mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-05-10 06:59:54 +08:00
Gautier Hattenberger
363dec8693
* [autopilot] refactor autopilot API for both firmwares With this, fixedwing and rotorcraft are mostly using the same interface for the autopilot. Some specific code and messages handling are still firmware dependent. A large part of the autopilot logic of the fixedwing is moved from main_ap to autopilot_static. More getter/setter functions are provided. * [autopilot] update the rest of the system and the conf for using the refactored autopilot API * [autopilot] fix some errors from CI servers * [actuators] use dummy actuators module to prevent autoloading * Rename Bart_heliDD_INDI.xml to tudelft_bs_helidd_indi.xml * Rename Bart_heliDD_pid.xml to tudelft_bs_helidd_pid.xml * Delete tudelft_course2016_bebop_colorfilter.xml * Delete tudelft_course2016_bebop_avoider.xml * [actuators] don't autoload actuators when set to 'none' * [gcs] autodetect firmware for strip mode button
215 lines
7.8 KiB
XML
215 lines
7.8 KiB
XML
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<airframe name="bebop">
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<firmware name="rotorcraft">
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<target name="ap" board="bebop"/>
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<target name="nps" board="pc">
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<module name="fdm" type="jsbsim"/>
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<module name="udp"/>
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</target>
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<define name="MT9F002_OUTPUT_HEIGHT" value="640" />
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<define name="MT9F002_OUTPUT_WIDTH" value="640" />
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<define name="MT9F002_TARGET_EXPOSURE" value="30" />
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<define name="MT9F002_GAIN_GREEN1" value="4"/>
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<define name="MT9F002_GAIN_GREEN2" value="4"/>
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<define name="MT9F002_GAIN_RED" value="5"/>
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<define name="MT9F002_GAIN_BLUE" value="5"/>
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<define name="MT9F002_OUTPUT_SCALER" value="0.25"/>
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<define name="MT9F002_X_ODD_INC_VAL" value="1"/>
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<define name="MT9F002_Y_ODD_INC_VAL" value="1"/>
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<!--define name="USE_SONAR" value="TRUE"/-->
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<!-- Subsystem section -->
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<module name="telemetry" type="transparent_udp"/>
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<module name="radio_control" type="datalink"/>
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<module name="motor_mixing"/>
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<module name="actuators" type="bebop"/>
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<module name="imu" type="bebop"/>
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<module name="gps" type="furuno"/>
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<module name="stabilization" type="int_quat"/>
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<module name="ahrs" type="float_mlkf"/>
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<module name="ins" type="extended"/>
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</firmware>
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<modules main_freq="512">
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<module name="geo_mag"/>
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<module name="air_data"/>
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<module name="send_imu_mag_current"/>
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<!--module name="logger_file">
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<define name="FILE_LOGGER_PATH" value="/data/ftp/internal_000"/>
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</module-->
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<module name="video_thread"/>
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<module name="video_rtp_stream">
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<define name="VIEWVIDEO_CAMERA" value="bottom_camera"/>
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<define name="VIEWVIDEO_CAMERA2" value="front_camera"/>
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<define name="VIEWVIDEO_DOWNSIZE_FACTOR" value="2"/>
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<define name="VIEWVIDEO_QUALITY_FACTOR" value="40"/>
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</module>
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<module name="bebop_ae_awb"/>
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</modules>
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<commands>
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<axis name="PITCH" failsafe_value="0"/>
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<axis name="ROLL" failsafe_value="0"/>
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<axis name="YAW" failsafe_value="0"/>
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<axis name="THRUST" failsafe_value="6000"/>
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</commands>
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<servos driver="Default">
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<servo name="TOP_LEFT" no="0" min="3000" neutral="3000" max="12000"/>
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<servo name="TOP_RIGHT" no="1" min="3000" neutral="3000" max="12000"/>
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<servo name="BOTTOM_RIGHT" no="2" min="3000" neutral="3000" max="12000"/>
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<servo name="BOTTOM_LEFT" no="3" min="3000" neutral="3000" max="12000"/>
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</servos>
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<section name="MIXING" prefix="MOTOR_MIXING_">
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<!-- Time cross layout (X), with order NW (CW), NE (CCW), SE (CW), SW (CCW) -->
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<define name="TYPE" value="QUAD_X"/>
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</section>
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<command_laws>
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<call fun="motor_mixing_run(autopilot_get_motors_on(),FALSE,values)"/>
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<set servo="TOP_LEFT" value="motor_mixing.commands[MOTOR_FRONT_LEFT]"/>
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<set servo="TOP_RIGHT" value="motor_mixing.commands[MOTOR_FRONT_RIGHT]"/>
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<set servo="BOTTOM_RIGHT" value="motor_mixing.commands[MOTOR_BACK_RIGHT]"/>
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<set servo="BOTTOM_LEFT" value="motor_mixing.commands[MOTOR_BACK_LEFT]"/>
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</command_laws>
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<section name="AIR_DATA" prefix="AIR_DATA_">
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<define name="CALC_AIRSPEED" value="FALSE"/>
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<define name="CALC_TAS_FACTOR" value="FALSE"/>
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<define name="CALC_AMSL_BARO" value="TRUE"/>
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</section>
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<section name="IMU" prefix="IMU_">
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<!-- Magneto calibration -->
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<define name="MAG_X_NEUTRAL" value="18"/>
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<define name="MAG_Y_NEUTRAL" value="157"/>
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<define name="MAG_Z_NEUTRAL" value="49"/>
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<define name="MAG_X_SENS" value="10.5007722373" integer="16"/>
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<define name="MAG_Y_SENS" value="11.1147400462" integer="16"/>
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<define name="MAG_Z_SENS" value="11.6479371722" integer="16"/>
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<!-- Magneto current calibration -->
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<define name="MAG_X_CURRENT_COEF" value="0.0"/>
