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<!DOCTYPE airframe SYSTEM "../airframe.dtd"> | ||
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<airframe name="bebop2_indi"> | ||
<description>Bebop2, Outdoor | ||
</description> | ||
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<firmware name="rotorcraft"> | ||
<target name="ap" board="bebop2"> | ||
<define name="INDI_RPM_FEEDBACK" value="TRUE"/> | ||
</target> | ||
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<target name="nps" board="pc"> | ||
<module name="fdm" type="jsbsim"/> | ||
<module name="udp"/> | ||
</target> | ||
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<module name="telemetry" type="transparent_udp"/> | ||
<module name="radio_control" type="datalink"/> | ||
<module name="actuators" type="bebop"/> | ||
<module name="imu" type="bebop"/> | ||
<module name="gps" type="ublox"/> | ||
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<module name="stabilization" type="indi"/> | ||
<module name="guidance" type="indi"> | ||
<define name="GUIDANCE_INDI_POS_GAIN" value="0.5"/> | ||
<define name="GUIDANCE_INDI_SPEED_GAIN" value="1.8"/> | ||
<define name="GUIDANCE_INDI_THRUST_DYNAMICS" value="0.06"/> | ||
</module> | ||
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<module name="ahrs" type="int_cmpl_quat"> | ||
<configure name="USE_MAGNETOMETER" value="TRUE"/> | ||
<define name="AHRS_USE_GPS_HEADING" value="FALSE"/> | ||
</module> | ||
<module name="ins" type="extended"/> | ||
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<module name="geo_mag"/> | ||
<module name="air_data"/> | ||
<module name="gps" type="ubx_ucenter"/> | ||
<module name="logger_file"> | ||
<define name="FILE_LOGGER_PATH" value="/data/ftp/internal_000"/> | ||
</module> | ||
</firmware> | ||
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<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> | ||
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<servos driver="Default"> | ||
<servo name="TOP_LEFT" no="0" min="2500" neutral="2500" max="12000"/> | ||
<servo name="TOP_RIGHT" no="1" min="2500" neutral="2500" max="12000"/> | ||
<servo name="BOTTOM_RIGHT" no="2" min="2500" neutral="2500" max="12000"/> | ||
<servo name="BOTTOM_LEFT" no="3" min="2500" neutral="2500" max="12000"/> | ||
</servos> | ||
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<command_laws> | ||
<set servo="TOP_LEFT" value="autopilot_get_motors_on() ? actuators_pprz[0] : -MAX_PPRZ"/> | ||
<set servo="TOP_RIGHT" value="autopilot_get_motors_on() ? actuators_pprz[1] : -MAX_PPRZ"/> | ||
<set servo="BOTTOM_RIGHT" value="autopilot_get_motors_on() ? actuators_pprz[2] : -MAX_PPRZ"/> | ||
<set servo="BOTTOM_LEFT" value="autopilot_get_motors_on() ? actuators_pprz[3] : -MAX_PPRZ"/> | ||
</command_laws> | ||
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<section name="AIR_DATA" prefix="AIR_DATA_"> | ||
<define name="CALC_AIRSPEED" value="FALSE"/> | ||
<define name="CALC_TAS_FACTOR" value="FALSE"/> | ||
<define name="CALC_AMSL_BARO" value="TRUE"/> | ||
</section> | ||
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<!-- Magnetometer still needs to be calibrated --> | ||
<section name="IMU" prefix="IMU_"> | ||
<define name="MAG_X_NEUTRAL" value="0"/> | ||
<define name="MAG_Y_NEUTRAL" value="0"/> | ||
<define name="MAG_Z_NEUTRAL" value="0"/> | ||
<define name="MAG_X_SENS" value="7.28514789391" integer="16"/> | ||
<define name="MAG_Y_SENS" value="7.33022132691" integer="16"/> | ||
<define name="MAG_Z_SENS" value="7.57102035692" integer="16"/> | ||
</section> | ||
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<!-- 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 --> | ||
<!-- Delft --> | ||
<define name="H_X" value="0.3892503"/> | ||
<define name="H_Y" value="0.0017972"/> | ||
<define name="H_Z" value="0.9211303"/> | ||
</section> | ||
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<section name="INS" prefix="INS_"> | ||
<define name="SONAR_MAX_RANGE" value="2.2"/> | ||
</section> | ||
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<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="300" unit="deg/s"/> | ||
<define name="DEADBAND_A" value="0"/> | ||
