Files
paparazzi/conf/airframes/examples/easy_glider.xml
T
Gautier Hattenberger cab93d76bb [conf] change link to dtd in example airframes
the symbolic link allowed to compile but was making an error when
launching the simulation because the dtd is then taken in temp directory
(copy made by hand by Makefile.ac)
2012-05-09 22:10:10 +02:00

184 lines
6.6 KiB
XML

<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<airframe name="Easy Glider Tiny 0.99">
<!-- commands section -->
<servos>
<servo name="THROTTLE" no="0" min="1290" neutral="1290" max="1810"/>
<servo name="ELEVATOR" no="1" min="1770" neutral="1457" max="970"/>
<servo name="RUDDER" no="3" min="1040" neutral="1595" max="2040"/>
<servo name="AILERON_LEFT" no="4" min="2000" neutral="1508" max="1000"/>
<servo name="AILERON_RIGHT" no="5" min="2000" neutral="1527" max="1000"/>
</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 ? AILERON_DIFF : 1) * $roll"/>
<set servo="AILERON_RIGHT" value="($roll > 0 ? 1 : AILERON_DIFF) * $roll"/>
</command_laws>
<section name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.7"/>
<define name="MAX_PITCH" value="0.6"/>
</section>
<section name="INFRARED" prefix="IR_">
<define name="ADC_IR1_NEUTRAL" value="512"/>
<define name="ADC_IR2_NEUTRAL" value="512"/>
<define name="ADC_TOP_NEUTRAL" value="512"/>
<define name="HORIZ_SENSOR_TILTED" value="1"/>
<define name="IR2_SIGN" value="-1"/>
<define name="TOP_SIGN" value="1"/>
<define name="LATERAL_CORRECTION" value="0.75"/>
<define name="LONGITUDINAL_CORRECTION" value="0.75"/>
<define name="VERTICAL_CORRECTION" value="1.5"/>
<define name="ROLL_NEUTRAL_DEFAULT" value="0." unit="deg"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="18" unit="deg"/>
<define name="CORRECTION_UP" value="1.0"/>
<define name="CORRECTION_DOWN" value="1.0"/>
<define name="CORRECTION_LEFT" value="1.0"/>
<define name="CORRECTION_RIGHT" value="1.0"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="10000."/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" 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>
<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="0.55"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.85"/>
<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="1.10800004005"/>
<define name="ROLL_MAX_SETPOINT" value="0.6" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="15184.5644531"/>
<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="NAV">
<define name="NAV_PITCH" value="0."/>
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
</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>
<firmware name="fixedwing">
<target name="sim" board="pc"/>
<target name="ap" board="tiny_0.99"/>
<define name="AGR_CLIMB" />
<define name="LOITER_TRIM" />
<define name="ALT_KALMAN" />
<subsystem name="radio_control" type="ppm"/>
<!-- Communication -->
<subsystem name="telemetry" type="transparent">
<configure name="MODEM_BAUD" value="B9600"/>
</subsystem>
<!-- Actuators are automatically chosen according to board -->
<subsystem name="control"/>
<!-- Sensors -->
<subsystem name="ahrs" type="infrared"/>
<subsystem name="gps" type="ublox_utm"/>
<subsystem name="navigation"/>
</firmware>
<firmware name="setup">
<target name="tunnel" board="tiny_0.99" />
</firmware>
<modules>
<load name="adc_generic.xml">
<configure name="ADC_CHANNEL_GENERIC1" value="ADC_7"/> <!-- current sensor -->
</load>
<load name="infrared_adc.xml"/>
</modules>
</airframe>