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<define name="MAG_Y_CURRENT_COEF" value="0.0"/>
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<define name="MAG_Z_CURRENT_COEF" value="0.0"/>
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<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
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<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
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<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
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</section>
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<!-- local magnetic field -->
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<!-- http://wiki.paparazziuav.org/wiki/Subsystem/ahrs#Local_Magnetic_Field -->
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<section name="AHRS" prefix="AHRS_">
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<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
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<!-- Delft -->
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<define name="H_X" value="0.3892503"/>
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<define name="H_Y" value="0.0017972"/>
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<define name="H_Z" value="0.9211303"/>
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</section>
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<section name="INS" prefix="INS_">
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<define name="SONAR_MAX_RANGE" value="2.2"/>
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<define name="SONAR_UPDATE_ON_AGL" value="TRUE"/>
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</section>
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<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
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<!-- setpoints -->
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<define name="SP_MAX_PHI" value="45" unit="deg"/>
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<define name="SP_MAX_THETA" value="45" unit="deg"/>
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<define name="SP_MAX_R" value="300" unit="deg/s"/>
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<define name="DEADBAND_A" value="0"/>
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<define name="DEADBAND_E" value="0"/>
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<define name="DEADBAND_R" value="50"/>
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<!-- reference -->
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<define name="REF_OMEGA_P" value="450" unit="deg/s"/>
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<define name="REF_ZETA_P" value="0.9"/>
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<define name="REF_MAX_P" value="600." unit="deg/s"/>
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<define name="REF_MAX_PDOT" value="RadOfDeg(8000.)"/>
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<define name="REF_OMEGA_Q" value="450" unit="deg/s"/>
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<define name="REF_ZETA_Q" value="0.9"/>
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<define name="REF_MAX_Q" value="600." unit="deg/s"/>
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<define name="REF_MAX_QDOT" value="RadOfDeg(8000.)"/>
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<define name="REF_OMEGA_R" value="450" unit="deg/s"/>
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<define name="REF_ZETA_R" value="0.9"/>
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<define name="REF_MAX_R" value="600." unit="deg/s"/>
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<define name="REF_MAX_RDOT" value="RadOfDeg(8000.)"/>
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<!-- feedback -->
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<define name="PHI_PGAIN" value="920"/>
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<define name="PHI_DGAIN" value="425"/>
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<define name="PHI_IGAIN" value="0"/>
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<define name="THETA_PGAIN" value="920"/>
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<define name="THETA_DGAIN" value="425"/>
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<define name="THETA_IGAIN" value="0"/>
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<define name="PSI_PGAIN" value="8000"/>
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<define name="PSI_DGAIN" value="700"/>
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<define name="PSI_IGAIN" value="0"/>
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<!-- feedforward -->
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<define name="PHI_DDGAIN" value="0"/>
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<define name="THETA_DDGAIN" value="0"/>
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<define name="PSI_DDGAIN" value="0"/>
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</section>
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<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
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<define name="HOVER_KP" value="283"/>
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<define name="HOVER_KD" value="82"/>
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<define name="HOVER_KI" value="13"/>
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<define name="NOMINAL_HOVER_THROTTLE" value="0.655"/>
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<define name="ADAPT_THROTTLE_ENABLED" value="TRUE"/>
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</section>
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<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
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<!-- Good weather -->
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<define name="MAX_BANK" value="20" unit="deg"/>
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<!-- Bad weather -->
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<!-- define name="MAX_BANK" value="32" unit="deg"/ -->
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<define name="PGAIN" value="79"/>
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<define name="DGAIN" value="100"/>
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<define name="IGAIN" value="30"/>
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</section>
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<section name="NAVIGATION" prefix="NAV_">
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<define name="CLIMB_VSPEED" value="2.5" />
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<define name="DESCEND_VSPEED" value="-1.0" />
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</section>
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<section name="SIMULATOR" prefix="NPS_">
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<define name="ACTUATOR_NAMES" value="nw_motor, ne_motor, se_motor, sw_motor" type="string[]"/>
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<define name="JSBSIM_MODEL" value="simple_x_quad_ccw" type="string"/>
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<define name="SENSORS_PARAMS" value="nps_sensors_params_default.h" type="string"/>
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</section>
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<section name="AUTOPILOT">
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<define name="MODE_STARTUP" value="AP_MODE_NAV"/>
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<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
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<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_Z_HOLD"/>
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<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
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</section>
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<section name="BAT">
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<define name="MILLIAMP_AT_FULL_THROTTLE" value="8700"/>
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<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
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<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/>
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<define name="LOW_BAT_LEVEL" value="10.6" unit="V"/>
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<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/>
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</section>
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</airframe>
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