CVS: data/Aircraft/C-2A c-2a-base.xml, 1.4, 1.5 c-2a-set.xml, 1.1, 1.2 c-2a-splash.png, 1.3, 1.4 c-2a-yasim-cnf.xml, 1.1, 1.2 c-2a-yasim.xml, 1.4, 1.5
Emmanuel Baranger <[email protected]> Wed, 21 Apr 2010 12:33:23 -0500
| Newsgroups | gmane.games.flightgear.cvc |
|---|---|
| Message-ID | <[email protected]> |
--===============1862616937110333473==
Update of /var/cvs/FlightGear-0.9/data/Aircraft/C-2A
In directory baron.flightgear.org:/tmp/cvs-serv29031
Modified Files:
c-2a-base.xml c-2a-set.xml c-2a-splash.png c-2a-yasim-cnf.xml
c-2a-yasim.xml
Log Message:
- little update on FDM (thanks to Melchior for the YASim_import script)
- Add Nav light and light Cone
- Add shadow
Index: c-2a-base.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/C-2A/c-2a-base.xml,v
retrieving revision 1.4
retrieving revision 1.5
diff -u -r1.4 -r1.5
--- c-2a-base.xml 20 Dec 2008 01:21:51 -0000 1.4
+++ c-2a-base.xml 21 Apr 2010 17:02:17 -0000 1.5
@@ -1,4 +1,4 @@
-<?xml version="1.0"?>
+<?xml version="1.0" encoding="UTF-8"?>
<PropertyList>
Index: c-2a-set.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/C-2A/c-2a-set.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
--- c-2a-set.xml 18 Dec 2008 20:49:41 -0000 1.1
+++ c-2a-set.xml 21 Apr 2010 17:03:42 -0000 1.2
@@ -1,4 +1,4 @@
-<?xml version="1.0"?>
+<?xml version="1.0" encoding="UTF-8"?>
<!-- <PropertyList include="c-2a-jsbsim-cnf.xml"> -->
<PropertyList include="c-2a-yasim-cnf.xml">
Index: c-2a-splash.png
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/C-2A/c-2a-splash.png,v
retrieving revision 1.3
retrieving revision 1.4
diff -u -r1.3 -r1.4
Binary files /tmp/cvsRfDV3g and /tmp/cvsGt3FlR differ
Index: c-2a-yasim-cnf.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/C-2A/c-2a-yasim-cnf.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
--- c-2a-yasim-cnf.xml 18 Dec 2008 20:49:41 -0000 1.1
+++ c-2a-yasim-cnf.xml 21 Apr 2010 17:05:24 -0000 1.2
@@ -1,9 +1,10 @@
-<?xml version="1.0"?>
+<?xml version="1.0" encoding="UTF-8"?>
+
<!--
-************************************************************************
-GRUMMAN C 2A
-December 2008 BARANGER Emmanuel
-************************************************************************
+ ************************************************************************
+ GRUMMAN C 2A
+ December 2008 BARANGER Emmanuel
+ ************************************************************************
-->
<PropertyList include="c-2a-base.xml">
Index: c-2a-yasim.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/C-2A/c-2a-yasim.xml,v
retrieving revision 1.4
retrieving revision 1.5
diff -u -r1.4 -r1.5
--- c-2a-yasim.xml 20 Dec 2008 14:19:56 -0000 1.4
+++ c-2a-yasim.xml 21 Apr 2010 17:05:49 -0000 1.5
@@ -1,3 +1,5 @@
+<?xml version="1.0" encoding="UTF-8"?>
+
<!-- GRUMMAN C 2A : 2008 BARANGER Emmanuel
wingspan : 24.69 m
@@ -33,22 +35,24 @@
<control-setting axis="/controls/gear/gear-down" value="0"/>
</cruise>
- <cockpit x="9.267" y="-0.570" z=".154"/>
+ <cockpit x="6.700" y="-0.570" z="0.154"/>
<!-- Fuselage -->
- <fuselage ax="8.641" ay="0" az="-0.425" bx="-8.651" by="0" bz="0.510" width="3" taper="0.5" midpoint="0.5"/>
+ <fuselage ax="8.641" ay="0" az="-0.850" bx="-3.769" by="0" bz="-0.737" width="2.4" taper="1" midpoint="0"/>
+ <fuselage ax="-3.769" ay="0" az="-0.737" bx="-8.716" by="0" bz="0.510" width="2.4" taper="1" midpoint="0"/>
<!-- Ailes -->
<wing x="0.625" y="0.549" z="0.131"
chord="3.747"
- length="11.565"
+ length="11.8"
taper="0.38"
- sweep="0"
- dihedral="2"
- camber="0.0-">
+ sweep="1.5"
+ dihedral="2.5"
+ camber="0.05">
<stall aoa="18" width="6" peak="1.5"/>
- <flap0 start="0" end=".6" lift="1.4" drag="1.9"/>
- <flap1 start=".6" end=".95" lift="1.4" drag="1.2"/>
+ <flap0 start="0.00" end="0.54" lift="1.4" drag="1.9"/>
+ <flap1 start="0.54" end="0.95" lift="1.4" drag="1.2"/>
+
<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"/>
@@ -64,7 +68,8 @@
<hstab x="-7.220" y="0.0" z="0.866"
chord="2.357"
length="3.923"
- taper="0.75">
+ taper="0.75"
+ sweep="4">
<stall aoa="18" width="4" peak="1.5"/>
<flap0 start="0" end="0.95" lift="1.5" drag="1.4"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
@@ -73,6 +78,20 @@
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
+ <vstab x="-7.110" y="1.919" z="0.890"
+ chord="1.535"
+ length="1.450"
+ taper="0.6"
+ sweep="12">
+ </vstab>
+
+ <vstab x="-7.110" y="-1.919" z="0.890"
+ chord="1.535"
+ length="1.450"
+ taper="0.6"
+ sweep="12">
+ </vstab>
+
<!-- Direction gauche -->
<vstab x="-7.566" y="3.925" z="-0.848"
chord="1.830"
@@ -102,14 +121,11 @@
<!-- Moteur gauche
- Rayon * Rayon * Mass(kg) 2.43*2.43 * 487.15
- moment d'après la doc : ________________________ = __________________ = 958.85
- 3 3
-->
<propeller x="2.743" y="3.169" z="-0.422"
mass="2994"
moment="958.85"
- radius="2.43"
+ radius="1.837"
cruise-speed="245"
cruise-rpm="920"
cruise-power="1800"
@@ -135,7 +151,7 @@
<propeller x="2.743" y="-3.169" z="-0.422"
mass="2994"
moment="958.85"
- radius="2.43"
+ radius="1.837"
cruise-speed="245"
cruise-rpm="920"
cruise-power="1800"
@@ -215,7 +231,7 @@
<control-speed control="LEXTEND" transition-time="1"/>
</launchbar>
- <!-- CG Théorique : x=0.625 y=0.0 z=-0.131" -->
+ <!-- CG Theorique : x=0.625 y=0.0 z=-0.131" -->
<ballast x="5.0" y="0.0" z="0.0" mass="6000"/>
</airplane>
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