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List: flightgear-cvs
Subject: [Flightgear-cvslogs] CVS: data/Aircraft/F80C F80C-electrical.xml,
From: "Curtis L. Olson" <curt () flightgear ! org>
Date: 2005-12-20 16:05:55
Message-ID: E1Eojzv-00029m-00 () baron ! me ! umn ! edu
[Download RAW message or body]
Update of /var/cvs/FlightGear-0.9/data/Aircraft/F80C
In directory baron:/tmp/cvs-serv7744
Added Files:
F80C-electrical.xml F80C-set.xml F80C.xml submodels.xml
thumbnail.jpg
Log Message:
Dave Culp:
I've just completed a Lockheed F-80C Shooting Star.
http://home.comcast.net/~davidculp2/F80C.tar.gz
screenshot:
http://home.comcast.net/~davidculp2/P80C-001.jpg
The exterior model was originally done by Massimo Taccoli, who has done
several very nice models for MSFS, and has given me permission to convert it
for use in FlightGear and release the resulting model under GPL. The FDM is
JSBSim, based on Aero-Matic output with a couple tweaks. It runs here in CVS
FlightGear, and should run in 0.9.8 and later?
It's a no-brainer to fly. Engine is running at startup, and flaps are set at
half (takeoff position). Check out the gunsight (you have to turn it on by
clicking on the on/off switch). It has auto-depression for g-load.
--- NEW FILE ---
<?xml version="1.0"?>
<!-- T38 electrical system
David Culp, March 2003, davidculp2@attbi.com
This system is a generic system of the kind one would find
on a twin-jet aircraft. FlightGear is presently supporting
only C-172 style electrical systems, so I had to make this one
conform. Eventually FlightGear will support more complex
systems. Until then, the whole system runs on batteries.
-->
<PropertyList>
<supplier>
<name>Battery</name>
<prop>/systems/electrical/suppliers/battery[0]</prop>
<kind>battery</kind>
<volts>28</volts>
<amps>60</amps>
</supplier>
<supplier>
<name>Static Inverter</name>
<prop>/systems/electrical/suppliers/static-inverter</prop>
<kind>alternator</kind>
<volts>28</volts>
<amps>60</amps>
</supplier>
<supplier>
<name>Gen 1</name>
<prop>/systems/electrical/suppliers/generator[0]</prop>
<kind>alternator</kind>
<volts>28</volts>
<amps>60</amps>
</supplier>
<supplier>
<name>TR 1</name>
<prop>/systems/electrical/suppliers/TR[0]</prop>
<kind>battery</kind>
<volts>28</volts>
<amps>60</amps>
</supplier>
<supplier>
<name>Gen 2</name>
<prop>/systems/electrical/suppliers/generator[1]</prop>
<kind>alternator</kind>
<volts>28</volts>
<amps>60</amps>
</supplier>
<supplier>
<name>TR 2</name>
<prop>/systems/electrical/suppliers/TR[1]</prop>
<kind>battery</kind>
<volts>28</volts>
<amps>60</amps>
</supplier>
<supplier>
<name>External Power</name>
<prop>/systems/electrical/suppliers/external[0]</prop>
<kind>external</kind>
<volts>0</volts>
<amps>0</amps>
</supplier>
<bus>
<name>Hot Battery Bus</name>
<prop>/systems/electrical/outputs/hot-battery-bus</prop>
<prop>/systems/electrical/outputs/fire-detection-dc</prop>
</bus>
<bus>
<name>Battery Bus</name>
<prop>/systems/electrical/outputs/battery-bus</prop>
<prop>/systems/electrical/outputs/fire-protection-dc</prop>
