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[paparazzi-commits] [4713] add Corsica plane jsbsim model (unfinished)
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From: |
Gautier Hattenberger |
|
Subject: |
[paparazzi-commits] [4713] add Corsica plane jsbsim model (unfinished) |
|
Date: |
Tue, 23 Mar 2010 15:52:37 +0000 |
Revision: 4713
http://svn.sv.gnu.org/viewvc/?view=rev&root=paparazzi&revision=4713
Author: gautier
Date: 2010-03-23 15:52:37 +0000 (Tue, 23 Mar 2010)
Log Message:
-----------
add Corsica plane jsbsim model (unfinished)
Added Paths:
-----------
paparazzi3/trunk/conf/simulator/Corsica/
paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml
paparazzi3/trunk/conf/simulator/Corsica/Engines/
paparazzi3/trunk/conf/simulator/Corsica/Engines/18x8.xml
paparazzi3/trunk/conf/simulator/Corsica/Engines/Axi.xml
Added: paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml
===================================================================
--- paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml
(rev 0)
+++ paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml 2010-03-23
15:52:37 UTC (rev 4713)
@@ -0,0 +1,441 @@
+<?xml version="1.0"?>
+<?xml-stylesheet href="http://jsbsim.sourceforge.net/JSBSim.xsl";
type="text/xsl"?>
+<fdm_config name="rascal" version="2.0" release="BETA"
+ xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance";
+ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd";>
+
+ <fileheader>
+ <author> Murat Bronz </author>
+ <filecreationdate> 18/03/2010 </filecreationdate>
+ <version> Version </version>
+ <description> Corsica10 Prototype </description>
+ </fileheader>
+
+ <metrics>
+ <wingarea unit="M2"> 0.21 </wingarea>
+ <wingspan unit="M"> 1.5 </wingspan>
+ <chord unit="M"> 0.14 </chord>
+ <htailarea unit="M2"> 0.026 </htailarea>
+ <htailarm unit="M"> 0.6 </htailarm>
+ <vtailarea unit="M2"> 0.011 </vtailarea>
+ <vtailarm unit="M"> 0.6 </vtailarm>
+ <location name="AERORP" unit="IN">
+ <x> 0 </x>
+ <y> 0 </y>
+ <z> 0 </z>
+ </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 0 </x>
+ <y> 0 </y>
+ <z> 0 </z>
+ </location>
+ <location name="VRP" unit="IN">
+ <x> 0 </x>
+ <y> 0 </y>
+ <z> 0 </z>
+ </location>
+ </metrics>
+
+ <mass_balance>
+ <ixx unit="KG*M2"> 0.125 </ixx>
+ <iyy unit="KG*M2"> 0.032 </iyy>
+ <izz unit="KG*M2"> 0.156 </izz>
+ <ixy unit="KG*M2"> 0 </ixy>
+ <ixz unit="KG*M2"> -0.003 </ixz>
+ <iyz unit="KG*M2"> 0 </iyz>
+ <emptywt unit="KG"> 2.0 </emptywt>
+ <location name="CG" unit="M">
+ <x> 0.067 </x>
+ <y> 0 </y>
+ <z> 0 </z>
+ </location>
+ </mass_balance>
+
+
+
+<!--Ground reactions deleted -->
+
+ <propulsion>
+ <engine file="Axi">
+ <location unit="M">
+ <x> -0.02 </x>
+ <y> 0 </y>
+ <z> 0 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 0 </pitch>
+ <yaw> 0 </yaw>
+ </orient>
+ <feed>0</feed>
+ <thruster file="18x8">
+ <location unit="M">
+ <x> -0.02 </x>
+ <y> 0 </y>
+ <z> 0 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 0.0 </pitch>
+ <yaw> 0.0 </yaw>
+ </orient>
+ <p_factor>1.0</p_factor>
+ </thruster>
+ </engine>
+ </propulsion>
+
+ <flight_control name="Corsica">
+ <channel name="All">
+
+ <summer name="Pitch Trim Sum">
+ <input>fcs/elevator-cmd-norm</input>
+ <input>fcs/pitch-trim-cmd-norm</input>
+ <clipto>
+ <min>-1</min>
+ <max>1</max>
+ </clipto>
+ </summer>
+
+ <aerosurface_scale name="Elevator Control">
+ <input>fcs/pitch-trim-sum</input>
+ <range>
+ <min>-0.5</min>
+ <max>0.5</max>
+ </range>
+ <output>fcs/elevator-pos-rad</output>
+ </aerosurface_scale>
+
+ <aerosurface_scale name="Elevator Normalized">
+ <input>fcs/elevator-pos-rad</input>
+ <domain>
+ <min>-0.5</min>
+ <max> 0.5</max>
