From 6acdf25b96be7fd443f3300a4b330be0a32034ab Mon Sep 17 00:00:00 2001
From: Stephen Dwyer <scdwyer@ualberta.ca>
Date: Wed, 7 Aug 2013 16:23:32 -0600
Subject: [PATCH] [conf][nps] Temporary addition of fw jsbsim models

---
 .../jsbsim/aircraft/Engines/18x8.xml          |  51 ++
 .../jsbsim/aircraft/Engines/Zenoah_G-26A.xml  |   8 +
 .../jsbsim/aircraft/LisaAspirin2.xml          | 546 ++++++++++++++++++
 3 files changed, 605 insertions(+)
 create mode 100644 conf/simulator/jsbsim/aircraft/Engines/18x8.xml
 create mode 100644 conf/simulator/jsbsim/aircraft/Engines/Zenoah_G-26A.xml
 create mode 100644 conf/simulator/jsbsim/aircraft/LisaAspirin2.xml

diff --git a/conf/simulator/jsbsim/aircraft/Engines/18x8.xml b/conf/simulator/jsbsim/aircraft/Engines/18x8.xml
new file mode 100644
index 00000000000..3dd84ebec32
--- /dev/null
+++ b/conf/simulator/jsbsim/aircraft/Engines/18x8.xml
@@ -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>
diff --git a/conf/simulator/jsbsim/aircraft/Engines/Zenoah_G-26A.xml b/conf/simulator/jsbsim/aircraft/Engines/Zenoah_G-26A.xml
new file mode 100644
index 00000000000..86d43a827e8
--- /dev/null
+++ b/conf/simulator/jsbsim/aircraft/Engines/Zenoah_G-26A.xml
@@ -0,0 +1,8 @@
+<?xml version="1.0"?>
+<!-- Zenoah G-26A -->
+<!-- 2.96 hp engine -->
+<!-- one horsepower equals 745.69987 Watts -->
+
+<electric_engine name="electric_1mw">
+  <power unit="WATTS">  2207.27 </power>
+</electric_engine>
diff --git a/conf/simulator/jsbsim/aircraft/LisaAspirin2.xml b/conf/simulator/jsbsim/aircraft/LisaAspirin2.xml
new file mode 100644
index 00000000000..b3dafa86fca
--- /dev/null
+++ b/conf/simulator/jsbsim/aircraft/LisaAspirin2.xml
@@ -0,0 +1,546 @@
+<?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> Author Name </author>
+        <filecreationdate> Creation Date </filecreationdate>
+        <version> Version </version>
+        <description> Models a Malolo </description>
+    </fileheader>
+
+    <metrics>
+        <wingarea unit="FT2"> 10.57 </wingarea>
+        <wingspan unit="FT"> 9.17 </wingspan>
+        <chord unit="FT"> 1.15 </chord>
+        <htailarea unit="FT2"> 1.69 </htailarea>
+        <htailarm unit="FT"> 3.28 </htailarm>
+        <vtailarea unit="FT2"> 1.06 </vtailarea>
+        <vtailarm unit="FT"> 0 </vtailarm>
+        <location name="AERORP" unit="IN">
+            <x> 37.4 </x>
+            <y> 0 </y>
+            <z> 0 </z>
+        </location>
+        <location name="EYEPOINT" unit="IN">
+            <x> 20 </x>
+            <y> 0 </y>
+            <z> 5 </z>
+        </location>
+        <location name="VRP" unit="IN">
+            <x> 0 </x>
+            <y> 0 </y>
+            <z> 0 </z>
+        </location>
+    </metrics>
+
+    <mass_balance>
+        <ixx unit="SLUG*FT2"> 1 </ixx>
+        <iyy unit="SLUG*FT2"> 1 </iyy>
+        <izz unit="SLUG*FT2"> 2 </izz>
+        <ixy unit="SLUG*FT2"> 0 </ixy>
+        <ixz unit="SLUG*FT2"> 0 </ixz>
+        <iyz unit="SLUG*FT2"> 0 </iyz>
+        <emptywt unit="LBS"> 12 </emptywt>
+        <location name="CG" unit="IN">
+            <x> 36.4 </x>
+            <y> 0 </y>
+            <z> 4 </z>
+        </location>
+        <pointmass name="payload">
+            <weight unit="LBS"> 1 </weight>
+            <location name="payload" unit="IN">
+                <x> 0 </x>
+                <y> 0 </y>
+                <z> 0 </z>
+            </location>
+        </pointmass>
+    </mass_balance>
+
+    <ground_reactions>
+        <contact type="BOGEY" name="LEFT_MLG">
+            <location unit="IN">
+                <x> 40.1 </x>
+                <y> -9.9 </y>
+                <z> -10.1 </z>
+            </location>
+            <static_friction> 0.8 </static_friction>
+            <dynamic_friction> 0.5 </dynamic_friction>
+            <rolling_friction> 0.02 </rolling_friction>
+            <spring_coeff unit="LBS/FT"> 120 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 20 </damping_coeff>
+            <max_steer unit="DEG"> 0.0 </max_steer>
+            <brake_group> LEFT </brake_group>
+            <retractable>0</retractable>
+        </contact>
+        <contact type="BOGEY" name="RIGHT_MLG">
+            <location unit="IN">
+                <x> 40.1 </x>
+                <y> 9.9 </y>
+                <z> -10.1 </z>
+            </location>
+            <static_friction> 0.8 </static_friction>