<prop>/systems/electrical/outputs/cockpit-floodlight-dc</prop>
</bus>
<bus>
<name>Main Bus 1</name>
<prop>/systems/electrical/outputs/gen-bus[0]</prop>
</bus>
<bus>
<name>DC Bus 1</name>
<prop>/systems/electrical/outputs/dc-bus[0]</prop>
</bus>
<bus>
<name>Main Bus 2</name>
<prop>/systems/electrical/outputs/gen-bus[1]</prop>
</bus>
<bus>
<name>DC Bus 2</name>
<prop>/systems/electrical/outputs/dc-bus[1]</prop>
</bus>
<bus>
<name>Standby AC Bus</name>
<prop>/systems/electrical/outputs/standby-bus-ac</prop>
<prop>/systems/electrical/outputs/pressurization-control-ac</prop>
<prop>/systems/electrical/outputs/nav[0]</prop>
<prop>/systems/electrical/outputs/hsi</prop>
<prop>/systems/electrical/outputs/dme[0]</prop>
<prop>/systems/electrical/outputs/audio-panel[0]</prop>
</bus>
<bus>
<name>Standby DC Bus</name>
<prop>/systems/electrical/outputs/standby-bus-dc</prop>
<prop>/systems/electrical/outputs/pressurization-control-dc</prop>
</bus>
<bus>
<name>Avionics Bus 1</name>
<prop>/systems/electrical/outputs/bus-avionics[0]</prop>
<prop>/systems/electrical/outputs/avionics-cooling</prop>
</bus>
<bus>
<name>Avionics Bus 2</name>
<prop>/systems/electrical/outputs/bus-avionics[1]</prop>
<prop>/systems/electrical/outputs/nav[1]</prop>
<prop>/systems/electrical/outputs/transponder</prop>
<prop>/systems/electrical/outputs/autopilot</prop>
</bus>
<bus>
<name>External Bus</name>
<prop>/systems/electrical/outputs/external-bus</prop>
</bus>
<connector>
<input>External Power</input>
<output>External Bus</output>
</connector>
<!--
<connector>
<input>External Bus</input>
<output>Main Bus 1</output>
<output>Main Bus 2</output>
</connector>
-->
<!-- the following two are a hack to get power to the main buses -->
<connector>
<input>Battery</input>
<output>Main Bus 1</output>
</connector>
<connector>
<input>Battery</input>
<output>Main Bus 2</output>
</connector>
<!-- doesn't work yet - generators not powered
<connector>
<input>Gen 1</input>
<output>Main Bus 1</output>
</connector>
<connector>
<input>Gen 2</input>
<output>Main Bus 2</output>
</connector>
<connector>
<input>Main Bus 1</input>
<output>TR 1</output>
<output>Avionics Bus 1</output>
</connector>
<connector>
<input>Main Bus 2</input>
<output>TR 2</output>
<output>Avionics Bus 2</output>
</connector>
-->
<connector>
<input>TR 1</input>
<output>DC Bus 1</output>
<output>DC Bus 2</output>
<output>Avionics Bus 1</output> <!-- a hack -->
</connector>
<connector>
<input>TR 2</input>
<output>DC Bus 2</output>
<output>DC Bus 1</output>
<output>Avionics Bus 2</output> <!-- a hack -->
</connector>
<connector>
<input>DC Bus 1</input>
<output>Battery Bus</output>
</connector>
<connector>
<input>Battery</input>
<output>Battery Bus</output>
<switch>/controls/switches/battery</switch>
</connector>
<connector>
<input>Battery</input>
<output>Hot Battery Bus</output>
</connector>
<connector>
<input>Battery Bus</input>
<output>Static Inverter</output>
<output>Standby DC Bus</output>
</connector>
<connector>
<input>Battery</input> <!-- a hack -->
<output>Standby AC Bus</output>
</connector>
<output>
<name>Start Switch 1</name>