+ </domain>
+ <range>
+ <min>-1</min>
+ <max> 1</max>
+ </range>
+ <output>fcs/elevator-pos-norm</output>
+ </aerosurface_scale>
+
+ <summer name="Roll Trim Sum">
+ <input>fcs/aileron-cmd-norm</input>
+ <input>fcs/roll-trim-cmd-norm</input>
+ <clipto>
+ <min>-1</min>
+ <max>1</max>
+ </clipto>
+ </summer>
+
+ <aerosurface_scale name="Left Aileron Control">
+ <input>fcs/roll-trim-sum</input>
+ <range>
+ <min>-0.5</min>
+ <max>0.5</max>
+ </range>
+ <output>fcs/left-aileron-pos-rad</output>
+ </aerosurface_scale>
+
+ <aerosurface_scale name="Right Aileron Control">
+ <input>-fcs/roll-trim-sum</input>
+ <range>
+ <min>-0.5</min>
+ <max>0.5</max>
+ </range>
+ <output>fcs/right-aileron-pos-rad</output>
+ </aerosurface_scale>
+
+ <aerosurface_scale name="Left aileron Normalized">
+ <input>fcs/left-aileron-pos-rad</input>
+ <domain>
+ <min>-0.5</min>
+ <max> 0.5</max>
+ </domain>
+ <range>
+ <min>-1</min>
+ <max> 1</max>
+ </range>
+ <output>fcs/left-aileron-pos-norm</output>
+ </aerosurface_scale>
+
+ <aerosurface_scale name="Right aileron Normalized">
+ <input>fcs/right-aileron-pos-rad</input>
+ <domain>
+ <min>-0.5</min>
+ <max> 0.5</max>
+ </domain>
+ <range>
+ <min>-1</min>
+ <max> 1</max>
+ </range>
+ <output>fcs/right-aileron-pos-norm</output>
+ </aerosurface_scale>
+
+ </channel>
+ </flight_control>
+
+
+ <aerodynamics>
+
+ <axis name="DRAG">
+ <function name="aero/coefficient/CD0">
+ <description>Drag_at_zero_lift</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <table>
+ <independentVar>aero/alpha-rad</independentVar>
+ <tableData>
+ -1.5700 1.5000
+ -0.2600 0.0560
+ 0.0000 0.0280
+ 0.2600 0.0560
+ 1.5700 1.5000
+ </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">
+ <description>Drag_due_to_sideslip</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <table>
+ <independentVar>aero/beta-rad</independentVar>
+ <tableData>
+ -1.5700 1.2300
+ -0.2600 0.0500
+ 0.0000 0.0000
+ 0.2600 0.0500
+ 1.5700 1.2300
+ </tableData>
+ </table>
+ </product>
+ </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>
+ </product>
+ </function>
+ </axis>
+
+ <axis name="SIDE">
+ <function name="aero/coefficient/CYb">
+ <description>Side_force_due_to_beta</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>aero/beta-rad</property>
+ <value>-1.0000</value>
+ </product>
+ </function>
+ </axis>
+
+ <axis name="LIFT">
+ <function name="aero/coefficient/CLalpha">
+ <description>Lift_due_to_alpha</description>
+ <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>
+ </product>
+ </function>
+ <function name="aero/coefficient/CLde">
+ <description>Lift_due_to_Elevator_Deflection</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>fcs/elevator-pos-rad</property>
+ <value>0.2000</value>
+ </product>
+ </function>
+ </axis>
+
+ <axis name="ROLL">
+ <function name="aero/coefficient/Clb">
+ <description>Roll_moment_due_to_beta</description>
+ <!-- aka dihedral effect -->
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/bw-ft</property>
+ <property>aero/beta-rad</property>
+ <value>-0.1000</value>
+ </product>
+ </function>
+ <function name="aero/coefficient/Clp">
+ <description>Roll_moment_due_to_roll_rate</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/bw-ft</property>
+ <property>aero/bi2vel</property>
+ <property>velocities/p-aero-rad_sec</property>
+ <value>-0.4000</value>
+ </product>
+ </function>
+ <function name="aero/coefficient/Clr">
+ <description>Roll_moment_due_to_yaw_rate</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/bw-ft</property>
+ <property>aero/bi2vel</property>
+ <property>velocities/r-aero-rad_sec</property>
+ <value>0.1500</value>
+ </product>
+ </function>
