diff --git a/Tools/autotest/aircraft/Rascal/Rascal110-JSBSim.xml b/Tools/autotest/aircraft/Rascal/Rascal110-JSBSim.xml
deleted file mode 100644
index a8deb22bb2..0000000000
--- a/Tools/autotest/aircraft/Rascal/Rascal110-JSBSim.xml
+++ /dev/null
@@ -1,522 +0,0 @@
-<?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 rascal </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"> 1.95 </ixx>
-        <iyy unit="SLUG*FT2"> 1.55 </iyy>
-        <izz unit="SLUG*FT2"> 1.91 </izz>
-        <ixy unit="SLUG*FT2"> 0 </ixy>
-        <ixz unit="SLUG*FT2"> 0 </ixz>
-        <iyz unit="SLUG*FT2"> 0 </iyz>
-        <emptywt unit="LBS"> 13 </emptywt>
-        <location name="CG" unit="IN">
-            <x> 36.4 </x>
-            <y> 0 </y>
-            <z> 4 </z>
-        </location>
-    </mass_balance>
-
-    <ground_reactions>
-        <contact type="BOGEY" name="LEFT_MLG">
-            <location unit="IN">
-                <x> 33.1 </x>
-                <y> -9.9 </y>
-                <z> -13.1 </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> 33.1 </x>
-                <y> 9.9 </y>
-                <z> -13.1 </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> -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>