<prop>/systems/electrical/outputs/starter[0]</prop>
</output>
<output>
<name>Start Switch 2</name>
<prop>/systems/electrical/outputs/starter[1]</prop>
</output>
<output>
<name>Cockpit Lights</name>
<prop>/systems/electrical/outputs/cabin-lights</prop>
</output>
<output>
<name>Fuel Boost Pump 1</name>
<prop>/systems/electrical/outputs/fuel-boost-pump[0]</prop>
</output>
<output>
<name>Fuel Boost Pump 2</name>
<prop>/systems/electrical/outputs/fuel-boost-pump[1]</prop>
</output>
<output>
<name>Landing Light</name>
<prop>/systems/electrical/outputs/landing-light</prop>
</output>
<output>
<name>Beacon</name>
<prop>/systems/electrical/outputs/beacon</prop>
</output>
<output>
<name>Map Light</name>
<prop>/systems/electrical/outputs/map-lights</prop>
</output>
<output>
<name>Instrument Lights</name>
<prop>/systems/electrical/outputs/instrument-lights</prop>
</output>
<output>
<name>Strobe Light</name>
<prop>/systems/electrical/outputs/strobe-lights</prop>
</output>
<output>
<name>Taxi Light</name>
<prop>/systems/electrical/outputs/taxi-lights</prop>
</output>
<output>
<name>Pitot Heat</name>
<prop>/systems/electrical/outputs/pitot-heat</prop>
</output>
<connector>
<input>Battery Bus</input>
<output>Start Switch 1</output>
<switch>/controls/starter[0]</switch>
</connector>
<connector>
<input>Battery Bus</input>
<output>Start Switch 2</output>
<switch>/controls/starter[1]</switch>
</connector>
<connector>
<input>Main Bus 2</input>
<output>Cockpit Lights</output>
<switch>/controls/circuit-breakers/cabin-lights-pwr</switch>
</connector>
<connector>
<input>Main Bus 1</input>
<output>Fuel Boost Pump 1</output>
<switch>/controls/boost-pump[0]</switch>
</connector>
<connector>
<input>Main Bus 2</input>
<output>Fuel Boost Pump 2</output>
<switch>/controls/boost-pump[1]</switch>
</connector>
<connector>
<input>Main Bus 1</input>
<output>Landing Light</output>
<switch>/controls/switches/landing-light</switch>
</connector>
<connector>
<input>Main Bus 1</input>
<output>Beacon</output>
<switch>/controls/switches/flashing-beacon</switch>
</connector>
<connector>
<input>DC Bus 2</input>
<output>Map Light</output>
<switch>/controls/switches/nav-lights</switch>
</connector>
<connector>
<input>DC Bus 1</input>
<output>Instrument Lights</output>
<switch>/controls/circuit-breakers/instrument-lights</switch>
</connector>
<connector>
<input>Main Bus 2</input>
<output>Strobe Light</output>
<switch>/controls/switches/strobe-lights</switch>
</connector>
<connector>
<input>Main Bus 2</input>
<output>Taxi Light</output>
<switch>/controls/switches/taxi-lights</switch>
</connector>
<connector>
<input>Main Bus 1</input>
<output>Pitot Heat</output>
<switch>/controls/switches/pitot-heat</switch>
</connector>
-->
</PropertyList>
--- NEW FILE ---
<?xml version="1.0"?>
<!--
************************************************************************
F-80C config file
David Culp, davidculp2@comcast.net
released under GPL
************************************************************************
-->
<PropertyList>
<sim>
<description>Lockheed F-80C Shooting Star</description>
