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f22-yasim.xml
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f22-yasim.xml
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<!--
=========================================
AeroFab - 2010 - Lockheed-Martin-FA-22A-Raptor Project
=========================================
http://aerofab.webnode.pt/
Creation : April 15, 2010 06:33:00 PM
Last update: November 10, 2010 07:41:02 PM
Revisions :
* October 1, 2010 04:27:45 PM
* November 10, 2010 07:41:02 PM ()
======================================================================
Contributions :
Fabrizio Fracaroli <[email protected] >
======================================================================
/*
* Copyright (c) 2010 Fabrizio Fracaroli <[email protected] >
*
* This file is free software: you may copy, redistribute and/or modify it
* under the terms of the GNU General Public License as published by the
* Free Software Foundation, either version 2 of the License.
*
* This file is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
* General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with this program. If not, see http://www.gnu.org/licenses/ .
*
* This file incorporates work covered by the following copyright and
* permission notice:
*
* Copyright 2010, Fabrizio Fracaroli <[email protected] >
*
* Permission to use, copy, modify, and/or distribute this software
* for any purpose with or without fee is hereby granted, provided
* that the above copyright notice and this permission notice appear
* in all copies.
* THE SOFTWARE IS PROVIDED "AS IS" AND THE AUTHOR DISCLAIMS ALL
* WARRANTIES WITH REGARD TO THIS SOFTWARE INCLUDING ALL IMPLIED
* WARRANTIES OF MERCHANTABILITY AND FITNESS. IN NO EVENT SHALL THE
* AUTHOR BE LIABLE FOR ANY SPECIAL, DIRECT, INDIRECT, OR
* CONSEQUENTIAL DAMAGES OR ANY DAMAGES WHATSOEVER RESULTING FROM LOSS
* OF USE, DATA OR PROFITS, WHETHER IN AN ACTION OF CONTRACT,
* NEGLIGENCE OR OTHER TORTIOUS ACTION, ARISING OUT OF OR IN
* CONNECTION WITH THE USE OR PERFORMANCE OF THIS SOFTWARE.
*/
======================================================================
Reference :
http://en.wikipedia.org/wiki/ -->
<airplane mass="43430">
<!-- Approach configuration -->
<approach speed="145" aoa="8" fuel="1">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<control-setting axis="/controls/flight/speedbrake" value="1"/>
<control-setting axis="/controls/flight/slats" value="1"/>
</approach>
<!-- Cruise configuration. -->
<cruise speed="1000" alt="45000" fuel="0.855">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.90"/>
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.90"/>
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
<control-setting axis="/controls/flight/slats" value="0"/>
</cruise>
<!-- pilot eyepoint -->
<cockpit x="4.47138" y="0" z="-0.016786"/>
<!-- fuselage -->
<fuselage ax="9.46348" ay="0" az="-1.12311"
bx="5.09406" by="0" bz="-0.660128"
width="1.79" taper= "0" midpoint= "1" />
<fuselage ax="5.09406" ay="0" az="-0.660128"
bx="-7.61961" by="0" bz="-0.721073"
width="1.79" taper= "0.5" midpoint= "0" />
<wing x="-2.81409" y="2.0" z="-0.781897"
length="4.7"
chord="7.5"
taper="0.2"
sweep="19"
dihedral="-2"
camber="0.1"
incidence="2.0"
twist="-2.0">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0.0" end="1" lift="1.4" drag="1.8"/>
<flap1 start="0.47" end="0.8" lift="1.5" drag="1.2"/>
<slat aoa="4" start="0.1" end="0.813" lift="1.4" drag="1.3"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/flaps" control="SLAT"/>
<control-output control="FLAP0" prop="/surface-positions/left-flap-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/right-flap-pos-norm"/>
