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MiG-21bis.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="MiG-21bis" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> David Culp, Petar Jedvaj, Justin Nicholson </author>
<filecreationdate> 26-08-2012 </filecreationdate>
<version>1.10.0</version>
<description> MiG-21bis </description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 247.50 </wingarea>
<wingspan unit="FT" > 23.50 </wingspan>
<wing_incidence> 0.0 </wing_incidence>
<chord unit="FT" > 10.53 </chord>
<htailarea unit="FT2"> 49.50 </htailarea>
<htailarm unit="FT" > 20.68 </htailarm>
<vtailarea unit="FT2"> 29.70 </vtailarea>
<vtailarm unit="FT" > 20.68 </vtailarm>
<location name="AERORP" unit="M">
<x> 0.010 </x>
<y> 0.00 </y>
<z> 0.19160 </z>
</location>
<location name="EYEPOINT" unit="M">
<x>-3.28217 </x>
<y> 0.00 </y>
<z> 0.9944 </z>
</location>
<location name="VRP" unit="M">
<x>0</x>
<y>0</y>
<z>0</z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 4534 </ixx> <!-- source: https://forums.eagle.ru/showthread.php?t=194892 -->
<iyy unit="SLUG*FT2"> 49792 </iyy>
<izz unit="SLUG*FT2"> 56859 </izz>
<ixy unit="SLUG*FT2"> 0 </ixy>
<ixz unit="SLUG*FT2"> 0 </ixz>
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS" > 13457 </emptywt> <!-- source: mig-21 weight and balance document -->
<location name="CG" unit="M"> <!-- source: mig21bis weight and balance document -->
<x> -0.03445 </x>
<y> 0.00 </y>
<z> 0.19160 </z>
</location>
<pointmass name="station1"><!-- left wing outboard pylon pointmass 0 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 1.20 </x>
<y> -2.73 </y>
<z> -0.15 </z>
</location>
</pointmass>
<pointmass name="station2"><!-- left wing inboard pylon pointmass 1 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 0.31 </x>
<y> -2.10 </y>
<z> -0.13 </z>
</location>
</pointmass>
<pointmass name="station3"><!-- empty centerline fuel tank pointmass 2 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 0.05 </x>
<y> 0.00 </y>
<z> -0.60 </z>
</location>
</pointmass>
<pointmass name="station4"><!-- right wing inboard pylon pointmass 3 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 0.31 </x>
<y> 2.10 </y>
<z> -0.13 </z>
</location>
</pointmass>
<pointmass name="station5"><!-- right wing outboard pylon pointmass 4 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 1.20 </x>
<y> 2.73 </y>
<z> -0.15 </z>
</location>
</pointmass>
<pointmass name="station6"><!-- left fuselage attachment point pointmass 5 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 1.54 </x>
<y> -0.49 </y>
<z> -0.15 </z>
</location>
</pointmass>
<pointmass name="station7"><!-- right fuselage attachment point pointmass 6 -->
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="M">
<x> 1.54 </x>
<y> 0.49 </y>
<z> -0.15 </z>
</location>
</pointmass>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE">
<location unit="M">
<x> -4.21 </x>
<y> -0.000 </y>
<z> -1.27543 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 12000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 3000.00 </damping_coeff>
<max_steer unit="DEG">360</max_steer>
<brake_group>CENTER</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MAIN">
<location unit="M">
<x> 0.61490 </x>
<y> -1.47895 </y>
<z> -1.53586 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 16000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 4000.00 </damping_coeff>
<brake_group>LEFT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MAIN">
<location unit="M">
<x> 0.61490 </x>
<y> 1.47895 </y>
<z> -1.53586 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 16000.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 4000.00 </damping_coeff>
<brake_group>RIGHT</brake_group>
<retractable>1</retractable>
</contact>
<contact type="STRUCTURE" name="LEFT_WING">
<location unit="M">
<x> 2.210388 </x>
<y> -3.72501 </y>
<z> 0.03630 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="RIGHT_WING">
