Files
paparazzi/conf/airframes/LAAS/mmlaas_N3.xml
T
2010-10-25 08:54:38 +00:00

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XML

<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<airframe name="MiniMag Laas N3 Tiny 1.1">
<firmware name="fixedwing">
<target name="sim" board="pc">
<define name="AGR_CLIMB" />
<define name="LOITER_TRIM" />
<define name="ALT_KALMAN" />
</target>
<target name="ap" board="tiny_1.1">
<define name="AGR_CLIMB" />
<define name="LOITER_TRIM" />
<define name="ALT_KALMAN" />
</target>
<subsystem name="radio_control" type="ppm"/>
<!-- Communication -->
<subsystem name="telemetry" type="xbee_api">
<param name="MODEM_BAUD" value="B57600"/>
</subsystem>
<subsystem name="control"/>
<!-- Sensors -->
<subsystem name="attitude" type="infrared">
<param name="ADC_IR1" value="ADC_0"/>
<param name="ADC_IR2" value="ADC_1"/>
<param name="ADC_IR_TOP" value="ADC_2"/>
</subsystem>
<subsystem name="gps" type="ublox_lea4p"/>
<subsystem name="navigation"/>
</firmware>
<firmware name="setup">
<target name="tunnel" board="tiny_1.1" />
<target name="setup_actuators" board="tiny_1.1" />
</firmware>
<modules>
<load name="formation_flight.xml"/>
<load name="tcas.xml"/>
<!--load name="potential.xml"/-->
</modules>
<!-- commands section -->
<servos>
<servo name="THROTTLE" no="0" min="1200" neutral="1200" max="2000"/>
<!-- max = valeur aileron vers le bas-->
<!-- Aileron gauche (jaune) oppose de l'aileron droit (blanc) -->
<!-- !!! pb d'inversion des sorties, roll < 0 à droite -->
<servo name="AILERON_LEFT" no="1" min="1775" neutral="1525" max="1150"/>
<servo name="AILERON_RIGHT" no="3" min="1775" neutral="1520" max="1200"/>
<servo name="RUDDER" no="4" min="1850" neutral="1550" max="1150"/>
<servo name="ELEVATOR" no="5" min="2000" neutral="1580" max="1150"/>
</servos>
<commands>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
</commands>
<rc_commands>
<set command="THROTTLE" value="@THROTTLE"/>
<set command="ROLL" value="@ROLL"/>
<set command="PITCH" value="@PITCH"/>
<set command="YAW" value="@YAW"/>
</rc_commands>
<section name="MIXER">
<define name="AILERON_DIFF" value="0.66"/>
<define name="COMBI_SWITCH" value="1.0"/>
</section>
<command_laws>
<set servo="THROTTLE" value="@THROTTLE"/>
<set servo="ELEVATOR" value="@PITCH"/>
<set servo="RUDDER" value="@YAW + @ROLL*COMBI_SWITCH"/>
<let var="roll" value="@ROLL"/>
<set servo="AILERON_LEFT" value="($roll > 0 ? 1 : AILERON_DIFF) * $roll"/>
<set servo="AILERON_RIGHT" value="($roll > 0 ? AILERON_DIFF : 1) * $roll"/>
</command_laws>
<section name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.6"/>
<define name="MAX_PITCH" value="0.6"/>
</section>
<section name="INFRARED" prefix="IR_">
<define name="ROLL_NEUTRAL_DEFAULT" value="3" unit="deg"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="9" unit="deg"/>
<define name="HORIZ_SENSOR_TILTED" value="1"/>
<define name="IR2_SIGN" value="-1"/>
<define name="TOP_SIGN" value="1"/>
<!--linear name="RollOfIrs" arity="2" coeff1="-0.7" coeff2="0.7"/>
<linear name="PitchOfIrs" arity="2" coeff1="-0.7" coeff2="-0.7"/>
<linear name="TopOfIr" arity="1" coeff1="1"/-->
<define name="ADC_IR1_NEUTRAL" value="519"/>
<define name="ADC_IR2_NEUTRAL" value="508"/>
<define name="ADC_TOP_NEUTRAL" value="516"/>
<define name="LATERAL_CORRECTION" value="1."/>
<define name="LONGITUDINAL_CORRECTION" value="1."/>
<define name="VERTICAL_CORRECTION" value="1.4"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="8600"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
</section>
<section name="MISC">
<define name="NOMINAL_AIRSPEED" value="11." unit="m/s"/>
