mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-05-09 22:49:53 +08:00
Gautier Hattenberger
214 lines
7.8 KiB
XML
214 lines
7.8 KiB
XML
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<airframe name="swing">
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<firmware name="rotorcraft">
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<configure name="PREFIX" value="/opt/arm-2012.03/bin/arm-none-linux-gnueabi"/>
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<target name="ap" board="swing"/>
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<target name="nps" board="pc">
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<module name="fdm" type="jsbsim"/>
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</target>
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<!--define name="USE_SONAR" value="TRUE"/-->
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<module name="radio_control" type="datalink"/>
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<module name="telemetry" type="transparent_udp"/>
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<module name="motor_mixing"/>
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<module name="actuators" type="swing"/>
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<module name="imu" type="swing"/>
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<module name="gps" type="datalink"/>
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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"/>
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<module name="air_data"/>
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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="0"/>
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</commands>
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<servos>
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<servo name="BOTTOM_RIGHT" no="0" min="0" neutral="15" max="511"/>
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<servo name="TOP_RIGHT" no="1" min="0" neutral="15" max="511"/>
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<servo name="BOTTOM_LEFT" no="2" min="0" neutral="15" max="511"/>
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<servo name="TOP_LEFT" no="3" min="0" neutral="15" max="511"/>
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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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<define name="NB_MOTOR" value="4"/>
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<define name="SCALE" value="256"/>
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<define name="MAX_SATURATION_OFFSET" value="3*MAX_PPRZ"/>
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<!-- Time cross layout (X), with order NW (CW), NE (CCW), SE (CW), SW (CCW) -->
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<define name="ROLL_COEF" value="{ -81, -81, 81, 81}"/>
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<define name="PITCH_COEF" value="{ 243, -243, 243, -243}"/>
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<define name="YAW_COEF" value="{ 128, -128, -128, 128}"/>
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<define name="THRUST_COEF" value="{ 256, 256, 256, 256}"/>
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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="BOTTOM_RIGHT" value="motor_mixing.commands[0]"/>
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<set servo="TOP_RIGHT" value="motor_mixing.commands[1]"/>
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<set servo="BOTTOM_LEFT" value="motor_mixing.commands[2]"/>
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<set servo="TOP_LEFT" value="motor_mixing.commands[3]"/>
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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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<!-- 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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</section>
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<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
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<!-- setpoints -->
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<define name="SP_MAX_P" value="10000"/>
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<define name="SP_MAX_Q" value="10000"/>
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<define name="SP_MAX_R" value="10000"/>
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<define name="DEADBAND_P" value="20"/>
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<define name="DEADBAND_Q" value="20"/>
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<define name="DEADBAND_R" value="200"/>
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<define name="REF_TAU" value="4"/>
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<!-- feedback -->
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<define name="GAIN_P" value="400"/>
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<define name="GAIN_Q" value="400"/>
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<define name="GAIN_R" value="350"/>
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<define name="IGAIN_P" value="75"/>
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<define name="IGAIN_Q" value="75"/>
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<define name="IGAIN_R" value="50"/>
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<!-- feedforward -->
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<define name="DDGAIN_P" value="300"/>
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<define name="DDGAIN_Q" value="300"/>
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<define name="DDGAIN_R" value="300"/>
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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="650"/>
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<define name="PHI_DGAIN" value="300"/>
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<define name="PHI_IGAIN" value="0"/>
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<define name="THETA_PGAIN" value="650"/>
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<define name="THETA_DGAIN" value="300"/>
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<define name="THETA_IGAIN" value="0"/>
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<define name="PSI_PGAIN" value="300"/>
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<define name="PSI_DGAIN" value="250"/>
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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="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_KILL"/>
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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_DIRECT"/>
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<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_Z_HOLD"/>
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</section>
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<section name="BAT">
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<define name="CATASTROPHIC_BAT_LEVEL" value="3.1" unit="V"/>
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<define name="CRITIC_BAT_LEVEL" value="3.3" unit="V"/>
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<define name="LOW_BAT_LEVEL" value="3.5" unit="V"/>
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<define name="MAX_BAT_LEVEL" value="4.1" unit="V"/>
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</section>
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</airframe>
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