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[Flightgear-cvslogs] CVS: data/Aircraft/Pterodactyl COPYING, NONE, 1.1 Read-Me.txt, NONE, 1.1 pterodactyl-base.xml, NONE, 1.1 pterodactyl-set.xml, NONE, 1.1 pterodactyl-splash.png, NONE, 1.1 pterodactyl-yasim-cnf.xml, NONE, 1.1 pterodactyl-yasim.xml, NONE, 1.1 thumbnail.jpg, NONE, 1.1
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From: Emmanuel B. <he...@ba...> - 2010-05-02 17:02:57
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Update of /var/cvs/FlightGear-0.9/data/Aircraft/Pterodactyl In directory baron.flightgear.org:/tmp/cvs-serv25398 Added Files: COPYING Read-Me.txt pterodactyl-base.xml pterodactyl-set.xml pterodactyl-splash.png pterodactyl-yasim-cnf.xml pterodactyl-yasim.xml thumbnail.jpg Log Message: - new plane --- NEW FILE "COPYING" --- GNU GENERAL PUBLIC LICENSE Version 2, June 1991 Copyright (C) 1989, 1991 Free Software Foundation, Inc. 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA Everyone is permitted to copy and distribute verbatim copies of this license document, but changing it is not allowed. Preamble The licenses for most software are designed to take away your freedom to share and change it. By contrast, the GNU General Public License is intended to guarantee your freedom to share and change free software--to make sure the software is free for all its users. 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You should also get your employer (if you work as a programmer) or your school, if any, to sign a "copyright disclaimer" for the program, if necessary. Here is a sample; alter the names: Yoyodyne, Inc., hereby disclaims all copyright interest in the program `Gnomovision' (which makes passes at compilers) written by James Hacker. <signature of Ty Coon>, 1 April 1989 Ty Coon, President of Vice This General Public License does not permit incorporating your program into proprietary programs. If your program is a subroutine library, you may consider it more useful to permit linking proprietary applications with the library. If this is what you want to do, use the GNU Library General Public License instead of this License. --- NEW FILE "Read-Me.txt" --- English/Français [English] ---------- Westland-Hill Pterodactyl MK V ============================== Manufacturer : Type : Year : Powerplant : Wingspan : Length : Height : weight max : Cruise speed : Range : Crew : Some useful keys: ================= Thanks ====== =============== BARANGER Emmanuel May, 01, 2010 http://helijah.free.fr/flightgear/hangar.htm emb...@fr... [Français] ---------- Un peu d'histoire ================= Westland-Hill Pterodactyl MK V ============================== Constructeur : Type : Année : Moteur : Envergure : Longueur : Hauteur : Poids max au décollage : Vitesse estimée de croisière : Autonomie estimée : Equipage : Quelques touches utiles : ========================= Remerciements ============= =============== BARANGER Emmanuel 01 Mai 2010. http://helijah.free.fr/flightgear/hangar.htm emb...@fr... --- NEW FILE "pterodactyl-base.xml" --- <?xml version="1.0" encoding="UTF-8"?