<author>David Culp (FDM), Massimo Taccoli, David Culp(3D)</author>
<flight-model>jsb</flight-model>
<aero>F80C</aero>
<sound>
<path>Aircraft/F80C/Sounds/F80C-sound.xml</path>
</sound>
<submodels>
<serviceable type="bool">true</serviceable>
<path>Aircraft/F80C/submodels.xml</path>
</submodels>
<virtual-cockpit archive="y">true</virtual-cockpit>
<allow-toggle-cockpit archive="y">false</allow-toggle-cockpit>
<panel>
<visibility archive="y">false</visibility>
</panel>
<view n="0">
<internal archive="y">true</internal>
<config>
<pitch-offset-deg>-4.5</pitch-offset-deg>
<x-offset-m archive="y">0.0</x-offset-m><!-- right/left -->
<y-offset-m archive="y">0.97</y-offset-m><!-- up/down -->
<z-offset-m archive="y">-0.80</z-offset-m><!-- aft/fore -->
</config>
</view>
<model>
<path>Aircraft/F80C/Models/f80.xml</path>
</model>
<chase-distance-m>-18</chase-distance-m>
<flaps>
<setting>0.000</setting>
<setting>0.500</setting>
<setting>1.000</setting>
</flaps>
<help>
<key>
<name>Shift-Q</name>
<desc>fuel cutoff switch or lever</desc>
</key>
<line> </line>
<line>Takeoff: half flaps, rotate at 120 kts.</line>
<line>Landing: full flaps, land at 120 kts.</line>
<line> </line>
<line>Clickable panel. Hit Ctrl-C to see hot spots.</line>
<text>
Original model by Massimo Taccoli, used with permission. Adapted from the original \
MDL format to AC3D format, and 3D cockpit by David Culp. Aerodynamics configuration \
for the JSBSim flight dynamics model is slightly modified from the AeroMatic output. \
Released under the GPL, December 2005. davidculp2@comcast.net
The Lockheed P-80 was designed in 1943, the first project of the famous "Skunk \
Works", lead by Clarence "Kelly" Johnson. The engine was a copy of Sir Frank \
Whittle's design, later license built by Allison as the J-33. The first XP-80 flew in \
early 1944, but saw no combat in WWII. The airplane was re-designated the F-80 in \
1948 when the new USAF was established. Although the F-80 was 100 knots faster than \
the piston-engined fighters of its time, it was no match for the swept wing fighters \
like the MiG-15 and F-86 which first flew in 1947. Because of this it was relegated \
to ground attack duties during the Korean War and suffered heavy losses from ground \
fire. The trainer version, the T-33, was very successful, and several still fly in \
private hands. </text>
</help>
</sim>
<controls>
<flight>
<flaps>0.5</flaps>
</flight>
<lighting>
<instruments-norm>0.3</instruments-norm>
</lighting>
<armament>
<gunsight>
<power-on type="bool">false</power-on>
<intensity type="double">0.3</intensity>
</gunsight>
</armament>
</controls>
<engines>
<engine n="0">
<running>true</running>
</engine>
</engines>
<input>
<keyboard>
<key n="81">
<name>Shift-Q</name>
<desc>Fuel Cutoff Switch or Lever.</desc>
<binding>
<condition>
<property>/sim/input/selected/engine[0]</property>
</condition>
<command>property-toggle</command>
<property>/controls/engines/engine[0]/cutoff</property>
</binding>
</key>
</keyboard>
</input>
</PropertyList>
--- NEW FILE ---
<FDM_CONFIG NAME="P80C" VERSION="1.65" RELEASE="ALPHA">
