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2024-05-30 09:25:58 +02:00

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<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<!-- this is a mentor Fixedwing with a Pixhawk 4 autopilot -->
<airframe name="Mentor">
<description>Mentor</description>
<firmware name="fixedwing">
<target name="ap" board="px4fmu_5.0_chibios"/>
<target name="nps" board="pc">
<module name="radio_control" type="spektrum"/>
<module name="fdm" type="jsbsim"/>
</target>
<configure name="PERIODIC_FREQUENCY" value="500"/>
<module name="telemetry" type="transparent">
<configure name="MODEM_BAUD" value="B115200"/>
</module>
<module name="imu" type="mpu6000"/>
<module name="gps" type="ublox">
<!--configure name="GPS_PORT" value="UART1"/-->
</module>
<module name="gps" type="ubx_ucenter"/>
<module name="ahrs" type="int_cmpl_quat">
<configure name="USE_MAGNETOMETER" value="FALSE"/>
<define name="AHRS_GRAVITY_UPDATE_COORDINATED_TURN"/>
</module>
<module name="ins" type="alt_float"/>
<module name="mag_ist8310">
<define name="MODULE_IST8310_UPDATE_AHRS" value="TRUE"/>
<configure name="MAG_IST8310_I2C_DEV" value="I2C3"/>
</module>
<!--module name="lidar" type="tfmini"/-->
<!--module name="airspeed" type="ms45xx_i2c">
<define name="USE_I2C4"/>
<configure name="MS45XX_I2C_DEV" value="i2c4"/>
</module-->
<module name="air_data"/>
<module name="control" type="energy"/>
<module name="navigation"/>
<module name="actuators" type="pwm"/>
<module name="radio_control" type="sbus">
<configure name="SBUS_PORT" value="UART3"/>
</module>
<!-- Logger -->
<!--module name="tlsf"/>
<module name="pprzlog"/>
<module name="logger" type="sd_chibios"/>
<module name="flight_recorder"/-->
</firmware>
<servos>
<servo name="THROTTLE" no="0" min="1000" neutral="1000" max="2000"/>
<servo name="AILERON_LEFT" no="1" min="1800" neutral="1500" max="1200"/>
<servo name="AILERON_RIGHT" no="2" min="1200" neutral="1500" max="1800"/>
<servo name="ELEVATOR" no="3" min="900" neutral="1500" max="2100"/>
<servo name="RUDDER" no="4" min="1900" neutral="1500" max="1100"/>
</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="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="1.2"/>
<define name="MAX_PITCH" value="0.8"/>
</section>
<command_laws>
<set servo="AILERON_LEFT" value="@ROLL"/>
<set servo="AILERON_RIGHT" value="-@ROLL"/>
<set servo="THROTTLE" value="@THROTTLE"/>
<set servo="ELEVATOR" value="@PITCH"/>
<set servo="RUDDER" value="@YAW"/>
</command_laws>
<section name="TRIM" prefix="COMMAND_">
<define name="ROLL_TRIM" value="0"/>
<define name="PITCH_TRIM" value="788."/>
</section>
<section name="FAILSAFE" prefix="FAILSAFE_">
<define name="DEFAULT_THROTTLE" value="0.35" unit="%"/>
<define name="DEFAULT_ROLL" value="10.0" unit="deg"/>
<define name="DEFAULT_PITCH" value="5.0" unit="deg"/>
<define name="HOME_RADIUS" value="DEFAULT_CIRCLE_RADIUS" unit="m"/>
<define name="KILL_MODE_DISTANCE" value="(MAX_DIST_FROM_HOME*1.5)"/>
<define name="DELAY_WITHOUT_GPS" value="10" unit="s"/>
</section>
<!-- ************************* SENSORS ************************* -->
<section name="IMU" prefix="IMU_">
<!-- replace this with your own calibration -->
<define name="MAG_X_NEUTRAL" value="-179"/>
<define name="MAG_Y_NEUTRAL" value="-21"/>
<define name="MAG_Z_NEUTRAL" value="79"/>
<define name="MAG_X_SENS" value="4.17334785618" integer="16"/>
<define name="MAG_Y_SENS" value="3.98885954135" integer="16"/>
<define name="MAG_Z_SENS" value="4.40442339014" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="0" unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="14" unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0" unit="deg"/>
</section>
<section name="AHRS" prefix="AHRS_">
<!-- Local magnetic field, on 3D fix is update by geo_mag module -->
<define name="H_X" value="0.51562740288882"/>
<define name="H_Y" value="-0.05707735220832"/>
<define name="H_Z" value="0.85490967783446"/>
</section>
<section name="INS" prefix="INS_">
<define name="ROLL_NEUTRAL_DEFAULT" value="0.0" unit="deg"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/>