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
<control-output control="SLAT" prop="/surface-positions/slat-pos-norm"/>
<control-speed control="SLAT" transition-time="1.1"/>
<control-speed control="FLAP0" transition-time="1.5"/>
<control-speed control="FLAP1" transition-time="1.5"/>
</wing>
<mstab x="-0.6" y="0.2" z="-0.781897"
length="2"
chord="12"
taper="0.8"
sweep="22"
dihedral="0"
camber="0.1"
incidence="2.0"
twist="-2.0">
<flap0 start="0.0" end="0.5" lift="0.25" drag="2"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="3.0"/>
</mstab>
<hstab x="-7.25" y="2.0" z="-0.75"
taper="0.3"
length="2.51"
chord="3.36"
sweep="25"
dihedral="0"
camber="-0.01"
effectiveness="2.0">
<stall aoa="40.0" width="2" peak="1.2"/>
<flap0 start="0" end="1" lift="2.1" drag="1"/>
<flap1 start="0.0" end="0.15" lift="0.0" drag="10"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP1"/>
<control-output control="FLAP0" side="left" prop="/surface-positions/left-taileron-pos-norm"/>
<control-output control="FLAP0" side="right" prop="/surface-positions/right-taileron-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/taileron-pos-norm"/>
<control-output control="FLAP0" side="left" prop="surface-positions/left-elevator-pos-norm"/>
<control-output control="FLAP0" side="right" prop="surface-positions/right-elevator-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="FLAP0" transition-time="0.5"/>
<control-speed control="FLAP1" transition-time="3.0"/>
</hstab>
<vstab x="-5.8" y="1.42478" z="-0.461207"
taper="0.32"
length="3.1"
chord="4.4"
dihedral="65"
sweep="0" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<flap1 start="0.0" end="0.15" lift="0.0" drag="0.8"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-speed control="FLAP0" transition-time="1"/>
</vstab>
<vstab x="-5.8" y="-1.42478" z="-0.461207"
taper="0.32"
length="3.1"
chord="4.4"
dihedral="115"
sweep="0" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
<flap1 start="0.0" end="0.15" lift="0.0" drag="0.8"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
<control-speed control="FLAP0" transition-time="1"/>
</vstab>
<!--The vectors should be setting to more than 20 degrees for a really vertical climb. I think
If the vectors would be setting to more than 20 degrees You must to change this (src0="-0.75" dst0="0.0" src1="1" dst1="1.0" control="VECTOR")
as this example If you increase the vectors for example 10 degrees so you must to decrease (src0="-0.75") minus 10 degress so it will be like this
(src0="-0.65" dst0="0.0" src1="1" dst1="1.0" control="VECTOR") SRC0="minus zero dot six five (pay attention)
If dont, the animation of the vectors will be wrong
PM for me if you have doubt -->
<jet x="-3.85632" y="-0.65189" z="-0.716246"
mass="3900"
thrust="23500"
afterburner="35000"
n1-idle="55"
n1-max="100"
n2-idle="55"
n2-max="105"
exhaust-speed="4550"
tsfc="0.7"
rotate="20">
<actionpt x="-7.99144" y="-0.65189" z="-0.716246"/>
<control-input axis="/controls/engines/engine[0]/throttle" src0="0.0" dst0="0.0" src1="0.86" dst1="1.0" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/throttle" src0="0.88" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
<control-input axis="/controls/flight/elevator" src0="-0.75" dst0="0.0" src1="1" dst1="1.0" control="VECTOR"/>
<control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
<control-output control="VECTOR" prop="/engines/engine[0]/vector-norm" min="-1" max="1"/>
<control-speed control="THROTTLE" transition-time="1.0"/>
<control-speed control="REHEAT" transition-time="8.0"/>
</jet>