+ <function name="aero/coefficient/Clda">
+ <description>Roll_moment_due_to_aileron</description>
+ <product>
+ <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>
+ </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">
+ <function name="aero/coefficient/Cmalpha">
+ <description>Pitch_moment_due_to_alpha</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/cbarw-ft</property>
+ <property>aero/alpha-rad</property>
+ <value>-0.5000</value>
+ </product>
+ </function>
+ <function name="aero/coefficient/Cmde">
+ <description>Pitch_moment_due_to_elevator</description>
+ <product>
+ <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>
+ </product>
+ </function>
+ <function name="aero/coefficient/Cmq">
+ <description>Pitch_moment_due_to_pitch_rate</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/cbarw-ft</property>
+ <property>aero/ci2vel</property>
+ <property>velocities/q-aero-rad_sec</property>
+ <value>-12.0000</value>
+ </product>
+ </function>
+ <function name="aero/coefficient/Cmadot">
+ <description>Pitch_moment_due_to_alpha_rate</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/cbarw-ft</property>
+ <property>aero/ci2vel</property>
+ <property>aero/alphadot-rad_sec</property>
+ <value>-7.0000</value>
+ </product>
+ </function>
+ </axis>
+
+ <axis name="YAW">
+ <function name="aero/coefficient/Cnb">
+ <description>Yaw_moment_due_to_beta</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/bw-ft</property>
+ <property>aero/beta-rad</property>
+ <value>0.1200</value>
+ </product>
+ </function>
+ <function name="aero/coefficient/Cnr">
+ <description>Yaw_moment_due_to_yaw_rate</description>
+ <product>
+ <property>aero/qbar-psf</property>
+ <property>metrics/Sw-sqft</property>
+ <property>metrics/bw-ft</property>
+ <property>aero/bi2vel</property>
+ <property>velocities/r-aero-rad_sec</property>
+ <value>-0.1500</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>
+ </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>
Added: paparazzi3/trunk/conf/simulator/Corsica/Engines/18x8.xml
===================================================================
--- paparazzi3/trunk/conf/simulator/Corsica/Engines/18x8.xml
(rev 0)
+++ paparazzi3/trunk/conf/simulator/Corsica/Engines/18x8.xml 2010-03-23
15:52:37 UTC (rev 4713)
@@ -0,0 +1,51 @@
+<?xml version="1.0"?>
+
+<!-- Generated by Aero-Matic v 0.7
+
+ Inputs:
+ horsepower: 3.8
+ pitch: fixed
+ Outputs:
+ linear-blade-inches: 10.331602005498
+-->
+
+<propeller name="Rascal Propeller">
+ <ixx> 0.00085 </ixx>
+ <diameter unit="IN"> 18.0 </diameter>
+ <numblades> 2 </numblades>
+ <minpitch> 30 </minpitch>
+ <maxpitch> 30 </maxpitch>
+
+ <table name="C_THRUST" type="internal">
+ <tableData>
+ 0.0 0.0776
+ 0.1 0.0744
+ 0.2 0.0712
+ 0.3 0.0655
+ 0.4 0.0588
+ 0.5 0.0518
+ 0.6 0.0419
+ 0.7 0.0318
+ 0.8 0.0172
+ 1.0 -0.0058
+ 1.4 -0.0549
+ </tableData>
+ </table>
+
+ <table name="C_POWER" type = "internal">
+ <tableData>
+ 0.0 0.0902
+ 0.1 0.0893
+ 0.2 0.0880
+ 0.3 0.0860
+ 0.4 0.0810
+ 0.5 0.0742
+ 0.6 0.0681
+ 0.7 0.0572
+ 0.8 0.0467
+ 1.0 0.0167
+ 1.4 -0.0803
+ </tableData>
+ </table>
+
+</propeller>
Added: paparazzi3/trunk/conf/simulator/Corsica/Engines/Axi.xml
===================================================================
--- paparazzi3/trunk/conf/simulator/Corsica/Engines/Axi.xml
(rev 0)
+++ paparazzi3/trunk/conf/simulator/Corsica/Engines/Axi.xml 2010-03-23
15:52:37 UTC (rev 4713)
@@ -0,0 +1,6 @@
+<?xml version="1.0"?>
+<!-- AXI motor for Corsica plane -->
+
+<electric_engine name="electric">
+ <power unit="WATTS"> 200 </power>
+</electric_engine>
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Gautier Hattenberger <=