<location unit="M">
<x> 2.21038 </x>
<y> 3.72501 </y>
<z> -0.03631 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="NOSE_CONE">
<location unit="M">
<x> -7.87703 </x>
<y> -0.00040 </y>
<z> 0.15073 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="BOT_INTAKE">
<location unit="M">
<x> -6.79990 </x>
<y> -0.00028 </y>
<z> -0.24743 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="LEFT_INTAKE">
<location unit="M">
<x> -6.81026 </x>
<y> -0.42279 </y>
<z> 0.17436 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="UPPER_INTAKE">
<location unit="M">
<x> -6.62056 </x>
<y> -0.00028 </y>
<z> 0.56914 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="RIGHT_INTAKE">
<location unit="M">
<x> -6.81026 </x>
<y> 0.42164 </y>
<z> 0.17436 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="CANOPY">
<location unit="M">
<x> -3.60229 </x>
<y> -0.00040 </y>
<z> 1.40279 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="FVSTAB">
<location unit="M">
<x> 5.47382 </x>
<y>-0.00028 </y>
<z> 2.71926 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="RVSTAB">
<location unit="M">
<x> 7.57439 </x>
<y> -0.00028 </y>
<z> 2.70694 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="CHUTE">
<location unit="M">
<x> 6.67427 </x>
<y> -0.00028 </y>
<z> 0.87715 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="EXHUAST">
<location unit="M">
<x> 6.01530 </x>
<y> -0.00040 </y>
<z> -0.26876 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="LHSTAB">
<location unit="M">
<x> 7.03807 </x>
<y> -1.93076 </y>
<z> 0.26072 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="RHSTAB">
<location unit="M">
<x> 7.03807 </x>
<y> 1.9.015 </y>
<z> 0.26672 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="FLOWERSTAB">
<location unit="M">
<x> 2.91317 </x>
<y> -0.00028 </y>
<z> -0.83579 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="RLOWERSTAB">
<location unit="M">
<x> 5.52340 </x>
<y> -0.00028 </y>
<z> -0.47535 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
<contact type="STRUCTURE" name="PITOT">
<location unit="M">
<x> -8.41349 </x>
<y> 0.21825 </y>
<z> 0.68078 </z>
</location>
<static_friction> 5.0 </static_friction>
<dynamic_friction> 4.0 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<damping_coeff_rebound unit="LBS/FT/SEC"> 25000 </damping_coeff_rebound>
</contact>
</ground_reactions>
<propulsion>
<engine file="Tumansky-R25-300">
<location unit="IN">
<x> 263.40 </x>
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<feed>14</feed>
<thruster file="direct">
<location unit="IN">
<x> 263.40 </x>
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<!--
from http://www.topedge.com/panels/aircraft/sites/kraft/fuel.htm
cutaway to locate tanks: https://s-media-cache-ak0.pinimg.com/originals/d8/41/4a/d8414a7cafc3e42dc42b2f390e1ea563.jpg
more source: mig-21 civil air worthiness doc, item 281.
#1 - cutaway of fuel tanks
#142 - port external fuel tank
#150 - port wing integral fuel tank
#59 - forward fuselage tank
#63 - gravity filler
#72 - starbord wing aft fuel tank
#74 - starbord wing leading edge fuel tank
#57 - external fuel tank
#170 - port leading edge fuel tank
#70 - dorsal tank
#88 - rear fuselage tanks
6 internal tanks ("group 2" is fuel tanks #1-3, "group 3" is fuel tanks #4-6)
4 wing tanks
3 drop tanks
- flow -
all the time:
level the fuel between 1 and 2 and 7
level the fuel between 4, 5, and 6
fuel in 2 pumps into 3
fuel in 3 goes straight to engine
ventral drop tank flows into 2
wing tanks flow into 2
wing drop tanks flow into wing tanks as wing tanks are emptied
#4,5,6 flow into #1
#1,2 emptied
#3 emptied
-->
<!-- Tanks:
0 - internal
1 - internal
2 - internal (Main)
3 - internal
4 - internal
5 - internal
6 - saddle (bis only)
7 - wing 1 left front
8 - wing 2 left rear
9 - wing 3 right front
10 - wing 4 right rear
11 - ventral drop tank
12 - left drop tank
13 - right drop tank
14 - accumulator (feeds 3 to engine via a pump)
