float">15.0</roll-out-smooth-deg>
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<zero-pitch-throttle type="float">0.5</zero-pitch-throttle>
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<zero-pitch-trim-full-throttle type="float">0.001</zero-pitch-trim-full-throttle>
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</config>
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</autopilot>
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</PropertyList>
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