Files
paparazzi/conf/airframes/tudelft/bebop_OF_hover.xml
2019-01-28 15:44:22 +01:00

230 lines
8.9 KiB
XML

<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<airframe name="tudelft_tb_bebop">
<firmware name="rotorcraft">
<target name="ap" board="bebop"/>
<define name="USE_SONAR" value="FALSE" />
<module name="telemetry" type="transparent_udp"/>
<module name="radio_control" type="datalink"/>
<module name="motor_mixing"/>
<module name="actuators" type="bebop"/>
<module name="imu" type="bebop"/>
<module name="gps" type="datalink"/>
<module name="stabilization" type="indi_simple"/>
<module name="stabilization" type="rate_indi"/>
<module name="ahrs" type="int_cmpl_quat">
<configure name="USE_MAGNETOMETER" value="FALSE"/> <!-- TURN ON OUTSIDE -->
<define name="AHRS_USE_GPS_HEADING" value="TRUE"/>
</module>
<!--module name="ins" type="extended">
</module-->
<module name="ins" type="gps_passthrough"/>
<!-- module name="guidance" type="indi"/-->
<!-- <module name="guidance" type="indi"> <define name="GUIDANCE_INDI_SPECIFIC_FORCE_GAIN"
value="-500.0"/> <define name="GUIDANCE_INDI_THRUST_DYNAMICS" value="0.1"/>
<define name="GUIDANCE_INDI_RC_DEBUG" value="TRUE"/> </module> -->
<module name="bebop_cam"/>
<module name="pose_history"/>
<module name="cv_opticflow">
<define name="OPTICFLOW_METHOD" value="0"/>
<define name="OPTICFLOW_CAMERA" value="bottom_camera"/>
<define name="OPTICFLOW_SEARCH_DISTANCE" value="40"/>
</module>
<module name="optical_flow_hover" >
<define name="OFH_HOVER_METHOD" value = "1" />
<define name="OFH_MAXBANK" value = "10.f" />
<define name="XY_SYMMETRICAL" value = "1" />
<define name="OFH_OSCPHI" value = "1" />
<define name="OFH_OSCTHETA" value = "0" />
<define name="OF_LP_CONST" value = "0.4" />
<define name="COV_WINDOW_SIZE" value = "300" />
<define name="OFH_IGAINZ" value = "0.002" />
<define name="OFH_RAMPZ" value = "0.15" />
<define name="OFH_REDUCTIONZ" value = "0.45" />
<define name="OFH_COVDIV_SETPOINT" value = "-0.02" />
<define name="OFH_IGAINX" value = "0.00002" />
<define name="OFH_IGAINY" value = "0.00002" />
<define name="OFH_RAMPXY" value = "0.0008" />
<define name="OFH_REDUCTIONXY" value = "0.3" />
<define name="OFH_COVFLOW_SETPOINT" value = "-500.f" />
<define name="OFH_VER_SLOPE_A" value = "3.f" />
<define name="OFH_VER_SLOPE_B" value = "-0.5" />
<define name="OFH_HOR_X_SLOPE_A" value = "0.003" />
<define name="OFH_HOR_X_SLOPE_B" value = "0.005" />
</module>
</firmware>
<commands>
<axis name="PITCH" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="6000"/>
</commands>
<servos driver="Default">
<servo name="TOP_LEFT" no="0" min="3000" neutral="3000" max="9800"/>
<servo name="TOP_RIGHT" no="1" min="3000" neutral="3000" max="9800"/>
<servo name="BOTTOM_RIGHT" no="2" min="3000" neutral="3000" max="9800"/>
<servo name="BOTTOM_LEFT" no="3" min="3000" neutral="3000" max="9800"/>
</servos>
<section name="MIXING" prefix="MOTOR_MIXING_">
<define name="TYPE" value="QUAD_X"/>
</section>
<!--command_laws>
<set servo="TOP_LEFT" value="autopilot_motors_on ? actuators_pprz[0] : -MAX_PPRZ" />
<set servo="TOP_RIGHT" value="autopilot_motors_on ? actuators_pprz[1] : -MAX_PPRZ" />
<set servo="BOTTOM_RIGHT" value="autopilot_motors_on ? actuators_pprz[2] : -MAX_PPRZ" />
<set servo="BOTTOM_LEFT" value="autopilot_motors_on ? actuators_pprz[3] : -MAX_PPRZ" />
</command_laws-->
<command_laws>
<call fun="motor_mixing_run(autopilot_get_motors_on(),FALSE,values)"/>
<set servo="TOP_LEFT" value="motor_mixing.commands[MOTOR_FRONT_LEFT]"/>
<set servo="TOP_RIGHT" value="motor_mixing.commands[MOTOR_FRONT_RIGHT]"/>
<set servo="BOTTOM_RIGHT" value="motor_mixing.commands[MOTOR_BACK_RIGHT]"/>
<set servo="BOTTOM_LEFT" value="motor_mixing.commands[MOTOR_BACK_LEFT]"/>
</command_laws>
<section name="IMU" prefix="IMU_">
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
<!-- local magnetic field -->
<!-- http://wiki.paparazziuav.org/wiki/Subsystem/ahrs#Local_Magnetic_Field -->
<section name="AHRS" prefix="AHRS_">
