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[paparazzi-commits] [4733] Add target jsbsim to compile both simulator i


From: Gautier Hattenberger
Subject: [paparazzi-commits] [4733] Add target jsbsim to compile both simulator independantly
Date: Thu, 25 Mar 2010 09:27:27 +0000

Revision: 4733
          http://svn.sv.gnu.org/viewvc/?view=rev&root=paparazzi&revision=4733
Author:   gautier
Date:     2010-03-25 09:27:26 +0000 (Thu, 25 Mar 2010)
Log Message:
-----------
Add  target jsbsim to compile both simulator independantly

Modified Paths:
--------------
    paparazzi3/trunk/Makefile.ac
    paparazzi3/trunk/conf/airframes/ENAC/fixed-wing/spocII.xml
    paparazzi3/trunk/conf/autopilot/sitl_jsbsim.makefile
    paparazzi3/trunk/conf/simulator/Corsica/Corsica.xml
    paparazzi3/trunk/sw/simulator/launchsitl
    paparazzi3/trunk/sw/simulator/sim_ac_jsbsim.c

Added Paths:
-----------
    paparazzi3/trunk/conf/Makefile.jsbsim

Removed Paths:
-------------
    paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml

Modified: paparazzi3/trunk/Makefile.ac
===================================================================
--- paparazzi3/trunk/Makefile.ac        2010-03-25 07:01:06 UTC (rev 4732)
+++ paparazzi3/trunk/Makefile.ac        2010-03-25 09:27:26 UTC (rev 4733)
@@ -159,6 +159,9 @@
 tiny_bl.upload:
        lpc21isp -control $(AIRBORNE)/arm7/test/bootloader/bl.hex 
$(BOOTLOADER_DEVICE) 38400 12000
 
+jsbsim jsbsim.compile: ac_h
+       cd $(AIRBORNE); $(MAKE) TARGET=jsbsim ARCHI=jsbsim all
+
 sim: ac_h
        cd $(AIRBORNE); $(MAKE) TARGET=sim ARCHI=sim all
 

Added: paparazzi3/trunk/conf/Makefile.jsbsim
===================================================================
--- paparazzi3/trunk/conf/Makefile.jsbsim                               (rev 0)
+++ paparazzi3/trunk/conf/Makefile.jsbsim       2010-03-25 09:27:26 UTC (rev 
4733)
@@ -0,0 +1,100 @@
+# Hey Emacs, this is a -*- makefile -*-
+# 
+#   $Id: Makefile.sim 3505 2009-06-17 12:59:32Z hecto $
+#   Copyright (C) 2006 Pascal Brisset, Antoine Drouin
+#
+# This file is part of paparazzi.
+#
+# paparazzi is free software; you can redistribute it and/or modify
+# it under the terms of the GNU General Public License as published by
+# the Free Software Foundation; either version 2, or (at your option)
+# any later version.
+#
+# paparazzi is distributed in the hope that it will be useful,
+# but WITHOUT ANY WARRANTY; without even the implied warranty of
+# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
+# GNU General Public License for more details.
+#
+# You should have received a copy of the GNU General Public License
+# along with paparazzi; see the file COPYING.  If not, write to
+# the Free Software Foundation, 59 Temple Place - Suite 330,
+# Boston, MA 02111-1307, USA.  
+# 
+
+#
+# This is the Makefile for the JSBSim target.
+# Compilator: g++
+#
+
+SRC_ARCH = sim
+
+CC = g++
+SIMDIR = $(PAPARAZZI_SRC)/sw/simulator
+
+# Launch with "make Q=''" to get full command display
+Q=@
+
+#
+# Compilation flags
+#
+
+CFLAGS = -W -Wall $(INCLUDES) -I$(PAPARAZZI_SRC)/sw/airborne/$(SRC_ARCH) 
$($(TARGET).CFLAGS) $(LOCAL_CFLAGS) -O2
+
+LDFLAGS                =       -lm $($(TARGET).LDFLAGS)
+
+#
+# General rules
+#
+
+$(TARGET).srcsnd = $(notdir $($(TARGET).srcs))
+$(TARGET).objso        = $($(TARGET).srcs:%.c=$(OBJDIR)/%.o)
+$(TARGET).objs = $($(TARGET).objso:%.S=$(OBJDIR)/%.o)
+
+all compile: $(OBJDIR)/simsitl
+
+
+$(OBJDIR)/simsitl : $($(TARGET).objs)
+       @echo LD $@
+       $(Q)$(CC) $(CFLAGS) -o $@ $($(TARGET).objs) $(LDFLAGS)
+
+
+%.s: %.c
+       $(CC) $(CFLAGS) -S -o $@ $<
+
+%.s: %.cpp
+       $(CC) $(CFLAGS) -S -o $@ $<
+
+$(OBJDIR)/%.s: %.c
+       @echo CC $@
+       $(Q)test -d $(dir $@) || mkdir -p $(dir $@)
+       $(CC) $(CFLAGS) -S -o $@ $<
+
+$(OBJDIR)/%.s: %.cpp
+       @echo CC $@
+       $(Q)test -d $(dir $@) || mkdir -p $(dir $@)
+       $(CC) $(CFLAGS) -S -o $@ $<
+
+$(OBJDIR)/%.o: %.c $(OBJDIR)/../Makefile.ac
+       @echo CC $@
+       $(Q)test -d $(dir $@) || mkdir -p $(dir $@)
+       $(Q)$(CC) $(CFLAGS) -c -o $@ $<
+
+$(OBJDIR)/%.o: %.cpp $(OBJDIR)/../Makefile.ac
+       @echo CC++ $@
+       $(Q)test -d $(dir $@) || mkdir -p $(dir $@)
+       $(Q)$(CC) $(CFLAGS) -c -o $@ $<
+
+
+#
+# Dependencies
+#
+$(OBJDIR)/.depend:
+       @test -d $(OBJDIR) || mkdir -p $(OBJDIR)
+       @echo DEPEND $@
+       $(Q)$(CC) -MM -MG $(CFLAGS) $($(TARGET).srcs) | sed 
's|\([^\.]*\.o\)|$(OBJDIR)/\1|' > $@
+
+ifneq ($(MAKECMDGOALS),clean) 
+ifneq ($(MAKECMDGOALS),erase) 
+-include $(OBJDIR)/.depend
+endif
+endif

