diff --git a/conf/airframes/examples/microjet_lisa_m.xml b/conf/airframes/examples/microjet_lisa_m.xml
new file mode 100644
index 0000000000..641542cc1e
--- /dev/null
+++ b/conf/airframes/examples/microjet_lisa_m.xml
@@ -0,0 +1,176 @@
+<!DOCTYPE airframe SYSTEM "../airframe.dtd">
+
+<!-- Microjet Multiplex (http://www.multiplex-rc.de/)
+     Lisa/M v1.0 board (http://paparazzi.enac.fr/wiki/Lisa/M_v10)
+     Aspirin IMU v1.5
+     Xbee modem in transparent mode
+-->
+
+<airframe name="Microjet Lisa/M 1.0">
+
+  <firmware name="fixedwing">
+    <target name="sim" 	board="pc"/>
+    <target name="ap"   board="lisa_m_1.0"/>
+
+    <define name="AGR_CLIMB" />
+    <define name="LOITER_TRIM" />
+    <define name="ALT_KALMAN" />
+
+    <subsystem name="radio_control" type="ppm"/>
+
+    <!-- Communication -->
+    <subsystem name="telemetry" 	type="transparent"/>
+
+    <!-- Sensors -->
+    <subsystem name="imu"           type="aspirin_v1.5"/>
+    <subsystem name="gps"           type="ublox"/>
+
+    <subsystem name="ahrs"          type="int_cmpl_quat"/>
+    <subsystem name="control"/>
+    <subsystem name="navigation"/>
+  </firmware>
+
+  <modules>
+    <load name="sys_mon.xml"/>
+  </modules>
+
+  <servos>
+    <servo name="MOTOR"         no="0" min="1290" neutral="1290" max="1810"/>
+    <servo name="AILEVON_LEFT"  no="1" min="2000" neutral="1510" max="1000"/>
+    <servo name="AILEVON_RIGHT" no="3" min="1000" neutral="1535" max="2000"/>
+  </servos>
+
+  <commands>
+    <axis name="THROTTLE" failsafe_value="0"/>
+    <axis name="ROLL"     failsafe_value="0"/>
+    <axis name="PITCH"    failsafe_value="0"/>
+  </commands>
+
+  <rc_commands>
+    <set command="THROTTLE" value="@THROTTLE"/>
+    <set command="ROLL"     value="@ROLL"/>
+    <set command="PITCH"    value="@PITCH"/>
+  </rc_commands>
+
+  <section name="MIXER">
+    <define name="AILEVON_AILERON_RATE" value="0.75"/>
+    <define name="AILEVON_ELEVATOR_RATE" value="0.75"/>
+  </section>
+
+  <command_laws>
+    <let var="aileron"  value="@ROLL  * AILEVON_AILERON_RATE"/>
+    <let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
+    <set servo="MOTOR"         value="@THROTTLE"/>
+    <set servo="AILEVON_LEFT"  value="$elevator - $aileron"/>
+    <set servo="AILEVON_RIGHT" value="$elevator + $aileron"/>
+  </command_laws>
+
+  <section name="IMU" prefix="IMU_">
+    <!-- ACCEL and GYRO calibration left out to take default datasheet values -->
+
+    <!-- replace this with your own mag calibration -->
+    <define name="MAG_X_NEUTRAL" value="-45"/>
+    <define name="MAG_Y_NEUTRAL" value="334"/>
+    <define name="MAG_Z_NEUTRAL" value="7"/>
+    <define name="MAG_X_SENS" value="4.47647816128" integer="16"/>
+    <define name="MAG_Y_SENS" value="4.71085671542" integer="16"/>
+    <define name="MAG_Z_SENS" value="4.41585354498" integer="16"/>
+
+    <define name="BODY_TO_IMU_PHI"   value="0." unit="deg"/>
+    <define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
+    <define name="BODY_TO_IMU_PSI"   value="0." unit="deg"/>
+  </section>
+
+  <section name="AHRS" prefix="AHRS_">
+    <!-- replace this with your local magnetic field -->
+    <define name="H_X" value="0.3770441"/>
+    <define name="H_Y" value="0.0193986"/>
+    <define name="H_Z" value="0.9259921"/>
+  </section>
+
+  <section name="INS" prefix="INS_">
+    <define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/>
+    <define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/>
+  </section>
+
+  <section name="VERTICAL CONTROL" prefix="V_CTL_">