</section>
<!-- ************************* GAINS ************************* -->
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.89"/>
<define name="COURSE_DGAIN" value="0.27"/>
<define name="COURSE_PRE_BANK_CORRECTION" value="1.0"/>
<define name="ROLL_MAX_SETPOINT" value="45" unit="deg"/>
<define name="PITCH_MAX_SETPOINT" value="50" unit="deg"/>
<define name="PITCH_MIN_SETPOINT" value="-50" unit="deg"/>
<define name="PITCH_PGAIN" value="13000"/>
<define name="PITCH_DGAIN" value="1.5"/>
<define name="ELEVATOR_OF_ROLL" value="1300"/>
<define name="ROLL_SLEW" value="1."/>
<define name="ROLL_ATTITUDE_GAIN" value="10000"/>
<define name="ROLL_RATE_GAIN" value="500."/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
<!-- power -->
<define name="POWER_CTL_BAT_NOMINAL" value="14.8" unit="volt"/>
<!-- outer loop proportional gain -->
<define name="ALTITUDE_PGAIN" value="0.1"/>
<define name="AIRSPEED_PGAIN" value="0.0"/>
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="3."/>
<define name="MAX_ACCELERATION" value="2."/>
<!-- energy -->
<define name="ENERGY_TOT_PGAIN" value="0.0"/>
<define name="ENERGY_TOT_IGAIN" value="0.0"/>
<define name="ENERGY_DIFF_PGAIN" value="0.0"/>
<define name="ENERGY_DIFF_IGAIN" value="0.0"/>
<define name="GLIDE_RATIO" value="7."/>
<!-- auto throttle -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.55"/>
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.1" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.15"/>
<!-- extra's -->
<define name="AUTO_THROTTLE_OF_AIRSPEED_PGAIN" value="0.0"/>
<define name="AUTO_THROTTLE_OF_AIRSPEED_IGAIN" value="0.0"/>
<!-- extra's -->
<define name="AUTO_PITCH_OF_AIRSPEED_PGAIN" value="0.0"/>
<define name="AUTO_PITCH_OF_AIRSPEED_IGAIN" value="0.0"/>
<define name="AUTO_PITCH_OF_AIRSPEED_DGAIN" value="0.0"/>
<define name="THROTTLE_SLEW_LIMITER" value="1" unit="m/s/s"/>
<!--define name="AUTO_GROUNDSPEED_SETPOINT" value="15." unit="m/s"/>
<define name="AUTO_GROUNDSPEED_PGAIN" value="1."/>
<define name="AUTO_GROUNDSPEED_IGAIN" value="0"/-->
</section>
<!-- ************************* MISC ************************* -->
<section name="BAT">
<define name="VoltageOfAdc(adc)" value="((3.3f/4096.0f) * 12.0877510901 * adc)"/>
<!--define name="MilliAmpereOfAdc(adc)" value="((adc) - 505) * 124.0f"/-->
<define name="LOW_BAT_LEVEL" value="10.5" unit="V"/>
<define name="CRITIC_BAT_LEVEL" value="10" unit="V"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.1" unit="V"/>
</section>
<section name="MISC">
<define name="CLIMB_AIRSPEED" value="14." unit="m/s"/>
<define name="NOMINAL_AIRSPEED" value="16." unit="m/s"/>
<define name="GLIDE_AIRSPEED" value="12." unit="m/s"/>
<define name="RACE_AIRSPEED" value="25." unit="m/s"/>
<define name="STALL_AIRSPEED" value="10." unit="m/s"/>
<define name="CARROT" value="5." unit="s"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="NAV_GLIDE_PITCH_TRIM" value="0."/>
</section>
<section name="CATAPULT" prefix="NAV_CATAPULT_">
<define name="MOTOR_DELAY" value="0.75" unit="seconds"/>
<define name="HEADING_DELAY" value="3.0" unit="seconds"/>
<define name="ACCELERATION_THRESHOLD" value="1.75"/>
<define name="INITIAL_PITCH" value="15.0" unit="deg"/>
<define name="INITIAL_THROTTLE" value="1.0"/>
</section>
<section name="GLS_APPROACH" prefix="APP_">
<define name="ANGLE" value="5" unit="deg"/>
<define name="INTERCEPT_AF_SD" value="10" unit="m"/>
<define name="TARGET_SPEED" value="13" unit="m/s"/>
</section>
<section name="DIGITAL_CAMERA" prefix="DC_">
<define name="AUTOSHOOT_PERIOD" value="1.5" unit="sec"/>
<define name="AUTOSHOOT_DISTANCE_INTERVAL" value="50" unit="meter"/>
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="JSBSIM_MODEL" value="Malolo1" type="string"/>
<define name="COMMANDS_NB" value="4"/>
<define name="ACTUATOR_NAMES" value="throttle-cmd-norm, aileron-cmd-norm, elevator-cmd-norm, rudder-cmd-norm" type="string[]"/>
<define name="JS_AXIS_MODE" value="4"/>
<define name="BYPASS_AHRS" value="TRUE"/>
<define name="BYPASS_INS" value="TRUE"/>
</section>
</airframe>