<!--
File: P80C.xml
Author: Aero-Matic v 0.71
Inputs:
name: P80C
type: single-engine transonic/supersonic fighter
max weight: 16800.0 lb
wing span: 38.8 ft
length: 34.5 ft
wing area: unspecified
gear type: tricycle
retractable?: yes
# engines: 1
engine type: turbine
engine layout: aft fuselage
yaw damper? yes
Outputs:
wing loading: 95.00 lb/sq-ft
CL-alpha: 3.5 per radian
CL-0: 0.08
CL-max: 1
CD-0: 0.021
K: 0.09
-->
<METRICS>
AC_WINGAREA 237.0
AC_WINGSPAN 38.80
AC_WINGINCIDENCE 2.0
AC_CHORD 4.56
AC_HTAILAREA 35.37
AC_HTAILARM 13.80
AC_VTAILAREA 21.22
AC_LV 13.80
AC_IXX 21472
AC_IYY 28527
AC_IZZ 42049
AC_IXZ 0
AC_EMPTYWT 8240
AC_CGLOC 248.4 0.0 0.0
AC_AERORP 250.0 0.0 0.0
AC_EYEPTLOC 82.8 0.0 36.0
AC_VRP 0 0 0
</METRICS>
<UNDERCARRIAGE>
AC_GEAR NOSE_LG 53.8 0.0 -72.0 5040.0 1680.0 0.5 0.8 0.02 STEERABLE NONE 5.0 \
RETRACT AC_GEAR LEFT_MLG 265.3 -41.9 -66.0 16800.0 3360.0 0.5 0.8 0.02 FIXED LEFT \
0 RETRACT AC_GEAR RIGHT_MLG 265.3 41.9 -66.0 16800.0 3360.0 0.5 0.8 0.02 FIXED RIGHT \
0 RETRACT <!-- following are ground contact points -->
AC_GEAR LEFT_WT -250 -232 0 50000 20000 0.2 0.2 0.2 FIXED NONE 0 FIXED
AC_GEAR RIGHT_WT -250 232 0 50000 20000 0.2 0.2 0.2 FIXED NONE 0 FIXED
AC_GEAR TAILPIPE -410 0 -2 50000 20000 0.2 0.2 0.2 FIXED NONE 0 FIXED
AC_GEAR NOSE 0 0 -1 50000 20000 0.2 0.2 0.2 FIXED NONE 0 FIXED
</UNDERCARRIAGE>
<PROPULSION>
<AC_ENGINE FILE="J33-A-35">
XLOC 354
YLOC 0
ZLOC 0
PITCH 0
YAW 0
FEED 0
<AC_THRUSTER FILE="direct">
XLOC 354
YLOC 0
ZLOC 0
PITCH 0.03
YAW 0
</AC_THRUSTER>
</AC_ENGINE>
<AC_TANK TYPE="FUEL" NUMBER="0">
XLOC 248.4
YLOC 0
ZLOC -10.35
RADIUS 1
CAPACITY 2848.0
CONTENTS 2800.0
</AC_TANK>
</PROPULSION>
<FLIGHT_CONTROL NAME="P80C">
<COMPONENT NAME="Pitch Trim Sum" TYPE="SUMMER">
INPUT fcs/elevator-cmd-norm
INPUT fcs/pitch-trim-cmd-norm
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Elevator Control" TYPE="AEROSURFACE_SCALE">
INPUT fcs/pitch-trim-sum
MIN -0.350
MAX 0.300
OUTPUT fcs/elevator-pos-rad
</COMPONENT>
<COMPONENT NAME="Roll Trim Sum" TYPE="SUMMER">
INPUT fcs/aileron-cmd-norm
INPUT fcs/roll-trim-cmd-norm
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Left Aileron Control" TYPE="AEROSURFACE_SCALE">
INPUT fcs/roll-trim-sum
MIN -0.35
MAX 0.35
OUTPUT fcs/left-aileron-pos-rad
</COMPONENT>
<COMPONENT NAME="Right Aileron Control" TYPE="AEROSURFACE_SCALE">
INPUT -fcs/roll-trim-sum
MIN -0.35
MAX 0.35
OUTPUT fcs/right-aileron-pos-rad
</COMPONENT>
<COMPONENT NAME="Rudder Command Sum" TYPE="SUMMER">
INPUT fcs/rudder-cmd-norm
INPUT fcs/yaw-trim-cmd-norm
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Yaw Damper Rate" TYPE="SCHEDULED_GAIN">
INPUT velocities/r-aero-rad_sec
SCHEDULED_BY aero/qbar-psf
ROWS 2
3.00 0.00
11.00 2.00
</COMPONENT>
<COMPONENT NAME="Yaw Damper Beta" TYPE="SCHEDULED_GAIN">
INPUT aero/beta-rad
SCHEDULED_BY aero/qbar-psf
ROWS 2
3.00 0.00
11.00 0.00
</COMPONENT>
<COMPONENT NAME="Yaw Damper Sum" TYPE="SUMMER">
INPUT fcs/yaw-damper-beta
INPUT fcs/yaw-damper-rate
CLIPTO -0.2 0.2
</COMPONENT>
<COMPONENT NAME="Yaw Damper Final" TYPE="SCHEDULED_GAIN">