+    <define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/>
+    <!-- outer loop proportional gain -->
+    <define name="ALTITUDE_PGAIN" value="0.03"/>
+    <!-- outer loop saturation -->
+    <define name="ALTITUDE_MAX_CLIMB" value="2."/>
+
+    <!-- auto throttle inner loop -->
+    <define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.32"/>
+    <define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/>
+    <define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.65"/>
+    <define name="AUTO_THROTTLE_LOITER_TRIM" value="1500"/>
+    <define name="AUTO_THROTTLE_DASH_TRIM" value="-4000"/>
+    <define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.15" unit="%/(m/s)"/>
+    <define name="AUTO_THROTTLE_PGAIN" value="0.01"/>
+    <define name="AUTO_THROTTLE_IGAIN" value="0.1"/>
+    <define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/>
+
+    <define name="THROTTLE_SLEW_LIMITER" value="2" unit="s"/>
+  </section>
+
+  <section name="HORIZONTAL CONTROL" prefix="H_CTL_">
+    <define name="COURSE_PGAIN" value="1.0"/>
+    <define name="COURSE_DGAIN" value="0.3"/>
+
+    <define name="ROLL_MAX_SETPOINT"  value="35"  unit="deg"/>
+    <define name="PITCH_MAX_SETPOINT" value="30"  unit="deg"/>
+    <define name="PITCH_MIN_SETPOINT" value="-30" unit="deg"/>
+
+    <define name="PITCH_PGAIN" value="12000."/>
+    <define name="PITCH_DGAIN" value="1.5"/>
+
+    <define name="ELEVATOR_OF_ROLL" value="1250"/>
+
+    <define name="ROLL_SLEW" value="0.1"/>
+
+    <define name="ROLL_ATTITUDE_GAIN" value="7500"/>
+    <define name="ROLL_RATE_GAIN" value="1500"/>
+  </section>
+
+  <section name="AGGRESSIVE" prefix="AGR_">
+    <define name="BLEND_START" value="20"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
+    <define name="BLEND_END" value="10"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes  CANNOT BE ZERO!!-->
+    <define name="CLIMB_THROTTLE" value="1.00"/><!-- Gaz for Aggressive Climb -->
+    <define name="CLIMB_PITCH" value="0.3"/><!-- Pitch for Aggressive Climb -->
+    <define name="DESCENT_THROTTLE" value="0.1"/><!-- Gaz for Aggressive Decent -->
+    <define name="DESCENT_PITCH" value="-0.25"/><!-- Pitch for Aggressive Decent -->
+    <define name="CLIMB_NAV_RATIO" value="0.8"/><!-- Percent Navigation for Altitude Error Equal to Start Altitude -->
+    <define name="DESCENT_NAV_RATIO" value="1.0"/>
+    </section>
+
+  <section name="FAILSAFE" prefix="FAILSAFE_">
+    <define name="DELAY_WITHOUT_GPS" value="2" 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"/>
+  </section>
+
+  <section name="AUTO1" prefix="AUTO1_">
+    <define name="MAX_ROLL" value="40." unit="deg"/>
+    <define name="MAX_PITCH" value="35." unit="deg"/>
+  </section>
+
+  <section name="BAT">
+    <define name="MILLIAMP_AT_FULL_THROTTLE" value="2000"/>
+    <define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
+    <define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/>
+    <define name="LOW_BAT_LEVEL" value="9.7" unit="V"/>
+    <define name="MAX_BAT_LEVEL" value="12.4" unit="V"/>
+  </section>
+
+  <section name="MISC">
+    <define name="NOMINAL_AIRSPEED" value="13." unit="m/s"/>
+    <define name="CARROT" value="5." unit="s"/>
+    <define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
+    <define name="CONTROL_RATE" value="60" unit="Hz"/>
+    <define name="ALT_KALMAN_ENABLED" value="TRUE"/>
+    <define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
+  </section>
+
+</airframe>