mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-05-09 22:49:53 +08:00
Tom van Dijk
cfabb51eed
* Add gazebo model for Parrot Bebop 1 * Add first-order high pass filter * First implementation of actuator dynamics and spinup torque Flies ok with PID control Does not fly ok with INDI, the required G1 R is 0.159 instead of 0.0022 (estimated by flying in adaptive mode). The other parameters are close to those specified in the airframe file. * FIX incorrect yaw behavior Fixed two bugs: 1. gazebo_actuators.torques was set to NPS_ACTUATOR_THRUSTS 2. spinup torque direction is now also controlled by motor mixing * Clean up debug code and file logger * Clean up gazebo example airframes * Minor cleanup * FIX warnings about missing initializer in fdm_gazebo * Update documentation * Remove modules section, move to firmware * Minor fixes to fdm_gazebo and high_pass_filter * Move actuator dynamics to included airframe files Should prevent duplicate actuator defines spread accross all airframe files. * Fix FILTER_ROLL_RATE in bebop2_indi airframe Moved to firmware targets so it will be disabled in gazebo. Is this actually working in jsbsim?? * Update documentation * Fix newlines * Minor fixes in nps_fdm_gazebo.cpp * Re-enable filter roll rate Caution: causes oscillations around roll axis in gazebo * Disable roll filter and cleanup
214 lines
8.0 KiB
XML
214 lines
8.0 KiB
XML
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<airframe name="ardrone2">
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<firmware name="rotorcraft">
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<target name="ap" board="ardrone2"/>
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<target name="nps" board="pc">
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<module name="fdm" type="gazebo"/>
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</target>
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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="ardrone2"/>
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<module name="imu" type="ardrone2"/>
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<!-- gps: "ublox" or change to "sirf" for usage with parrot flight recorder -->
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<module name="gps" type="ublox"/>
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<module name="stabilization" type="int_quat"/>
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<module name="ahrs" type="int_cmpl_quat"/>
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<module name="ins" type="extended"/>
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<module name="bat_voltage_ardrone2"/>
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<module name="send_imu_mag_current"/>
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<module name="air_data"/>
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<module name="geo_mag"/>
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<module name="video_thread"/>
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<module name="cv_opticflow">
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<define name="OPTICFLOW_CAMERA" value="bottom_camera"/>
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<define name="OPTICFLOW_DEROTATION_CORRECTION_FACTOR_X" value="0.8"/> <!--Obtained from a linefit-->
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<define name="OPTICFLOW_DEROTATION_CORRECTION_FACTOR_Y" value="0.85"/> <!--Obtained from a linefit-->
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<!-- ARDrone2 FPS improvements - Remaining in sync with real life-->
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<define name="OPTICFLOW_PYRAMID_LEVEL" value="0"/>
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<define name="OPTICFLOW_FEATURE_MANAGEMENT" value="1"/>
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</module>
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<module name="cv_colorfilter">
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<define name="COLORFILTER_CAMERA" value="front_camera"/>
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<!--define name="COLORFILTER_SEND_OBSTACLE" value="TRUE"/--> <!-- If you want to test out the guided flightplan, uncomment this define-->
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</module>
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<module name="video_rtp_stream">
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<define name="VIEWVIDEO_CAMERA" value="front_camera"/>
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<define name="VIEWVIDEO_DOWNSIZE_FACTOR" value="4"/>
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<define name="VIEWVIDEO_QUALITY_FACTOR" value="60"/>
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</module>
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</firmware>
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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="3000"/>
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</commands>
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<servos driver="Default">
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<servo name="TOP_LEFT" no="0" min="0" neutral="1" max="500"/>
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<servo name="TOP_RIGHT" no="1" min="0" neutral="1" max="500"/>
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<servo name="BOTTOM_RIGHT" no="2" min="0" neutral="1" max="500"/>
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<servo name="BOTTOM_LEFT" no="3" min="0" neutral="1" max="500"/>
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</servos>
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<section name="MIXING" prefix="MOTOR_MIXING_">
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<define name="TRIM_ROLL" value="0"/>
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<define name="TRIM_PITCH" value="0"/>
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<define name="TRIM_YAW" value="0"/>
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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="IMU" prefix="IMU_">
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<!-- Accelero -->
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<define name="ACCEL_X_NEUTRAL" value="2048"/>
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<define name="ACCEL_Y_NEUTRAL" value="2048"/>
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<define name="ACCEL_Z_NEUTRAL" value="2048"/>
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<!-- Magneto calibration -->
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<define name="MAG_X_NEUTRAL" value="0"/>
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<define name="MAG_Y_NEUTRAL" value="0"/>
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<define name="MAG_Z_NEUTRAL" value="-180"/>
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<define name="MAG_X_SENS" value="16." integer="16"/>
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<define name="MAG_Y_SENS" value="16." integer="16"/>
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<define name="MAG_Z_SENS" value="16." 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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<!-- Toulouse -->
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<define name="H_X" value="0.513081"/>
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<define name="H_Y" value="-0.00242783"/>
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<define name="H_Z" value="0.858336"/>
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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="600" 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="250"/>
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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="200" 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="300." unit="deg/s"/>
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<define name="REF_MAX_RDOT" value="RadOfDeg(4000.)"/>
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<!-- feedback -->
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<define name="PHI_PGAIN" value="850"/>
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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="850"/>
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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="1000"/>
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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="100"/>
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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="460"/>
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<define name="HOVER_KD" value="160"/>
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<define name="HOVER_KI" value="26"/>
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<define name="NOMINAL_HOVER_THROTTLE" value="0.655"/>
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<define name="ADAPT_THROTTLE_ENABLED" value="FALSE"/>
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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="160"/>
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<define name="DGAIN" value="200"/>
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<define name="IGAIN" value="60"/>
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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_ardrone2" type="string"/>
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<define name="SENSORS_PARAMS" value="nps_sensors_params_ardrone2.h" type="string"/>
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</section>
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<include href="conf/simulator/gazebo/airframes/ardrone2.xml"/>
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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="9.7" 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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