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weasel_mavlink.xml
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weasel_mavlink.xml
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<!DOCTYPE airframe SYSTEM "../../airframe.dtd">
<!-- Weasel by Murat
Umarim
XBee modem
LEA 5H GPS
-->
<airframe name="Funjet">
<modules>
<load name="baro_board.xml"/>
<load name="airspeed_ads1114.xml"/>
<!--load name="mcp355x.xml"/-->
<load name="mavlink.xml"/>
</modules>
<firmware name="fixedwing">
<define name="USE_I2C0"/>
<define name="USE_I2C1"/>
<!--define name="AGR_CLIMB"/-->
<define name="ALT_KALMAN"/>
<define name="USE_AIRSPEED"/>
<!--define name="LOITER_TRIM"/-->
<!--define name="PITCH_TRIM"/-->
<target name="sim" board="pc"/>
<target name="ap" board="umarim_1.0">
<configure name="FLASH_MODE" value="IAP"/>
</target>
<subsystem name="radio_control" type="ppm"/>
<!-- Communication -->
<subsystem name="telemetry" type="dummy"/>
<!-- Actuators are automatically chosen according to board-->
<subsystem name="imu" type="umarim"/>
<subsystem name="ahrs" type="float_dcm">
<define name="USE_HIGH_ACCEL_FLAG"/>
</subsystem>
<subsystem name="control" type="new"/>
<subsystem name="navigation"/>
<!-- Sensors -->
<subsystem name="gps" type="ublox"/>
<!--subsystem name="spi"/-->
</firmware>
<firmware name="setup">
<target name="setup_actuators" board="umarim_1.0"/>
</firmware>
<!-- commands section -->
<servos>
<servo name="MOTOR" no="7" min="1040" neutral="1040" max="2000"/>
<servo name="AILEVON_LEFT" no="6" min="1900" neutral="1543" max="1100"/>
<servo name="AILEVON_RIGHT" no="3" min="1100" neutral="1561" max="1900"/>
</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="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.85"/>
<define name="MAX_PITCH" value="0.6"/>
</section>
<section name="IMU" prefix="IMU_">
<!-- Calibration Neutral -->
<define name="GYRO_P_NEUTRAL" value="-15"/>
<define name="GYRO_Q_NEUTRAL" value="94"/>
<define name="GYRO_R_NEUTRAL" value="-7"/>
<!-- SENS ITG3200 1/14.375 (deg/s)/LSB, rate frac 12bit => 1/14.375 * pi / 180 * 2^12 -->
<define name="GYRO_P_SENS" value="4.97312" integer="16"/>
<define name="GYRO_Q_SENS" value="4.97312" integer="16"/>
<define name="GYRO_R_SENS" value="4.97312" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="0"/>
<define name="ACCEL_Y_NEUTRAL" value="0"/>
<define name="ACCEL_Z_NEUTRAL" value="0"/>
<!-- SENS ADXL345 16G 31.2 mg/LSB, accel frac 10bit => 31.2 * 2^10 / 1000 -->
<define name="ACCEL_X_SENS" value="31.9488" integer="10"/>
<define name="ACCEL_Y_SENS" value="31.9488" integer="10"/>
<define name="ACCEL_Z_SENS" value="31.9488" integer="10"/>
<!-- Just to compile -->
<define name="MAG_X_NEUTRAL" value="0"/>
<define name="MAG_Y_NEUTRAL" value="0"/>
<define name="MAG_Z_NEUTRAL" value="0"/>
<define name="BODY_TO_IMU_PHI" value="0"/>
<define name="BODY_TO_IMU_THETA" value="0"/>
<define name="BODY_TO_IMU_PSI" value="0"/>
</section>
<section name="INS" prefix="INS_">
<define name="ROLL_NEUTRAL_DEFAULT" value="0.048" unit="rad"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="0." unit="rad"/>
</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="15." 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="TRIGGER_DELAY" value="1."/>