Modified: paparazzi3/trunk/conf/airframes/ENAC/fixed-wing/spocII.xml
===================================================================
--- paparazzi3/trunk/conf/airframes/ENAC/fixed-wing/spocII.xml  2010-03-25 
07:01:06 UTC (rev 4732)
+++ paparazzi3/trunk/conf/airframes/ENAC/fixed-wing/spocII.xml  2010-03-25 
09:27:26 UTC (rev 4733)
@@ -193,13 +193,19 @@
   </section>
 
   <section name="FAILSAFE" prefix="FAILSAFE_">
-       <define name="DELAY_WITHOUT_GPS" value="1" unit="s"/>
-       <define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
-       <define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
-       <define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
-       <define name="HOME_RADIUS" value="100" unit="m"/>
-</section>
- 
+    <define name="DELAY_WITHOUT_GPS" value="1" unit="s"/>
+    <define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
+    <define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
+    <define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
+    <define name="HOME_RADIUS" value="100" unit="m"/>
+  </section>
+
+  <section name="SIMU">
+    <define name="JSBSIM_MODEL" value="&quot;Corsica&quot;"/>
+    <define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
+    <define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
+  </section>
+
  <makefile>
 CONFIG = \"tiny_2_1_1.h\"
 
@@ -258,7 +264,17 @@
 
 sim.srcs += nav_line.c nav_survey_rectangle.c
 
+# Config for JSBSim simulation
+include $(PAPARAZZI_SRC)/conf/autopilot/sitl_jsbsim.makefile
 
+jsbsim.CFLAGS += -I/home/cocoleon/usr/include/JSBSim
+jsbsim.LDFLAGS += -L/home/cocoleon/usr/lib/
+
+jsbsim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM 
-DALT_KALMAN
+jsbsim.srcs += nav_line.c nav_survey_rectangle.c
+jsbsim.srcs += $(SIMDIR)/sim_ac_fw.c
+
+
 # a test program to setup actuators 
 setup_actuators.ARCHDIR = $(ARCHI)
 setup_actuators.ARCH = arm7tdmi