<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
<define name="HEADING_UPDATE_GPS_MIN_SPEED" value="0"/>
<!-- For vibrating airframes -->
<define name="GRAVITY_HEURISTIC_FACTOR" value="0"/>
<!-- Delft -->
<define name="H_X" value="0.3892503"/>
<define name="H_Y" value="0.0017972"/>
<define name="H_Z" value="0.9211303"/>
</section>
<section name="INS" prefix="INS_">
<!-- define name="SONAR_MAX_RANGE" value="2.2"/>
<define name="SONAR_UPDATE_ON_AGL" value="TRUE"/-->
<!-- Optitrack -->
<define name="USE_GPS_ALT" value="1"/>
<define name="VFF_R_GPS" value="0.01"/>
</section>
<section name="RC_SETPOINT" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoint limits for attitude stabilization rc flight -->
<define name="SP_MAX_PHI" value="45" unit="deg"/>
<define name="SP_MAX_THETA" value="45" unit="deg"/>
<define name="SP_MAX_R" value="120" unit="deg/s"/>
<define name="DEADBAND_A" value="0"/>
<define name="DEADBAND_E" value="0"/>
<define name="DEADBAND_R" value="50"/>
</section>
<section name="ATTITUDE_REFERENCE" prefix="STABILIZATION_ATTITUDE_">
<!-- attitude reference generation model -->
<define name="REF_OMEGA_P" value="450" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="600." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_Q" value="450" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="600." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_R" value="450" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="600." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(8000.)"/>
</section>
<section name="STABILIZATION_ATTITUDE_INDI" prefix="STABILIZATION_INDI_">
<!-- control effectiveness -->
<define name="G1_P" value="0.030367"/>
<define name="G1_Q" value="0.023655"/>
<define name="G1_R" value="0.001005"/>
<define name="G2_R" value="0.10882"/>
<!-- reference acceleration for attitude control -->
<define name="REF_ERR_P" value="600.0"/>
<define name="REF_ERR_Q" value="600.0"/>
<define name="REF_ERR_R" value="600.0"/>
<define name="REF_RATE_P" value="28.0"/>
<define name="REF_RATE_Q" value="28.0"/>
<define name="REF_RATE_R" value="28.0"/>
<!--Maxium yaw rate, to avoid instability-->
<define name="MAX_R" value="120.0" unit="deg/s"/>
<!-- second order filter parameters -->
<define name="FILT_CUTOFF" value="8.0"/>
<define name="FILT_CUTOFF_R" value="8.0"/>
<!-- first order actuator dynamics -->
<define name="ACT_DYN_P" value="0.1"/>
<define name="ACT_DYN_Q" value="0.1"/>
<define name="ACT_DYN_R" value="0.1"/>
<!-- Adaptive Learning Rate -->
<define name="USE_ADAPTIVE" value="FALSE"/>
<define name="ADAPTIVE_MU" value="0.0001"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<!--define name="HOVER_KP" value="550"/-->
<define name="HOVER_KP" value="700"/>
<define name="HOVER_KD" value="300"/>
<define name="HOVER_KI" value="100"/> <!-- 13 -->
<define name="NOMINAL_HOVER_THROTTLE" value="0.715"/>
<define name="ADAPT_THROTTLE_ENABLED" value="FALSE"/>
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<!-- Good weather -->
<define name="MAX_BANK" value="20" unit="deg"/>
<!-- Bad weather -->
<!-- define name="MAX_BANK" value="32" unit="deg"/ -->
<define name="PGAIN" value="300"/>
<define name="DGAIN" value="350"/>
<define name="IGAIN" value="30"/>
<define name="REF_MAX_SPEED" value="0.5"/>
</section>
<section name="NAVIGATION" prefix="NAV_">
<define name="CLIMB_VSPEED" value="1.0"/>
<define name="DESCEND_VSPEED" value="-0.75"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_STARTUP" value="AP_MODE_NAV"/>
<define name="MODE_MANUAL" value="AP_MODE_MODULE"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_Z_HOLD"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
<define name="NO_RC_THRUST_LIMIT" value="TRUE"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="12700"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.6" unit="V"/>
<define name="CRITIC_BAT_LEVEL" value="9.9" unit="V"/>
<define name="LOW_BAT_LEVEL" value="10.4" unit="V"/>
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/>
</section>
</airframe>