> <PropertyList> <sim include="Nasal/views.xml"> <author>BARANGER Emmanuel (3D/FDM)</author> <aircraft-version>0.2</aircraft-version> <status>Alpha</status> <fuel-fraction>1.0</fuel-fraction> <startup> <splash-texture>Aircraft/Pterodactyl/pterodactyl-splash.png</splash-texture> </startup> <sound> <path archive="y">Aircraft/Pterodactyl/Sounds/pterodactyl-sound.xml</path> </sound> <model> <path archive="y">Aircraft/Pterodactyl/Models/pterodactyl.xml</path> <livery> <file type="string">default</file> </livery> </model> <multiplay> <chat_display>1</chat_display> <generic> <int type="int">0</int> <int type="int">0</int> <int type="int">0</int> <int type="int">0</int> <int type="int">0</int> <int type="int">0</int> </generic> </multiplay> <help> <title>Westland Pterodactyl</title> <line>______________________________________________</line> </help> <pterodactyl> <state type="int">0</state> <airspeed-kmh type="float">0.0</airspeed-kmh> <engine-rpm type="float">0.0</engine-rpm> <engine-volume-low-rpm type="float">0.0</engine-volume-low-rpm> <engine-volume-high-rpm type="float">0.0</engine-volume-high-rpm> </pterodactyl> <weight n="0"> <name>Pilot</name> <weight-lb>180</weight-lb> <max-lb>240</max-lb> <min-lb>140</min-lb> </weight> <weight n="1"> <name>Pax</name> <weight-lb>0</weight-lb> <max-lb>240</max-lb> <min-lb>0</min-lb> </weight> <weight n="2"> <name>Baggage</name> <weight-lb>0</weight-lb> <max-lb>20</max-lb> <min-lb>0</min-lb> </weight> <flaps> <setting>0.00</setting> <!-- Cruise --> <setting>0.50</setting> <!-- Half --> <setting>1.0</setting> <!-- Full --> </flaps> <menubar include="Dialogs/pterodactyl-menu.xml"/> </sim> <input> <keyboard include="Nasal/pterodactyl-keyboard.xml"/> </input> <engines> <engine> <rpm type="float">0.0</rpm> </engine> </engines> <nasal> <pterodactyl> <file>Aircraft/Pterodactyl/Nasal/doors.nas</file> <file>Aircraft/Pterodactyl/Nasal/liveries.nas</file> <file>Aircraft/Pterodactyl/Nasal/light.nas</file> </pterodactyl> </nasal> </PropertyList> --- NEW FILE "pterodactyl-set.xml" --- <?xml version="1.0" encoding="UTF-8"?> <!-- <PropertyList include="pterodactyl-jsbsim-cnf.xml"> --> <PropertyList include="pterodactyl-yasim-cnf.xml"> <sim> <description>Westland Pterodactyl</description> <author>Emmanuel BARANGER (3D/FDM)</author> </sim> </PropertyList> --- NEW BINARY FILE "pterodactyl-splash.png" --- --- NEW FILE "pterodactyl-yasim-cnf.xml" --- <?xml version="1.0" encoding="UTF-8"?> <PropertyList include="pterodactyl-base.xml"> <sim> <description>Westland Pterodactyl (YASim)</description> <flight-model archive="y">yasim</flight-model> <aero archive="y">pterodactyl-yasim</aero> </sim> </PropertyList> --- NEW FILE "pterodactyl-yasim.xml" --- <?xml version="1.0" encoding="UTF-8"?> <!-- Westland-Hill Pterodactyl MK V - 2010 Emmanuel BARANGER sources : http://www.aviastar.org/air/england/west_pterodactyl5.php wingspan : 14.22 m ( 47 ft 8 in ) length : 6.24 m ( 20 ft 6 in ) height : 3.55 m ( 12 ft 8 in ) empty weight : 1602 kg ( 3532 lb ) engine : Rolls Royce Goshawk steam-cooled vee-type engine (600 hp) Maximum speed : 305 km/h ( 164.69 kt ) --> <airplane mass="3532"> <!-- Approach configuration --> <approach speed="40" aoa="6" fuel="0.3"> <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/> <control-setting axis="/controls/engines/engine[0]/mixture" value="1"/> <control-setting axis="/controls/flight/flaps" value="1"/> </approach> <!-- Cruise configuration --> <cruise speed="150" alt="6000" fuel="0.5"> <control-setting axis="/controls/engines/engine[0]/throttle" value="0.7"/> <control-setting axis="/controls/engines/engine[0]/mixture" value="0.6"/> <control-setting axis="/controls/flight/flaps" value="0"/> </cruise> <cockpit x="-0.998" y="0" z="0.905"/> <fuselage ax="2.466" ay="0" az="-0.346" bx="-2.651" by="0" bz="-0.214" width="0.95" taper="0.8" midpoint="0.9"/> <mstab x="1.096" y="0" z="1.264" chord="2.080" length="2.40" taper="1.54" sweep="14" camber="0.005"> <stall aoa="16" width="1.5" peak="1.5"/> </mstab> <wing