Modified: paparazzi3/trunk/conf/autopilot/sitl_jsbsim.makefile
===================================================================
--- paparazzi3/trunk/conf/autopilot/sitl_jsbsim.makefile        2010-03-25 
07:01:06 UTC (rev 4732)
+++ paparazzi3/trunk/conf/autopilot/sitl_jsbsim.makefile        2010-03-25 
09:27:26 UTC (rev 4733)
@@ -1,15 +1,16 @@
-SIM_TYPE = JSBSIM
-sim.ARCHDIR = $(ARCHI)
-sim.ARCH = sitl
-sim.TARGET = autopilot
-sim.TARGETDIR = autopilot
+jsbsim.ARCHDIR = $(ARCHI)
+jsbsim.ARCH = sitl
+jsbsim.TARGET = autopilot
+jsbsim.TARGETDIR = autopilot
 # external libraries
-sim.CFLAGS = -I$(SIMDIR) -I/usr/include `pkg-config glib-2.0 --cflags`
-sim.LDFLAGS += `pkg-config glib-2.0 --libs` -lm -lpcre -lglibivy -L/usr/lib 
-lJSBSim
+jsbsim.CFLAGS = -I$(SIMDIR) -I/usr/include `pkg-config glib-2.0 --cflags`
+jsbsim.LDFLAGS += `pkg-config glib-2.0 --libs` -lm -lpcre -lglibivy -L/usr/lib 
-lJSBSim
 
-sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK 
-DDOWNLINK_TRANSPORT=IvyTransport -DINFRARED -DNAV -DLED -DWIND_INFO
-sim.srcs = $(SRC_ARCH)/jsbsim_hw.c $(SRC_ARCH)/jsbsim_gps.c 
$(SRC_ARCH)/jsbsim_ir.c $(SRC_ARCH)/jsbsim_transport.c 
$(SRC_ARCH)/ivy_transport.c 
-sim.srcs += latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c 
infrared.c fw_h_ctl.c fw_v_ctl.c nav.c estimator.c sys_time.c main_fbw.c 
main_ap.c datalink.c
-sim.srcs += $(SIMDIR)/sim_ac_jsbsim.c
-#$(SIMDIR)/sim_ac_fw.c
+jsbsim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK 
-DDOWNLINK_TRANSPORT=IvyTransport -DINFRARED -DNAV -DLED -DWIND_INFO
+jsbsim.srcs = $(SRC_ARCH)/jsbsim_hw.c $(SRC_ARCH)/jsbsim_gps.c 
$(SRC_ARCH)/jsbsim_ir.c $(SRC_ARCH)/jsbsim_transport.c 
$(SRC_ARCH)/ivy_transport.c 
+jsbsim.srcs += latlong.c radio_control.c downlink.c commands.c gps.c 
inter_mcu.c infrared.c fw_h_ctl.c fw_v_ctl.c nav.c estimator.c sys_time.c 
main_fbw.c main_ap.c datalink.c
+jsbsim.srcs += $(SIMDIR)/sim_ac_jsbsim.c
+# Choose in your airframe file type of airframe
+# jsbsim.srcs += $(SIMDIR)/sim_ac_fw.c
+# jsbsim.srcs += $(SIMDIR)/sim_ac_booz.c
 

Modified: paparazzi3/trunk/conf/simulator/Corsica/Corsica.xml
===================================================================
--- paparazzi3/trunk/conf/simulator/Corsica/Corsica.xml 2010-03-25 07:01:06 UTC 
(rev 4732)
+++ paparazzi3/trunk/conf/simulator/Corsica/Corsica.xml 2010-03-25 09:27:26 UTC 
(rev 4733)
@@ -52,9 +52,69 @@
     </mass_balance>
 
 
+    <ground_reactions>
+        <contact type="BOGEY" name="LEFT_MLG">
+            <location unit="M">
+                <x> 0.07 </x>
+                <y> -0.6 </y>
+                <z> -0.01 </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"> 30 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 5 </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="M">
+                <x> 0.07 </x>
+                <y> 0.6 </y>
+                <z> -0.01 </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"> 30 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 5 </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="M">
+                <x> 0.6 </x>
+                <y> 0.0 </y>
+                <z> -0.01 </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"> 6 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 5 </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="M">
+                <x> 0.01 </x>
+                <y> 0.0 </y>
+                <z> -0.01 </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"> 6 </spring_coeff>
+            <damping_coeff unit="LBS/FT/SEC"> 5 </damping_coeff>
+            <max_steer unit="DEG"> 360.0 </max_steer>
+            <brake_group> NONE </brake_group>
+            <retractable>0</retractable>
+        </contact>
+    </ground_reactions>
 
