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[bebop2] add example ac for usb cdc
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@martinmm
martinmm committed Mar 2, 2017
1 parent c8f657b commit c062dae
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0 conf/airframes/mm/bebop.xml → conf/airframes/MM/bebop.xml
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262 changes: 262 additions & 0 deletions conf/airframes/MM/bebop2_lum1_xbee.xml
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<!DOCTYPE airframe SYSTEM "../airframe.dtd">

<!-- no dampers -->
<airframe name="bebop2_lum1_xbee">

<firmware name="rotorcraft">
<target name="ap" board="bebop2"/>

<target name="nps" board="pc">
<module name="fdm" type="jsbsim"/>
<module name="udp"/>
</target>

<define name="UART4_DEV" value="/dev/ttyACM0"/>
<define name="UART5_DEV" value="/dev/ttyACM1"/>

<define name="SENSOR_SYNC_SEND"/>
<define name="IMU_TEMP_CTRL_DEBUG"/>

<module name="telemetry" type="xbee_api">
<configure name="MODEM_PORT" value="UART4"/>
<configure name="MODEM_BAUD" value="B57600"/>
</module>

<!--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="ublox"/>
<module name="stabilization" type="indi_simple"/>
<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"/>
</firmware>

<modules main_freq="512">
<!--module name="wind_estimator"/-->
<module name="geo_mag"/>
<module name="air_data"/>
<module name="send_imu_mag_current"/>
<module name="gps" type="ubx_ucenter"/>
<module name="logger_file">
<define name="FILE_LOGGER_PATH" value="/data/ftp/internal_000"/>
</module>
<module name="humid_sht_uart">
<configure name="SHT_UART" value="UART5"/>
</module>
<module name="imu_temp_ctrl"/>
</modules>

<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="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>

<section name="MIXING" prefix="MOTOR_MIXING_">
<define name="TRIM_ROLL" value="0"/>
<define name="TRIM_PITCH" value="0"/>
<define name="TRIM_YAW" value="0"/>
<define name="REVERSE" value="TRUE"/>
<define name="TYPE" value="QUAD_X"/>
</section>

<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="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>

<section name="IMU" prefix="IMU_">
<!-- Magnetometer still needs to be calibrated -->

<!--red LM/-->
<define name="MAG_X_NEUTRAL" value="-12"/>
<define name="MAG_Y_NEUTRAL" value="123"/>
<define name="MAG_Z_NEUTRAL" value="239"/>
<define name="MAG_X_SENS" value="6.56662079024" integer="16"/>
<define name="MAG_Y_SENS" value="6.56528562457" integer="16"/>
<define name="MAG_Z_SENS" value="6.89245853894" integer="16"/>

<define name= "MAG_X_CURRENT_COEF" value="0.00349278666278"/>
<define name= "MAG_Y_CURRENT_COEF" value="-0.00294581023579"/>
<define name= "MAG_Z_CURRENT_COEF" value="0.00744261463196"/>

</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 -->
<!-- Toulouse -->
<!--define name="H_X" value="0.513081"/>
<define name="H_Y" value="-0.00242783"/>
<define name="H_Z" value="0.858336"/-->
<!-- Delft -->
<!--define name="H_X" value="0.3892503"/>
<define name="H_Y" value="0.0017972"/>
<define name="H_Z" value="0.9211303"/-->
<!-- Gross Lobke -->
<!--define name="H_X" value="0.382151"/>
<define name="H_Y" value="0.01674"/>
<define name="H_Z" value="0.923948"/-->
<!-- Longyearbyen -->
<!--define name="H_X" value="0.133047"/>
<define name="H_Y" value="0.019769"/>
<define name="H_Z" value="0.990913"/-->
<!-- Andenes HAF -->
<!--define name="H_X" value="0.20751"/>
<define name="H_Y" value="-0.0244116"/>
<define name="H_Z" value="0.977928"/-->

<!-- Hailuoto -->
<define name="H_X" value="0.236568"/>
<define name="H_Y" value="0.0424621"/>
<define name="H_Z" value="0.970687"/>
</section>

<section name="INS" prefix="INS_">
<define name="SONAR_MAX_RANGE" value="2.2"/>
<define name="SONAR_UPDATE_ON_AGL" value="TRUE"/>
</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="300" 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="0.05"/>
<define name="G1_Q" value="0.04"/>
<define name="G1_R" value="0.0022"/>
<define name="G2_R" value="0.20"/>

<!-- Here it is assumed that your removed the damping from your bebop2!
The dampers do not really damp, but cause oscillation. By removing/
fixing them, the bebop2 will fly much better-->
<define name="FILTER_ROLL_RATE" value="FALSE"/>
<define name="FILTER_PITCH_RATE" value="FALSE"/>
<define name="FILTER_YAW_RATE" value="FALSE"/>

<!-- 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"/>

<!-- second order filter parameters -->
<define name="FILT_OMEGA" value="20.0"/>
<define name="FILT_ZETA" value="0.7"/>
<define name="FILT_OMEGA_R" value="20.0"/>
<define name="FILT_ZETA_R" value="0.7"/>

<!-- second order filter parameters -->
<define name="FILT_CUTOFF" value="3.2"/>
<define name="FILT_CUTOFF_R" value="3.2"/>

<!-- first order actuator dynamics -->
<define name="ACT_DYN_P" value="0.06"/>
<define name="ACT_DYN_Q" value="0.06"/>
<define name="ACT_DYN_R" value="0.06"/>

<!-- 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="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>

<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="REF_MAX_SPEED" value="2" unit="m/s"/>
<define name="MAX_BANK" value="32" unit="deg"/>
<define name="PGAIN" value="60"/>
<define name="DGAIN" value="170"/>
<define name="IGAIN" value="30"/>
</section>

<section name="NAVIGATION" prefix="NAV_">
<define name="CLIMB_VSPEED" value="4.5"/>
<define name="DESCEND_VSPEED" value="-1.0"/>
</section>

<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="simple_x_quad_ccw" type="string"/>
<define name="SENSORS_PARAMS" value="nps_sensors_params_default.h" type="string"/>
</section>

<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_RC_CLIMB"/>
<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="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>

<section name="GCS">
<define name="AC_ICON" value="quadrotor_xi"/>
</section>
</airframe>

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