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[paparazzi-commits] [4714] aero value of corsica plane
|
From: |
Gautier Hattenberger |
|
Subject: |
[paparazzi-commits] [4714] aero value of corsica plane |
|
Date: |
Tue, 23 Mar 2010 17:37:52 +0000 |
Revision: 4714
http://svn.sv.gnu.org/viewvc/?view=rev&root=paparazzi&revision=4714
Author: gautier
Date: 2010-03-23 17:37:51 +0000 (Tue, 23 Mar 2010)
Log Message:
-----------
aero value of corsica plane
Modified Paths:
--------------
paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml
Modified: paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml
===================================================================
--- paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml 2010-03-23
15:52:37 UTC (rev 4713)
+++ paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml 2010-03-23
17:37:51 UTC (rev 4714)
@@ -184,50 +184,45 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
- <independentVar>aero/alpha-rad</independentVar>
+ <independentVar>aero/alpha-deg</independentVar>
<tableData>
- -1.5700 1.5000
- -0.2600 0.0560
- 0.0000 0.0280
- 0.2600 0.0560
- 1.5700 1.5000
+ -10.0 0.02748
+ -8.0 0.02243
+ -6.0 0.02335
+ -4.0 0.02770
+ -2.0 0.03369
+ 0.0 0.04284
+ 2.0 0.05454
+ 4.0 0.06868
+ 6.0 0.08515
+ 8.0 0.1055
+ 10.0 0.1595
</tableData>
</table>
</product>
</function>
- <function name="aero/coefficient/CDi">
- <description>Induced_drag</description>
- <product>
- <property>aero/qbar-psf</property>
- <property>metrics/Sw-sqft</property>
- <property>aero/cl-squared</property>
- <value>0.0400</value>
- </product>
- </function>
- <function name="aero/coefficient/CDbeta">
+ <!--function name="aero/coefficient/CDbeta">
<description>Drag_due_to_sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
- <independentVar>aero/beta-rad</independentVar>
+ <independentVar>aero/beta-deg</independentVar>
<tableData>
- -1.5700 1.2300
- -0.2600 0.0500
- 0.0000 0.0000
- 0.2600 0.0500
- 1.5700 1.2300
+ -10.0 -0.00284
+ 0.0 0.0
+ 10.0 -0.00284
</tableData>
</table>
</product>
- </function>
+ </function-->
<function name="aero/coefficient/CDde">
<description>Drag_due_to_Elevator_Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
- <property>fcs/elevator-pos-norm</property>
- <value>0.0300</value>
+ <property>fcs/elevator-pos-deg</property>
+ <value>0.000094</value>
</product>
</function>
</axis>
@@ -239,7 +234,7 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
- <value>-1.0000</value>
+ <value>-0.141391</value>
</product>
</function>
</axis>
@@ -250,15 +245,8 @@
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
- <table>
- <independentVar>aero/alpha-rad</independentVar>
- <tableData>
- -0.2000 -0.7500
- 0.0000 0.2500
- 0.2300 1.4000
- 0.6000 0.7100
- </tableData>
- </table>
+ <property>aero/alpha-rad</property>
+ <value>5.1460</value>
</product>
</function>
<function name="aero/coefficient/CLde">
@@ -266,8 +254,8 @@
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
- <property>fcs/elevator-pos-rad</property>
- <value>0.2000</value>
+ <property>fcs/elevator-pos-deg</property>
+ <value>0.003644</value>
</product>
</function>
</axis>
@@ -281,7 +269,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
- <value>-0.1000</value>
+ <value>-0.04235</value>
</product>
</function>
<function name="aero/coefficient/Clp">
@@ -292,7 +280,7 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
- <value>-0.4000</value>
+ <value>-0.561207</value>
</product>
</function>
<function name="aero/coefficient/Clr">
@@ -303,7 +291,7 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
- <value>0.1500</value>
+ <value>0.17269</value>
</product>
</function>
<function name="aero/coefficient/Clda">
@@ -312,26 +300,10 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
- <property>fcs/left-aileron-pos-rad</property>
- <table>
- <independentVar>velocities/mach</independentVar>
- <tableData>
- 0.0000 0.1300
- 2.0000 0.0570
- </tableData>
- </table>
+ <property>fcs/right-aileron-pos-deg</property>
+ <value>-0.004076</value>
</product>
</function>
- <function name="aero/coefficient/Cldr">
- <description>Roll_moment_due_to_rudder</description>
- <product>
- <property>aero/qbar-psf</property>
- <property>metrics/Sw-sqft</property>
- <property>metrics/bw-ft</property>
- <property>fcs/rudder-pos-rad</property>
- <value>0.0100</value>
- </product>
- </function>
</axis>
<axis name="PITCH">
@@ -342,7 +314,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
- <value>-0.5000</value>
+ <value>-0.523384</value>
</product>
</function>
<function name="aero/coefficient/Cmde">
@@ -351,14 +323,8 @@
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
- <property>fcs/elevator-pos-rad</property>
- <table>
- <independentVar>velocities/mach</independentVar>
- <tableData>
- 0.0000 -0.5000 <!-- was -1.1 -->
- 2.0000 -0.2750
- </tableData>
- </table>
+ <property>fcs/elevator-pos-deg</property>
+ <value>-0.014833</value>
</product>
</function>
<function name="aero/coefficient/Cmq">
@@ -369,7 +335,7 @@
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
- <value>-12.0000</value>
+ <value>-15.281710</value>
</product>
</function>
<function name="aero/coefficient/Cmadot">
@@ -393,7 +359,7 @@
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
- <value>0.1200</value>
+ <value>0.039729</value>
</product>
</function>
<function name="aero/coefficient/Cnr">
@@ -404,38 +370,19 @@
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
- <value>-0.1500</value>
+ <value>-0.048425</value>
</product>
</function>
- <function name="aero/coefficient/Cndr">
- <description>Yaw_moment_due_to_rudder</description>
- <product>
- <property>aero/qbar-psf</property>
- <property>metrics/Sw-sqft</property>
- <property>metrics/bw-ft</property>
- <property>fcs/rudder-pos-rad</property>
- <value>-0.0500</value>
- </product>
- </function>
<function name="aero/coefficient/Cnda">
<description>Adverse_yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
- <property>fcs/left-aileron-pos-rad</property>
- <value>-0.0300</value>
+ <property>fcs/right-aileron-pos-deg</property>
+ <value>0.00026</value>
</product>
</function>
- <function name="aero/coefficient/Cndi">
- <description>Yaw_moment_due_to_tail_incidence</description>
- <product>
- <property>aero/qbar-psf</property>
- <property>metrics/Sw-sqft</property>
- <property>metrics/bw-ft</property>
- <value>0.0007</value>
- </product>
- </function>
</axis>
</aerodynamics>
</fdm_config>
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