/
qmk1.xml
242 lines (201 loc) · 9.2 KB
/
qmk1.xml
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<!-- this is a mikrokopter frame equiped with Lisa/L and mikrokopter controllers -->
<airframe name="qmk1">
<servos>
<servo name="FRONT" no="0" min="0" neutral="0" max="255"/>
<servo name="BACK" no="1" min="0" neutral="0" max="255"/>
<servo name="RIGHT" no="2" min="0" neutral="0" max="255"/>
<servo name="LEFT" no="3" min="0" neutral="0" max="255"/>
</servos>
<commands>
<axis name="PITCH" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="0"/>
</commands>
<section name="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4"/>
<define name="ADDR" value="{ 0x52, 0x54, 0x58, 0x56 }"/>
</section>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="3"/>
<define name="MAX_MOTOR" value="200"/>
<define name="TRIM_A" value="0"/>
<define name="TRIM_E" value="0"/>
<define name="TRIM_R" value="0"/>
<define name="NB_MOTOR" value="4"/>
<define name="SCALE" value="256"/>
<define name="ROLL_COEF" value="{ 0 , 0, 256, -256 }"/>
<define name="PITCH_COEF" value="{ 256, -256, 0, 0 }"/>
<define name="YAW_COEF" value="{ -256, -256, 256, 256 }"/>
<define name="THRUST_COEF" value="{ 256, 256, 256, 256 }"/>
</section>
<section name="IMU" prefix="IMU_">
<define name="GYRO_P_NEUTRAL" value="32858"/>
<define name="GYRO_Q_NEUTRAL" value="33152"/>
<define name="GYRO_R_NEUTRAL" value="31779"/>
<define name="GYRO_P_SENS" value=" 1.101357422" integer="16"/>
<define name="GYRO_Q_SENS" value=" 1.122670898" integer="16"/>
<define name="GYRO_R_SENS" value=" 1.104890137" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="32907"/>
<define name="ACCEL_Y_NEUTRAL" value="33046"/>
<define name="ACCEL_Z_NEUTRAL" value="32830"/>
<define name="ACCEL_X_SENS" value="2.57332012257" integer="16"/>
<define name="ACCEL_Y_SENS" value="2.56968772349" integer="16"/>
<define name="ACCEL_Z_SENS" value="2.56894625325" integer="16"/>
<define name="MAG_X_NEUTRAL" value="58"/>
<define name="MAG_Y_NEUTRAL" value="92"/>
<define name="MAG_Z_NEUTRAL" value="-3"/>
<define name="MAG_X_SENS" value="4.70018395734" integer="16"/>
<define name="MAG_Y_SENS" value="4.884119848" integer="16"/>
<define name="MAG_Z_SENS" value="2.59926404993" integer="16"/>
<!-- old calibration
<define name="MAG_X_NEUTRAL" value="30"/>
<define name="MAG_Y_NEUTRAL" value="80"/>
<define name="MAG_Z_NEUTRAL" value="19"/>
<define name="MAG_X_SENS" value="4.73590916868" integer="16"/>
<define name="MAG_Y_SENS" value="4.86013203775" integer="16"/>
<define name="MAG_Z_SENS" value="2.5947951512" integer="16"/>
-->
<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="45." unit="deg"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_Z_HOLD"/>
</section>
<section name="BAT">
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
</section>
<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
<define name="SP_MAX_P" value="10000"/>
<define name="SP_MAX_Q" value="10000"/>
<define name="SP_MAX_R" value="10000"/>
<define name="GAIN_P" value="400"/>
<define name="GAIN_Q" value="400"/>
<define name="GAIN_R" value="350"/>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="2000"/>
<define name="PHI_DGAIN" value="400"/>
<define name="PHI_IGAIN" value="200"/>
<define name="THETA_PGAIN" value="2000"/>
<define name="THETA_DGAIN" value="400"/>
