CVS: data/Aircraft/21 21-yasim.xml,1.1,1.2
Emmanuel Baranger <[email protected]> Thu, 8 Apr 2010 12:34:17 -0500
| Newsgroups | gmane.games.flightgear.cvc |
|---|---|
| Message-ID | <[email protected]> |
Update of /var/cvs/FlightGear-0.9/data/Aircraft/21
In directory baron.flightgear.org:/tmp/cvs-serv2995
Modified Files:
21-yasim.xml
Log Message:
- little update on FDM (thanks to Melchior for the YASim_import script)
Index: 21-yasim.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/21/21-yasim.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
--- 21-yasim.xml 13 Mar 2009 10:26:25 -0000 1.1
+++ 21-yasim.xml 8 Apr 2010 17:33:41 -0000 1.2
@@ -1,19 +1,22 @@
<?xml version="1.0" encoding="UTF-8"?>
<!-- Santo Dumont N 21 "Demoiselle" 1909 : 2009 Emmanuel BARANGER
+ 2010 EMmanuel BARANGER with melchior script
- Winspan : 5 m ( 16,4 ft)
- Lenght : 8 m ( 26.2 ft)
- Masse : 93 kg (pilote 50 kg) (205.0 lb - 110 lb)
- Engine : 1 x Darrack 30 ch
- Speed : 90 km/h ( 50.0 kt)
+ sources :
+ wingspan : 5 m ( 16,4 ft)
+ length : 8 m ( 26.2 ft)
+ max speed : 90 km/h ( 50.0 kt)
+ empty weight : 93 kg (pilote 50 kg) (205.0 lb - 110 lb)
+ engine : Darrack (30 hp)
-->
+
<airplane mass="500">
<!-- Approach configuration -->
- <approach speed="20" aoa="15">
+ <approach speed="15" aoa="8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
<control-setting axis="/sim/weight[0]/weight-lb" value ="110"/>
@@ -30,69 +33,77 @@
<!-- pilot's eyepoint -->
<cockpit x="2.514" y="0.0" z="-0.221"/>
- <fuselage ax="3.978" ay="0" az="-0.181" bx="-4.0" by="0" bz="-0.181" width="0.728" taper="0.2" midpoint="0.5"/>
+ <fuselage ax="3.659" ay="0" az="-0.181" bx="-2.817" by="0" bz="-0.324" width="0.728" midpoint="0.1" taper="0.2"/>
- <wing x="2.579" y="0" z="0.054"
- chord="1.60"
- length="4.87"
- taper="1.0"
- incidence="2"
- twist="-3"
- sweep="0"
- dihedral="5"
- camber="0.065">
+ <wing x="2.529" y="0" z="0.054"
+ chord="2.260"
+ length="2.516"
+ incidence="4"
+ dihedral="10"
+ camber="0.001"
+ taper="1">
<stall aoa="18" width="4" peak="1.5"/>
- <flap0 start=".31" end="0.85" lift="1.5" drag="1.4"/>
+ <flap0 start="0.45" end="1" lift="1.5" drag="1.4"/>
+
<control-input axis="/controls/flight/aileron" control="FLAP0" 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"/>
</wing>
- <hstab x="-2.887" y="0.0" z="-0.320"
+ <hstab x="-3.45" y="0.0" z="-0.320"
chord="1.13"
- length="1.49"
- taper="0.8"
- effectiveness="1.24"
- sweep="0">
+ length="1.16"
+ taper="1">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
+
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
+
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
- <vstab x="-3.386" y="0" z="-0.855"
- taper="0.38"
- effectiveness="2.0"
- length="1.31"
+ <vstab x="-3.3" y="0" z="-0.855"
chord="1.37"
- sweep="0"
- incidence="1.5">
+ length="1.068"
+ taper="1">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="2.0" 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>
- <propeller x="3.681" y="0.0" z="0.324"
+ <!-- Engines source :
+
+ name : flat-twin Darracq
+ type :
+ power cruise : 30 hp
+ weight :
+ -->
+ <propeller x="3.618" y="0.0" z="0.324"
+ radius="0.927"
mass="150"
moment="4"
- radius="0.90"
- cruise-speed="50"
- cruise-rpm="2150"
+ cruise-speed="50"
cruise-alt="8000"
cruise-power="30"
+ cruise-rpm="2150"
takeoff-power="30"
takeoff-rpm="2300"
- eng-power="30"
- eng-rpm="2500">
+ gear-ratio="0.5">
+ <piston-engine eng-rpm="2500"
+ eng-power="30"
+ displacement="1751"/>
<actionpt x="3.827" y="0.0" z="0.324"/>
- <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
- <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
- <control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
- <control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
+ <control-input control="THROTTLE" axis="/controls/engines/engine[0]/throttle"/>
+ <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"/>
</propeller>
<gear x="3.367" y="0.376" z="-1.193"
@@ -110,14 +121,11 @@
<tank x="2.806" y="0" z="0.318" capacity="56" />
<!-- pilot -->
- <weight x="2.616" y="0" z="-0.421" mass-prop="/sim/weight[0]/weight-lb"/>
-
- <!-- CG Middle of chord : x=2.579 y=0 z=0.054 -->
- <ballast x="2.5" y="0" z="-1" mass="50"/>
+ <weight x="2.426" y="0" z="-0.551" mass-prop="/sim/weight[0]/weight-lb"/>
<!-- hitch -->
<hitch name="aerotow"
- x="-5.0" y="0" z="-0.65"
+ x="-3.0" y="0" z="-0.65"
force-is-calculated-by-other="1">
<tow length="60"
weight-per-meter="0.035"
------------------------------------------------------------------------------
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