<jet x="-3.85632" y="0.65189" z="-0.716246"
mass="3900"
thrust="23500"
afterburner="35000"
n1-idle="55"
n1-max="100"
n2-idle="55"
n2-max="105"
exhaust-speed="4550"
tsfc="0.7"
rotate="20">
<actionpt x="-7.99144" y="0.65189" z="-0.716246"/>
<control-input axis="/controls/engines/engine[1]/throttle" src0="0.0" dst0="0.0" src1="0.86" dst1="1.0" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/throttle" src0="0.88" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
<control-input axis="/controls/flight/elevator" src0="-0.75" dst0="0.0" src1="1" dst1="1.0" control="VECTOR"/>
<control-output control="REHEAT" prop="engines/engine[1]/afterburner" />
<control-output control="VECTOR" prop="/engines/engine[1]/vector-norm" min="-1" max="1"/>
<control-speed control="THROTTLE" transition-time="1.0"/>
<control-speed control="REHEAT" transition-time="8.0"/>
</jet>
<!-- gear -->
<!-- nose -->
<gear x="3.7" y="0" z="-2.65"
retract-time="8"
compression="0.5" spring="0.5" upx="0" upy="0" upz="0.3">
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- left main -->
<gear x="-2.49889" y="1.9" z="-2.65"
retract-time="8"
compression="0.2"
spring="0.8"
damp="3"
dfric="1.4">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-output control="BRAKE" prop="/gear/gear[1]/brake-position-norm"/>
<control-speed control="EXTEND" transition-time="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<!-- right main -->
<gear x="-2.49889" y="-1.9" z="-2.65"
retract-time="8"
compression="0.2"
spring="0.8"
damp="3"
dfric="1.4">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-output control="BRAKE" prop="/gear/gear[2]/brake-position-norm"/>
<control-speed control="EXTEND" transition-time="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<tank x="3.0232" y="0" z="-0.684553" jet="true" capacity="6500"/>
<tank x="1.01233" y="0" z="-0.641769" jet="true" capacity="3500"/>
<!-- left wing tank -->
<tank x="-2.02343" y="3.7483" z="-0.484877" jet="true" capacity="4000"/>
<!-- right wing tank -->
<tank x="-2.02343" y="-3.7483" z="-0.484877" jet="true" capacity="4000"/>
<!-- drop tanks -->
<tank x="-2.05" y="3.1" z="-1.3" jet="true" capacity="2271"/>
<tank x="-2.05" y="-3.1" z="-1.3" jet="true" capacity="2271"/>
<!-- external loads -->
<!-- left drop tank -->
<weight x="-2.05"
y="3.1"
z="-1.3"
size="0.6"
mass-prop="sim/weight[0]/weight-lb"/>
<weight x="-2.05"
y="2.8"
z="-1.1"
size="0.2"
mass-prop="sim/weight[1]/weight-lb"/>
<weight x="-2.05"
y="3.4"
z="-1.1"
size="0.2"
mass-prop="sim/weight[2]/weight-lb"/>
<!-- left side bay -->
<weight x="1.0"
y="1.4"
z="-1.3"
size="0"
mass-prop="sim/weight[3]/weight-lb"/>
<!-- left belly bay -->
<weight x="0.5"
y="0.7"
z="-1.6"
size="0"
mass-prop="sim/weight[4]/weight-lb"/>
<!-- right belly bay -->
<weight x="0.5"
y="-0.7"
z="-1.6"
size="0"
mass-prop="sim/weight[5]/weight-lb"/>
<!-- left side bay -->
<weight x="1.0"
y="-1.4"
z="-1.3"
size="0"
mass-prop="sim/weight[6]/weight-lb"/>
<weight x="-2.05"
y="-3.4"
z="-1.1"
size="0.2"
mass-prop="sim/weight[7]/weight-lb"/>
<weight x="-2.05"
y="-2.8"
z="-1.1"
size="0.2"
mass-prop="sim/weight[8]/weight-lb"/>
<!-- right drop tank -->
<weight x="-2.05"
y="-3.1"
z="-1.3"
size="0.6"
mass-prop="sim/weight[9]/weight-lb"/>
<ballast x="4.56742" y="0" z="-0.684553" mass ="4650"/>
<ballast x="1.78245" y="0" z="-0.94126" mass ="5000"/>
<ballast x="7.40563" y="0" z="-0.810242" mass ="1995"/>
<!-- Hook -->
<hook x="-5"
y="0.0"
z="-0.861891"
length="3.5"
down-angle="77"
up-angle="-13">
<control-input axis="/controls/gear/tailhook"
control="HEXTEND"/>
<control-speed control="HEXTEND"
transition-time="5"/>
</hook>
</airplane>