<define name="DEADBAND_E" value="0"/> | ||
<define name="DEADBAND_R" value="50"/> | ||
</section> | ||
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<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.)"/> | ||
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<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.)"/> | ||
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<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> | ||
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<section name="STABILIZATION_ATTITUDE_INDI" prefix="STABILIZATION_INDI_"> | ||
<!-- control effectiveness --> | ||
<define name="G1_ROLL" value="{16 , -16, -16, 16}"/> | ||
<define name="G1_PITCH" value="{12, 12, -12, -12}"/> | ||
<define name="G1_YAW" value="{ 0.8, -0.8, 0.8, -0.8}"/> | ||
<define name="G1_THRUST" value="{-.6, -.6, -.6, -.6}"/> | ||
<!--Counter torque effect of spinning up a rotor--> | ||
<define name="G2" value="{112, -112, 112, -112}"/> | ||
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<!-- reference acceleration for attitude control --> | ||
<define name="REF_ERR_P" value="320.0"/> | ||
<define name="REF_ERR_Q" value="320.0"/> | ||
<define name="REF_ERR_R" value="320.0"/> | ||
<define name="REF_RATE_P" value="16.0"/> | ||
<define name="REF_RATE_Q" value="16.0"/> | ||
<define name="REF_RATE_R" value="16.0"/> | ||
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<define name="ESTIMATION_FILT_CUTOFF" value="3.2"/> | ||
<define name="FILT_CUTOFF" value="3.2"/> | ||
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<!-- first order actuator dynamics --> | ||
<define name="ACT_DYN" value="{0.1, 0.1, 0.1, 0.1}"/> | ||
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<!-- Adaptive Learning Rate --> | ||
<define name="USE_ADAPTIVE" value="FALSE"/> | ||
<define name="ADAPTIVE_MU" value="0.0001"/> | ||
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<!--Priority for each axis (roll, pitch, yaw and thrust)--> | ||
<define name="WLS_PRIORITIES" value="{1000, 1000, 1, 100}"/> | ||
</section> | ||
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<section name="GUIDANCE_V" prefix="GUIDANCE_V_"> | ||
<define name="HOVER_KP" value="350"/> | ||
<define name="HOVER_KD" value="85"/> | ||
<define name="HOVER_KI" value="20"/> | ||
<define name="NOMINAL_HOVER_THROTTLE" value="0.655"/> | ||
<define name="ADAPT_THROTTLE_ENABLED" value="TRUE"/> | ||
</section> | ||
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<section name="GUIDANCE_H" prefix="GUIDANCE_H_"> | ||
<define name="REF_MAX_SPEED" value="8" unit="m/s"/> | ||
<define name="MAX_BANK" value="32" unit="deg"/> | ||
<define name="PGAIN" value="120"/> | ||
<define name="DGAIN" value="100"/> | ||
<define name="IGAIN" value="30"/> | ||
</section> | ||
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<section name="NAVIGATION" prefix="NAV_"> | ||
<define name="CLIMB_VSPEED" value="4.5"/> | ||
<define name="DESCEND_VSPEED" value="-1.0"/> | ||
</section> | ||
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<section name="SIMULATOR" prefix="NPS_"> | ||
<define name="ACTUATOR_NAMES" value="nw_motor, ne_motor, se_motor, sw_motor" type="string[]"/> | ||
<define name="JSBSIM_MODEL" value="bebop2" type="string"/> | ||
<define name="NO_MOTOR_MIXING" value="TRUE"/> | ||
</section> | ||
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<section name="AUTOPILOT"> | ||
<define name="MODE_STARTUP" value="AP_MODE_NAV"/> | ||
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/> | ||
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_Z_HOLD"/> | ||
<define name="MODE_AUTO2" value="AP_MODE_NAV"/> | ||
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<define name="NO_RC_THRUST_LIMIT" value="TRUE"/> | ||
</section> | ||
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<section name="BAT"> | ||
<define name="MILLIAMP_AT_FULL_THROTTLE" value="8700"/> | ||
<define name="CATASTROPHIC_BAT_LEVEL" value="9.9" unit="V"/> | ||
<define name="CRITIC_BAT_LEVEL" value="11.0" unit="V"/> | ||
<define name="LOW_BAT_LEVEL" value="11.1" unit="V"/> | ||
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/> | ||
</section> | ||
</airframe> |
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