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="UNLOCKED_HOME_MODE" value="TRUE"/>
</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="-0.159999996424"/> <!-- -0.024 -->
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="5."/>
<!-- Cruise throttle + limits -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.5"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.85"/>
<define name="AUTO_PITCH_MAX_PITCH" value="RadOfDeg(20.)"/>
<define name="AUTO_PITCH_MIN_PITCH" value="-RadOfDeg(20.)"/>
<!-- Climb loop (throttle) -->
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.1" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PGAIN" value="-0.004"/> <!-- -0.005 -->
<define name="AUTO_THROTTLE_DGAIN" value="-0.01"/> <!-- 0.005 -->
<define name="AUTO_THROTTLE_IGAIN" value="-0.004"/> <!-- 0.005 -->
<!-- Climb loop (pitch) -->
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.02"/>
<define name="AUTO_PITCH_PGAIN" value="-0.038"/> <!-- -0.03 -->
<define name="AUTO_PITCH_DGAIN" value="-0.036"/> <!-- -0.03 -->
<define name="AUTO_PITCH_IGAIN" value="-0.0"/>
<!-- airspeed control -->
<define name="AUTO_AIRSPEED_SETPOINT" value="16."/>
<define name="AUTO_AIRSPEED_THROTTLE_PGAIN" value="0.1"/>
<define name="AUTO_AIRSPEED_THROTTLE_DGAIN" value="0.12"/>
<define name="AUTO_AIRSPEED_THROTTLE_IGAIN" value="0.0"/>
<define name="AUTO_AIRSPEED_PITCH_PGAIN" value="0.06"/>
<define name="AUTO_AIRSPEED_PITCH_DGAIN" value="0.0"/>
<define name="AUTO_AIRSPEED_PITCH_IGAIN" value="0.042"/>
<define name="AIRSPEED_MAX" value="30"/>
<define name="AIRSPEED_MIN" value="10"/>
<!-- groundspeed control -->
<define name="AUTO_GROUNDSPEED_SETPOINT" value="15"/>
<define name="AUTO_GROUNDSPEED_PGAIN" value="1."/>
<define name="AUTO_GROUNDSPEED_IGAIN" value="0."/>
<!-- pitch trim --> <!-- 5 deg -->
<define name="PITCH_LOITER_TRIM" value="RadOfDeg(0.)"/>
<define name="PITCH_DASH_TRIM" value="RadOfDeg(-0.)"/>
<define name="THROTTLE_SLEW" value="0.1"/>
</section>
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="-0.7"/>
<define name="ROLL_MAX_SETPOINT" value="0.8" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="ROLL_ATTITUDE_GAIN" value="-3800."/>
<define name="ROLL_RATE_GAIN" value="-500."/>
<define name="ROLL_IGAIN" value="-150."/>
<define name="ROLL_KFFA" value="0"/>
<define name="ROLL_KFFD" value="0"/>
<define name="PITCH_PGAIN" value="-10000."/>
<define name="PITCH_DGAIN" value="0."/>
<define name="PITCH_IGAIN" value="-250."/>
<define name="PITCH_KFFA" value="0."/>
<define name="PITCH_KFFD" value="0."/>
<define name="PITCH_OF_ROLL" value="RadOfDeg(0.0)"/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<!--define name="ELEVATOR_OF_ROLL" value="1400"/-->
</section>
<section name="NAV">
<define name="NAV_PITCH" value="0."/>
<define name="NAV_GLIDE_PITCH_TRIM" value="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"/>
<define name="HOME_RADIUS" value="100" unit="m"/>
</section>
<section name="SIMU">
<!--define name="ROLL_RESPONSE_FACTOR" value="10"/>
<define name="MAX_ROLL_DOT" value="20" unit="rad/s"/-->
<define name="JSBSIM_MODEL" value=""Malolo1""/>
<!--define name="JSBSIM_INIT" value=""Malolo1-IC""/-->
<define name="JSBSIM_LAUNCHSPEED" value="15.0"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
</airframe>