INPUT fcs/yaw-damper-sum
SCHEDULED_BY aero/qbar-psf
ROWS 2
2.99 0.0
3.00 1.0
</COMPONENT>
<COMPONENT NAME="Rudder Sum" TYPE="SUMMER">
INPUT fcs/rudder-command-sum
INPUT fcs/yaw-damper-final
CLIPTO -1 1
</COMPONENT>
<COMPONENT NAME="Rudder Control" TYPE="AEROSURFACE_SCALE">
INPUT fcs/rudder-sum
MIN -0.35
MAX 0.35
OUTPUT fcs/rudder-pos-rad
</COMPONENT>
<COMPONENT NAME="Flaps Control" TYPE="KINEMAT">
INPUT fcs/flap-cmd-norm
DETENTS 3
0 0
15 4
30 3
OUTPUT fcs/flap-pos-deg
</COMPONENT>
<COMPONENT NAME="Gear Control" TYPE="KINEMAT">
INPUT gear/gear-cmd-norm
DETENTS 2
0 0
1 5
OUTPUT gear/gear-pos-norm
</COMPONENT>
<COMPONENT NAME="Speedbrake Control" TYPE="KINEMAT">
INPUT fcs/speedbrake-cmd-norm
DETENTS 2
0 0
1 1
OUTPUT fcs/speedbrake-pos-norm
</COMPONENT>
</FLIGHT_CONTROL>
<AERODYNAMICS>
<AXIS NAME="LIFT">
<COEFFICIENT NAME="CLalpha" TYPE="TABLE">
Lift_due_to_alpha
5
2
aero/alpha-rad
fcs/components/flaps-control/output-norm
aero/qbar-psf|metrics/Sw-sqft
0 1
-0.20 -0.620 -0.4975
0.00 0.080 0.2025
0.225 0.8775 1.000
0.26 1.000 0.8971
0.60 0.448 0.3451
</COEFFICIENT>
<COEFFICIENT NAME="dCLflap" TYPE="VALUE">
Delta_Lift_due_to_flaps
aero/qbar-psf|metrics/Sw-sqft|fcs/components/flaps-control/output-norm
0.29
</COEFFICIENT>
<COEFFICIENT NAME="CLde" TYPE="VALUE">
Lift_due_to_Elevator_Deflection
aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-rad
0.2
</COEFFICIENT>
</AXIS>
<AXIS NAME="DRAG">
<COEFFICIENT NAME="CD0" TYPE="VECTOR">
Drag_at_zero_lift
5
aero/alpha-rad
aero/qbar-psf|metrics/Sw-sqft
-1.57 1.500
-0.26 0.042
0.00 0.021
0.26 0.042
1.57 1.500
</COEFFICIENT>
<COEFFICIENT NAME="CDi" TYPE="VALUE">
Induced_drag
aero/qbar-psf|metrics/Sw-sqft|aero/cl-squared-norm
0.09
</COEFFICIENT>
<COEFFICIENT NAME="CDmach" TYPE="VECTOR">
Drag_due_to_mach
4
velocities/mach-norm
aero/qbar-psf|metrics/Sw-sqft
0.0 0.000
0.77 0.000
1.1 0.023
1.8 0.015
</COEFFICIENT>
<COEFFICIENT NAME="CDflap" TYPE="VALUE">
Drag_due_to_flaps
aero/qbar-psf|metrics/Sw-sqft|fcs/components/flaps-control/output-norm
0.08
</COEFFICIENT>
<COEFFICIENT NAME="CDgear" TYPE="VALUE">
Drag_due_to_gear
aero/qbar-psf|metrics/Sw-sqft|gear/gear-pos-norm
0.02
</COEFFICIENT>
<COEFFICIENT NAME="CDsb" TYPE="VALUE">
Drag_due_to_speedbrakes
aero/qbar-psf|metrics/Sw-sqft|fcs/speedbrake-pos-norm
0.022
</COEFFICIENT>
<COEFFICIENT NAME="CDbeta" TYPE="VECTOR">
Drag_due_to_sideslip
5
aero/beta-rad
aero/qbar-psf|metrics/Sw-sqft
-1.57 1.230
-0.26 0.050
0.00 0.00
0.26 0.050
1.57 1.230
</COEFFICIENT>
<COEFFICIENT NAME="CDde" TYPE="VALUE">
Drag_due_to_Elevator_Deflection
aero/qbar-psf|metrics/Sw-sqft|fcs/elevator-pos-norm
0.08
</COEFFICIENT>
</AXIS>
<AXIS NAME="SIDE">
<COEFFICIENT NAME="CYb" TYPE="VALUE">
Side_force_due_to_beta
aero/qbar-psf|metrics/Sw-sqft|aero/beta-rad
-1
</COEFFICIENT>
</AXIS>
<AXIS NAME="ROLL">
<COEFFICIENT NAME="Clb" TYPE="VALUE">
Roll_moment_due_to_beta
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
-0.1
</COEFFICIENT>
<COEFFICIENT NAME="Clp" TYPE="VALUE">
Roll_moment_due_to_roll_rate
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/p-aero-rad_sec
-0.4
</COEFFICIENT>