x="0.520" y="2.320" z="1.264" chord="3.2" length="5.8" sweep="34" taper="0.3" camber="0.005"> <stall aoa="16" width="1.5" peak="1.5"/> <flap0 start="0.47" end="1" lift="1.4" drag="1.2"/> <control-input axis="/controls/flight/aileron" control="FLAP0" square="false" split="true"/> <control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/> <control-output control="FLAP0" side="left" prop="/surface-positions/left-aileron-pos-norm"/> <control-output control="FLAP0" side="right" prop="/surface-positions/right-aileron-pos-norm"/> <control-output control="FLAP0" prop="/surface-positions/aileron-pos-norm"/> </wing> <hstab x="0.520" y="2.320" z="1.264" chord="3.2" length="5.8" sweep="34" taper="0.3" camber="0.005"> <stall aoa="16" width="1.5" peak="1.5"/> <flap0 start="0.47" end="1" lift="1.4" drag="1.2"/> <control-input axis="/controls/flight/elevator" square="false" control="FLAP0" /> <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/> <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="FLAP0" prop="/surface-positions/elevator-pos-norm"/> </hstab> <vstab x="-2.560" y="7" z="0.551" chord="0.710" length="1.45" taper="1"> <stall aoa="16" width="5" peak="1.5"/> <flap0 start="0" end="1" lift="1.4" drag="1.2"/> <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" min="1" max="-1"/> </vstab> <vstab x="-2.560" y="-7" z="0.551" chord="0.710" length="1.45" taper="1"> <stall aoa="16" width="5" peak="1.5"/> <flap0 start="0" end="1" lift="1.4" drag="1.2"/> <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" min="1" max="-1"/> </vstab> <mstab x="-0.700" y="0" z="-0.561" chord="1.330" length="3.400" taper="0.5" camber="0.048"> </mstab> <!-- Engines source : http://en.wikipedia.org/wiki/Rolls-Royce_Goshawk name : Rolls-Royce Goshawk type : 12-cylinder liquid-cooled 60 degree Vee aircraft piston engine power cruise : 600 hp at 2,600 rpm weight : 442 kg ( 975 lb) displacement : 1295.88 in3 (21.25 L) compression : 6:1 --> <propeller x="1.784" y="0" z="0.079" radius="1.493" mass="975" moment="2.5" cruise-speed="150" cruise-rpm="2500" cruise-alt="6000" cruise-power="550" takeoff-power="600" takeoff-rpm="2600"> <actionpt x="2.865" y="0" z="0.079"/> <piston-engine eng-rpm="2700" eng-power="600" displacement="1295.88" compression="6"/> <control-input control="THROTTLE" axis="/controls/engines/engine[0]/throttle" src0="0.0" src1="1.0" dst0="0.0" dst1="1.0"/> <control-input control="STARTER" axis="/controls/engines/engine[0]/starter" /> <control-input control="MAGNETOS" axis="/controls/engines/engine[0]/magnetos" /> <control-input control="MIXTURE" axis="/controls/engines/engine[0]/mixture" src0="0.0" src1="1.0" dst0="0.8" dst1="0.8"/> </propeller> <!-- Noze wheel 1 --> <gear x="1.385" y="0" z="-1.995" compression="0.15" spring="0.8" on-solid="1" sfric="1" dfric="1"> <control-input axis="/controls/flight/rudder" control="STEER" square="false"/> </gear> <!-- Noze wheel 2 --> <gear x="0.100" y="0" z="-1.685" compression="0.2" spring="1.8" damp="0.03" on-solid="1"> </gear> <!-- Left wheel --> <gear x="-2.792" y="2.980" z="-1.052" compression="0.2" spring="1.8" damp="0.03" on-solid="1"> </gear> <!-- Right wheel --> <gear x="-2.792" y="-2.980" z="-1.052" compression="0.2" spring="1.8" damp="0.03" on-solid="1"> </gear> <!-- Left wing --> <tank x="0" y="2.32" z="1.28" capacity="50"/> <!-- Right wing --> <tank x="0" y="-2.32" z="1.288" capacity="50"/> <!-- Mass distribution --> <ballast x="-1.2" y="0" z="-2" mass="1500"/> </airplane> --- NEW BINARY FILE "thumbnail.jpg" --- |