-<!--Ground reactions deleted -->
-
     <propulsion>
         <engine file="Axi">
             <location unit="M">
@@ -82,6 +142,14 @@
                 <p_factor>1.0</p_factor>
             </thruster>
         </engine>
+        <tank type="OXIDIZER">    <!-- Tank number 0 --> 
+            <location unit="M">
+                <x> 0.7 </x>
+                <y> 0.0 </y>
+                <z> 0.0 </z>
+            </location>
+            <capacity unit="LBS"> 0.001 </capacity>
+        </tank>
     </propulsion>
 
     <flight_control name="Corsica">

Deleted: paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml
===================================================================
--- paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml     2010-03-25 
07:01:06 UTC (rev 4732)
+++ paparazzi3/trunk/conf/simulator/Corsica/Corsica2010.xml     2010-03-25 
09:27:26 UTC (rev 4733)
@@ -1,388 +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> 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-deg</independentVar>
-                          <tableData>
-                              -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/CDbeta">
-                <description>Drag_due_to_sideslip</description>
-                <product>
-                    <property>aero/qbar-psf</property>
-                    <property>metrics/Sw-sqft</property>
-                      <table>
-                          <independentVar>aero/beta-deg</independentVar>
-                          <tableData>
-                              -10.0   -0.00284
-                              0.0     0.0
-                              10.0    -0.00284
-                          </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-deg</property>
-                    <value>0.000094</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>-0.141391</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>
-                    <property>aero/alpha-rad</property>
-                    <value>5.1460</value>
-                </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-deg</property>
-                    <value>0.003644</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>-0.04235</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>-0.561207</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>0.17269</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/right-aileron-pos-deg</property>
-                    <value>-0.004076</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>-0.523384</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-deg</property>
-                    <value>-0.014833</value>
-                </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>-15.281710</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>0.039729</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>-0.048425</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/right-aileron-pos-deg</property>
-                    <value>0.00026</value>
-                </product>
-            </function>
-        </axis>
-    </aerodynamics>
-</fdm_config>

Modified: paparazzi3/trunk/sw/simulator/launchsitl
===================================================================
--- paparazzi3/trunk/sw/simulator/launchsitl    2010-03-25 07:01:06 UTC (rev 
4732)
+++ paparazzi3/trunk/sw/simulator/launchsitl    2010-03-25 09:27:26 UTC (rev 
4733)
@@ -12,14 +12,22 @@
   try
     let rec loop = fun i ->
       if Sys.argv.(i) = "-a" && (i+1) < n then
-       let ac = Sys.argv.(i+1) in
-       (* Shift other args *)
-       for j = i+2 to n-1 do Sys.argv.(j-2) <- Sys.argv.(j) done;
-       ac
+        let ac = Sys.argv.(i+1) in
+        (* Shift other args *)
+        for j = i+2 to n-1 do Sys.argv.(j-2) <- Sys.argv.(j) done;
+        ac
       else if i = n then raise Not_found
       else loop (i+1) in
     let ac = loop 0 in
-    let com = paparazzi_home // "var" // ac // "sim/simsitl" in
+    (*let rec sim_type = fun i ->
+      if Sys.argv.(i) = "-jsbsim" then
+        "jsbsim"
+      else if i = n then "sim"
+      else loop (i+1) in
+    let sim = sim_type 0 in*)
+    let sim = "jsbsim" in
+    let com = paparazzi_home // "var" // ac // sim // "simsitl" in
+    prerr_endline com;
     if not (Sys.file_exists com) then begin
       Printf.fprintf stderr "Error: '%s' is missing. Build target sim for A/C 
%s ?\n" com ac;
       exit 1

Modified: paparazzi3/trunk/sw/simulator/sim_ac_jsbsim.c
===================================================================
--- paparazzi3/trunk/sw/simulator/sim_ac_jsbsim.c       2010-03-25 07:01:06 UTC 
(rev 4732)
+++ paparazzi3/trunk/sw/simulator/sim_ac_jsbsim.c       2010-03-25 09:27:26 UTC 
(rev 4733)
@@ -112,7 +112,7 @@
 
 
 static void ivy_transport_init(void) {
-  IvyInit ("Paparazzi sim " + AC_ID, "READY", NULL, NULL, NULL, NULL);
+  IvyInit ("Paparazzi jsbsim " + AC_ID, "READY", NULL, NULL, NULL, NULL);
   IvyStart(ivyBus.c_str());
 }
 
@@ -147,6 +147,9 @@
     else if (argument == "-norc") {
       // Compatibility with ocaml
     }
+    else if (argument == "-jsbsim") {
+      // Compatibility with ocaml
+    }
     else if (argument == "-b") {
       ivyBus = string(argv[++i]);
     }





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