<define name="MINIMUM_AIRSPEED" value="8." unit="m/s"/>
<define name="MAXIMUM_AIRSPEED" value="16." unit="m/s"/>
<define name="CARROT" value="3." unit="s"/>
<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
<!-- <define name="XBEE_INIT" value="\"ATPL2\rATRN1\rATTT80\rATBD6\rATWR\r\""/> -->
<define name="XBEE_INIT" value="\"ATPL2\rATRN1\rATTT80\r\""/>
<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
<define name="ALT_KALMAN_ENABLED" value="TRUE"/>
<define name="TRIGGER_DELAY" value="1."/>
<define name="DEFAULT_CIRCLE_RADIUS" value="60."/>
</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="-0.15"/>
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="2."/>
<!-- auto throttle inner loop -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.55"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.30"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.90"/>
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1500"/>
<define name="AUTO_THROTTLE_DASH_TRIM" value="-2000"/>
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.15" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PGAIN" value="-0.05"/>
<define name="AUTO_THROTTLE_IGAIN" value="0.1"/>
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/>
<!-- auto pitch inner loop -->
<define name="AUTO_PITCH_PGAIN" value="-0.065"/>
<define name="AUTO_PITCH_IGAIN" value="0.15"/>
<define name="AUTO_PITCH_MAX_PITCH" value="0.35"/>
<define name="AUTO_PITCH_MIN_PITCH" value="-0.35"/>
<define name="THROTTLE_SLEW" value="0.05"/>
</section>
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="-1."/>
<define name="ROLL_MAX_SETPOINT" value="0.6" unit="radians"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="radians"/>
<define name="ROLL_ATTITUDE_GAIN" value="-10000"/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<define name="PITCH_PGAIN" value="-12000."/>
<define name="PITCH_DGAIN" value="1.5"/>
<define name="ELEVATOR_OF_ROLL" value="1250"/>
</section>
<section name="NAV">
<define name="NAV_PITCH" value="0."/>
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
<define name="NAV_GROUND_SPEED_PGAIN" value="-0.015"/>
<define name="NAV_FOLLOW_PGAIN" value="-0.05"/>
</section>
<section name="FORMATION" prefix="FORM_">
<define name="CARROT" value="3." unit="s"/> <!-- carrot distance for followers -->
<define name="POS_PGAIN" value="0.02"/> <!-- coef on position error -->
<define name="SPEED_PGAIN" value="0.4"/> <!-- coef on speed error -->
<define name="COURSE_PGAIN" value="0.8"/> <!-- coef on course error (override course pgain for followers) -->
<define name="ALTITUDE_PGAIN" value="0.1"/> <!-- coef on altitude error -->
<define name="PROX" value="60." unit="m"/> <!-- proximity distance -->
<define name="MODE" value="0"/> <!-- mode 0 = global, 1 = local -->
</section>
<section name="TCAS" prefix="TCAS_">
<define name="TAU_TA" value="10." unit="s"/> <!-- traffic advisory -->
<define name="TAU_RA" value="6." unit="s"/> <!-- resolution advisory -->
<define name="ALIM" value="15." unit="m"/> <!-- altitude limitation -->
<define name="DT_MAX" value="2000" unit="ms"/> <!-- lost comm or timeout -->
</section>
<section name="POTENTIAL">
<define name="FORCE_POS_GAIN" value="50"/>
<define name="FORCE_SPEED_GAIN" value="1"/>
<define name="FORCE_CLIMB_GAIN" value="8"/>
</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="0.8"/><!-- 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="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="YAW_RESPONSE_FACTOR" value="1."/>
</section>
<makefile>
# external module
#ap.srcs += external.c
</makefile>
</airframe>