mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-05-12 01:50:11 +08:00
Gautier Hattenberger
363dec8693
* [autopilot] refactor autopilot API for both firmwares With this, fixedwing and rotorcraft are mostly using the same interface for the autopilot. Some specific code and messages handling are still firmware dependent. A large part of the autopilot logic of the fixedwing is moved from main_ap to autopilot_static. More getter/setter functions are provided. * [autopilot] update the rest of the system and the conf for using the refactored autopilot API * [autopilot] fix some errors from CI servers * [actuators] use dummy actuators module to prevent autoloading * Rename Bart_heliDD_INDI.xml to tudelft_bs_helidd_indi.xml * Rename Bart_heliDD_pid.xml to tudelft_bs_helidd_pid.xml * Delete tudelft_course2016_bebop_colorfilter.xml * Delete tudelft_course2016_bebop_avoider.xml * [actuators] don't autoload actuators when set to 'none' * [gcs] autodetect firmware for strip mode button
190 lines
7.0 KiB
XML
190 lines
7.0 KiB
XML
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<!-- this is a quadrotor frame with the OpenPilot CC3D board:
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* Autopilot: OpenPilot CC3D https://www.openpilot.org/product/coptercontrol/
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-->
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<airframe name="QuadCC3D">
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<firmware name="rotorcraft">
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<target name="ap" board="cc3d">
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</target>
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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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<module name="radio_control" type="spektrum">
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<define name="RADIO_MODE" value="RADIO_AUX1"/>
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<define name="RADIO_KILL_SWITCH" value="RADIO_GEAR"/>
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</module>
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<module name="motor_mixing"/>
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<module name="actuators" type="pwm">
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<define name="SERVO_HZ" value="400"/>
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</module>
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<module name="telemetry" type="transparent"/>
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<module name="stabilization" type="int_quat"/>
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<module name="imu" type="mpu6000"/>
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<module name="ahrs" type="int_cmpl_quat">
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<define name="AHRS_GRAVITY_HEURISTIC_FACTOR" value="30"/>
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</module>
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<module name="ins"/>
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<!-- CC3D board does not have a mag -->
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<configure name="USE_MAGNETOMETER" value="FALSE"/>
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<!-- compress trig tables so it fits in board -->
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<define name="PPRZ_TRIG_INT_COMPR_FLASH"/>
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<define name="PPRZ_TRIG_INT_COMPR_LOW"/>
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</firmware>
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<firmware name="test_progs">
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<target name="test_sys_time_timer" board="cc3d"/>
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<target name="test_sys_time_usleep" board="cc3d"/>
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<target name="test_telemetry" board="cc3d"/>
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<target name="test_imu" board="cc3d">
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<module name="imu" type="mpu6000"/>
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</target>
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<target name="test_ahrs" board="cc3d">
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<module name="imu" type="mpu6000"/>
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<module name="ahrs" type="int_cmpl_quat"/>
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<configure name="USE_MAGNETOMETER" value="FALSE"/>
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</target>
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<target name="test_actuators_pwm" board="cc3d"/>
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</firmware>
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<servos driver="Pwm">
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<servo name="FL" no="0" min="1000" neutral="1100" max="2000"/>
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<servo name="FR" no="1" min="1000" neutral="1100" max="2000"/>
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<servo name="BR" no="2" min="1000" neutral="1100" max="2000"/>
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<servo name="BL" no="3" min="1000" neutral="1100" max="2000"/>
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</servos>
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<section name="MIXING" prefix="MOTOR_MIXING_">
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<!-- front left (CW), front right (CCW), back right (CW), back left (CCW) -->
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<define name="TYPE" value="QUAD_X"/>
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</section>
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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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<command_laws>
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<call fun="motor_mixing_run(autopilot_get_motors_on(),FALSE,values)"/>
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<set servo="FL" value="motor_mixing.commands[MOTOR_FRONT_LEFT]"/>
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<set servo="FR" value="motor_mixing.commands[MOTOR_FRONT_RIGHT]"/>
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<set servo="BR" value="motor_mixing.commands[MOTOR_BACK_RIGHT]"/>
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<set servo="BL" 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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<define name="MAG_X_NEUTRAL" value="22"/>
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<define name="MAG_Y_NEUTRAL" value="-314"/>
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<define name="MAG_Z_NEUTRAL" value="13"/>
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<define name="MAG_X_SENS" value="3.68160078446" integer="16"/>
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<define name="MAG_Y_SENS" value="3.6093630842" integer="16"/>
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<define name="MAG_Z_SENS" value="3.48306842466" integer="16"/>
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<define name="BODY_TO_IMU_PHI" value="180." 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="-90." unit="deg"/>
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</section>
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<section name="AHRS" prefix="AHRS_">
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<define name="H_X" value="0.3770441"/>
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<define name="H_Y" value="0.0193986"/>
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<define name="H_Z" value="0.9259921"/>
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</section>
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<section name="INS" prefix="INS_">
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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="60." unit="deg"/>
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<define name="SP_MAX_THETA" value="60." unit="deg"/>
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<define name="SP_MAX_R" value="90." 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="400" unit="deg/s"/>
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<define name="REF_ZETA_P" value="0.85"/>
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<define name="REF_MAX_P" value="400." 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="400" unit="deg/s"/>
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<define name="REF_ZETA_Q" value="0.85"/>
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<define name="REF_MAX_Q" value="400." 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="250" unit="deg/s"/>
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<define name="REF_ZETA_R" value="0.85"/>
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<define name="REF_MAX_R" value="180." unit="deg/s"/>
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<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
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<!-- feedback -->
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<define name="PHI_PGAIN" value="1000"/>
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<define name="PHI_DGAIN" value="400"/>
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<define name="PHI_IGAIN" value="200"/>
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<define name="THETA_PGAIN" value="1000"/>
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<define name="THETA_DGAIN" value="400"/>
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<define name="THETA_IGAIN" value="200"/>
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<define name="PSI_PGAIN" value="500"/>
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<define name="PSI_DGAIN" value="300"/>
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<define name="PSI_IGAIN" value="10"/>
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<!-- feedforward -->
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<define name="PHI_DDGAIN" value="300"/>
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<define name="THETA_DDGAIN" value="300"/>
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<define name="PSI_DDGAIN" value="300"/>
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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="150"/>
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<define name="HOVER_KD" value="80"/>
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<define name="HOVER_KI" value="20"/>
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<define name="NOMINAL_HOVER_THROTTLE" value="0.5"/>
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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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<define name="APPROX_FORCE_BY_THRUST" value="TRUE"/>
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<define name="MAX_BANK" value="30" unit="deg"/>
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<define name="USE_SPEED_REF" value="TRUE"/>
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<define name="PGAIN" value="50"/>
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<define name="DGAIN" value="100"/>
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<define name="AGAIN" value="70"/>
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<define name="IGAIN" value="20"/>
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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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<!-- mode switch on joystick channel 5 (axis numbering starting at zero) -->
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<define name="JS_AXIS_MODE" value="4"/>
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</section>
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<section name="AUTOPILOT">
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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="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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