+            <dynamic_friction> 0.5 </dynamic_friction>
+            <rolling_friction> 0.02 </rolling_friction>
+            <spring_coeff unit="LBS/FT"> 120 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 20 </damping_coeff>
+            <max_steer unit="DEG"> 0.0 </max_steer>
+            <brake_group> RIGHT </brake_group>
+            <retractable>0</retractable>
+        </contact>
+        <contact type="BOGEY" name="TAIL_LG">
+            <location unit="IN">
+                <x> 68.9 </x>
+                <y> 0 </y>
+                <z>-4.3 </z>
+            </location>
+            <static_friction> 0.8 </static_friction>
+            <dynamic_friction> 0.5 </dynamic_friction>
+            <rolling_friction> 0.02 </rolling_friction>
+            <spring_coeff unit="LBS/FT"> 24 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 20 </damping_coeff>
+            <max_steer unit="DEG"> 360.0 </max_steer>
+            <brake_group> NONE </brake_group>
+            <retractable>0</retractable>
+        </contact>
+        <contact type="BOGEY" name="NOSE_LG">
+            <location unit="IN">
+                <x>10</x>
+                <y>0</y>
+                <z>-8.3</z>
+            </location>
+            <static_friction> 0.8 </static_friction>
+            <dynamic_friction> 0.5 </dynamic_friction>
+            <rolling_friction> 0.02 </rolling_friction>
+            <spring_coeff unit="LBS/FT"> 24 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 20 </damping_coeff>
+            <max_steer unit="DEG"> 360.0 </max_steer>
+            <brake_group> NONE </brake_group>
+            <retractable>0</retractable>
+        </contact>
+
+    </ground_reactions>
+
+    <propulsion>
+        <engine file="Zenoah_G-26A">
+            <location unit="IN">
+                <x> 36 </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="IN">
+                    <x> 1 </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>
+        <tank type="FUEL">    <!-- Tank number 0 -->
+            <location unit="IN">
+                <x> 36.36 </x>
+                <y> 0 </y>
+                <z> -1.89375 </z>
+            </location>
+            <capacity unit="LBS"> 1.5 </capacity>
+            <contents unit="LBS"> 1.5 </contents>
+        </tank>
+    </propulsion>
+
+    <flight_control name="FCS: rascal">
+     <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>-0.35</min>
+                <max>0.3</max>
+            </range>
+            <output>fcs/elevator-pos-rad</output>
+        </aerosurface_scale>
+
+        <aerosurface_scale name="Elevator Normalized">
+            <input>fcs/elevator-pos-rad</input>
+            <domain>
+                <min>-0.3</min>
+                <max> 0.3</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>-0.35</min>
+                <max>0.35</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>-0.35</min>
+                <max>0.35</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>-0.35</min>
+                <max> 0.35</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>-0.35</min>
+                <max> 0.35</max>
+            </domain>
+            <range>
+                <min>-1</min>
+                <max> 1</max>
+            </range>
+            <output>fcs/right-aileron-pos-norm</output>
+        </aerosurface_scale>
+
+        <summer name="Rudder Command Sum">
+            <input>fcs/rudder-cmd-norm</input>
+            <input>fcs/yaw-trim-cmd-norm</input>
+            <clipto>
+                <min>-1</min>
+                <max>1</max>
+            </clipto>
+        </summer>
+
+        <aerosurface_scale name="Rudder Control">
+            <input>fcs/rudder-command-sum</input>
+            <range>
+                <min>-0.35</min>
+                <max>0.35</max>
+            </range>
+            <output>fcs/rudder-pos-rad</output>
+        </aerosurface_scale>
+
+        <aerosurface_scale name="Rudder Normalized">
+            <input>fcs/rudder-pos-rad</input>
+            <domain>
+                <min>-0.35</min>
+                <max> 0.35</max>
+            </domain>
+            <range>
+                <min>-1</min>
+                <max> 1</max>
+            </range>
+            <output>fcs/rudder-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>