<COEFFICIENT NAME="Clr" TYPE="VALUE">
Roll_moment_due_to_yaw_rate
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
0.15
</COEFFICIENT>
<COEFFICIENT NAME="Clda" TYPE="VECTOR">
Roll_moment_due_to_aileron
2
velocities/mach-norm
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
0.0 0.11
2.0 0.037
</COEFFICIENT>
<COEFFICIENT NAME="Cldr" TYPE="VALUE">
Roll_moment_due_to_rudder
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
0.01
</COEFFICIENT>
</AXIS>
<AXIS NAME="PITCH">
<COEFFICIENT NAME="Cmalpha" TYPE="VALUE">
Pitch_moment_due_to_alpha
aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/alpha-rad
-0.3
</COEFFICIENT>
<COEFFICIENT NAME="Cmde" TYPE="VECTOR">
Pitch_moment_due_to_elevator
2
velocities/mach-norm
aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|fcs/elevator-pos-rad
0.0 -0.5
2.0 -0.200
</COEFFICIENT>
<COEFFICIENT NAME="Cmq" TYPE="VALUE">
Pitch_moment_due_to_pitch_rate
aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|velocities/q-aero-rad_sec
-18
</COEFFICIENT>
<COEFFICIENT NAME="Cmadot" TYPE="VALUE">
Pitch_moment_due_to_alpha_rate
aero/qbar-psf|metrics/Sw-sqft|metrics/cbarw-ft|aero/ci2vel|aero/alphadot-rad_sec
-9
</COEFFICIENT>
</AXIS>
<AXIS NAME="YAW">
<COEFFICIENT NAME="Cnb" TYPE="VALUE">
Yaw_moment_due_to_beta
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/beta-rad
0.12
</COEFFICIENT>
<COEFFICIENT NAME="Cnr" TYPE="VALUE">
Yaw_moment_due_to_yaw_rate
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|aero/bi2vel|velocities/r-aero-rad_sec
-0.15
</COEFFICIENT>
<COEFFICIENT NAME="Cndr" TYPE="VALUE">
Yaw_moment_due_to_rudder
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/rudder-pos-rad
-0.1
</COEFFICIENT>
<COEFFICIENT NAME="Cnda" TYPE="VALUE">
Adverse_yaw
aero/qbar-psf|metrics/Sw-sqft|metrics/bw-ft|fcs/left-aileron-pos-rad
0
</COEFFICIENT>
</AXIS>
</AERODYNAMICS>
</FDM_CONFIG>
--- NEW FILE ---
<?xml version="1.0"?>
<PropertyList>
<!-- Each submodel here represents one 0.50in Browning machine gun
firing tracers. I don't have ballistics information for tracers,
so I'm using data for the standard M2 bullet.
-->
<submodel>
<name>left-guns</name>
<model>Models/Geometry/tracer.ac</model>
<trigger>controls/armament/trigger</trigger>
<speed>2840.0</speed>
<repeat>true</repeat>
<delay>0.15</delay>
<count>-1</count>
<x-offset>10.0</x-offset>
<y-offset>-1.0</y-offset>
<z-offset>-2.0</z-offset>
<yaw-offset>0.0</yaw-offset>
<pitch-offset>-1</pitch-offset>
<life>2.0</life>
<wind>false</wind>
<weight>0.1069</weight>
<cd>0.193</cd>
<eda>0.00136354</eda>
</submodel>
<submodel>
<name>right-guns</name>
<model>Models/Geometry/tracer.ac</model>
<trigger>controls/armament/trigger</trigger>
<speed>2840.0</speed>
<repeat>true</repeat>
<delay>0.15</delay>
<count>-1</count>
<x-offset>10.0</x-offset>
<y-offset>1.0</y-offset>
<z-offset>-1.0</z-offset>
<yaw-offset>0.0</yaw-offset>
<pitch-offset>-1</pitch-offset>
<life>2.0</life>
<wind>false</wind>
<weight>0.1069</weight>
<cd>0.193</cd>
<eda>0.00136354</eda>
</submodel>
</PropertyList>
--- NEW FILE ---
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