***** FUEL AMOUNTS PER TANK ARE FICTIONAL ******* but the total fuel matches what the indicator lights should show
***** LOCATIONS ARE ESTIMATES ***** i didn't have a map of tank 1 is here, tank 2 is there. just a cutaway.
-->
<!-- internal fuel 1 -->
<tank type="FUEL" number="0">
<location unit="M">
<x> -3.20 </x>
<y> 0.00 </y>
<z> 0.50 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 257.57 </capacity>
<contents unit="LBS"> 257.57 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="1">
<location unit="M">
<x> -2.55 </x>
<y> 0.00 </y>
<z> 0.50 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 214.64 </capacity>
<contents unit="LBS"> 214.64 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="2">
<location unit="M">
<x> -1.30 </x>
<y> 0.00 </y>
<z> 0.50 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 128.79 </capacity>
<contents unit="LBS"> 128.79 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="3">
<location unit="M">
<x> -0.35 </x>
<y> 0.00 </y>
<z> 0.45 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 283.33 </capacity>
<contents unit="LBS"> 283.33 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="4">
<location unit="M">
<x> 0.65 </x>
<y> 0.00 </y>
<z> 0.45 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 240.40 </capacity>
<contents unit="LBS"> 240.40 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="5">
<location unit="M">
<x> 1.50 </x>
<y> 0.00 </y>
<z> 0.45 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 171.71 </capacity>
<contents unit="LBS"> 171.71 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="6">
<location unit="M">
<x> -1.75 </x>
<y> 0.00 </y>
<z> 1.12 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 506.56 </capacity>
<contents unit="LBS"> 506.56 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<!-- wing tanks -->
<tank type="FUEL" number="7">
<location unit="M">
<x> -0.89435 </x>
<y> -1.75428</y>
<z> 0.1971 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 858.57 </capacity>
<contents unit="LBS"> 858.57 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="8">
<location unit="M">
<x> 0.49838 </x>
<y> -1.27481 </y>
<z> 0.1971 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 601.00 </capacity>
<contents unit="LBS"> 601.00 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="9">
<location unit="M">
<x> -0.89435 </x>
<y> 1.75428</y>
<z> 0.1971 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 858.57 </capacity>
<contents unit="LBS"> 858.57 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<tank type="FUEL" number="10">
<location unit="M">
<x> 0.49838 </x>
<y> 1.27481 </y>
<z> 0.1971 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 601.00 </capacity>
<contents unit="LBS"> 601.00 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<!-- drop tanks -->
<tank type="FUEL" number="11">
<location unit="IN">
<x> 3.00 </x>
<y> 0.00 </y>
<z> -30.00 </z>
</location>
<priority>2</priority>
<density>6.5</density>
<capacity unit="LBS"> 1400 </capacity>
<contents unit="LBS"> 0 </contents>
</tank>
<tank type="FUEL" number="12">
<location unit="IN">
<x> 21.00 </x>
<y>-120.00 </y>
<z> -10.00 </z>
</location>
<density>6.5</density>
<capacity unit="LBS"> 850 </capacity>
<contents unit="LBS"> 0 </contents>
</tank>
<tank type="FUEL" number="13">
<location unit="IN">
<x> 21.00 </x>
<y> 120.00 </y>
<z> -10.00 </z>
</location>
<density>6.5</density>
<capacity unit="LBS"> 850 </capacity>
<contents unit="LBS"> 0 </contents>
</tank>
<!-- accumulator - inside tank 3 -->
<tank type="FUEL" number="14">
<location unit="M">
<x> -0.50 </x>
<y> 0.00 </y>
<z> 0.50 </z>
</location>
<priority>1</priority>
<density>6.5</density>
<capacity unit="LBS"> 2 </capacity>
<contents unit="LBS"> 2 </contents>
<standpipe unit="LBS"> 0 </standpipe>
</tank>
<dump-rate unit="LBS/MIN"> 1500 </dump-rate>
</propulsion>
<system file="gear"/>
<system file="flaps"/>
<system file="speedbrakes"/>
<system file="FCS-Pitch"/>
<system file="FCS-Roll"/>
<system file="FCS-Yaw"/>
<system file="chute"/>
<system file="canopy"/>
<system file="electric"/>
<system file="fuel"/>
<system file="propulsion"/>
<system file="gyros"/>
<system file="air_intake"/>
<system file="payloads"/>
<system file="hydraulic"/>
<system file="pneumatic"/>
<system file="brakes"/>
<system file="jsb-instrumentation"/>
<system file="warning-lights"/>
<system file="radar-cooling"/>
<system file="external-animation"/>
<system file="headmove"/>
<system file="gyro-compass"/>
<system file="dead-reckoner"/>
<system file="flightdirector"/>
<flight_control name="none"/>
<aerodynamics file="mig-21-aero-aeromatic-v3_3_10.xml"/>
</fdm_config>