<define name="THETA_IGAIN" value="400"/>
<define name="PSI_PGAIN" value="1000"/>
<define name="PSI_DGAIN" value="350"/>
<define name="PSI_IGAIN" value="10"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value=" 300"/>
<define name="THETA_DDGAIN" value=" 300"/>
<define name="PSI_DDGAIN" value=" 300"/>
</section>
<section name="INS" prefix="INS_">
<!-- <define name="BARO_SENS" value="15." integer="16"/> -->
<define name="BARO_SENS" value="10." integer="16"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<define name="MIN_ERR_Z" value="POS_BFP_OF_REAL(-10.)"/>
<define name="MAX_ERR_Z" value="POS_BFP_OF_REAL( 10.)"/>
<define name="MIN_ERR_ZD" value="SPEED_BFP_OF_REAL(-10.)"/>
<define name="MAX_ERR_ZD" value="SPEED_BFP_OF_REAL( 10.)"/>
<define name="MAX_SUM_ERR" value="2000000"/>
<define name="HOVER_KP" value="500"/>
<define name="HOVER_KD" value="200"/>
<define name="HOVER_KI" value="0"/>
<!-- 1.5m/s for full stick : BOOZ_SPEED_I_OF_F(1.5) / (MAX_PPRZ/2) -->
<define name="RC_CLIMB_COEF" value ="163"/>
<!-- BOOZ_SPEED_I_OF_F(1.5) * 20% -->
<define name="RC_CLIMB_DEAD_BAND" value ="160000"/>
<!--define name="INV_M" value ="0.2"/-->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="PGAIN" value="100"/>
<define name="DGAIN" value="100"/>
<define name="IGAIN" value="0"/>
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="{"front_motor", "back_motor", "right_motor", "left_motor"}"/>
<define name="INITIAL_CONDITITONS" value=""reset00""/>
<define name="SENSORS_PARAMS" value=""nps_sensors_params_booz2_a1.h""/>
</section>
<!-- -->
<modules main_freq="512">
<load name="vehicle_interface_overo_link.xml"/>
</modules>
<!-- -->
<firmware name="rotorcraft">
<target name="ap" board="lisa_l_1.0">
<!-- <define name="ACTUATORS_START_DELAY" value="1"/> -->
<subsystem name="radio_control" type="ppm"/>
<subsystem name="actuators" type="mkk"/>
</target>
<target name="nps" board="pc">
<subsystem name="fdm" type="nps"/>
<subsystem name="radio_control" type="ppm"/>
<subsystem name="actuators" type="mkk"/>
</target>
<subsystem name="telemetry" type="transparent"/>
<subsystem name="imu" type="b2_v1.1"/>
<subsystem name="gps" type="ublox">
<configure name="GPS_PORT" value="UART3"/>
</subsystem>
<subsystem name="stabilization" type="euler"/>
<subsystem name="ahrs" type="int_cmpl_euler"/>
</firmware>
<firmware name="lisa_test_progs">
<target name="test_led" board="lisa_l_1.0"/>
<target name="test_uart" board="lisa_l_1.0"/>
<target name="test_servos" board="lisa_l_1.0"/>
<target name="test_telemetry" board="lisa_l_1.0"/>
<target name="test_baro" board="lisa_l_1.0"/>
<target name="test_imu_b2" board="lisa_l_1.0"/>
<target name="test_imu_b2_2" board="lisa_l_1.0"/>
<target name="test_imu_aspirin" board="lisa_l_1.0"/>
<target name="test_rc_spektrum" board="lisa_l_1.0"/>
<target name="test_rc_ppm" board="lisa_l_1.0"/>
<target name="test_adc" board="lisa_l_1.0"/>
<target name="test_hmc5843" board="lisa_l_1.0"/>
<target name="test_itg3200" board="lisa_l_1.0"/>
<target name="test_adxl345" board="lisa_l_1.0"/>
<target name="test_esc_mkk_simple" board="lisa_l_1.0"/>
<target name="test_esc_asctecv1_simple" board="lisa_l_1.0"/>
<target name="test_actuators_mkk" board="lisa_l_1.0"/>
<target name="test_actuators_asctecv1" board="lisa_l_1.0"/>
</firmware>
<firmware name="lisa_passthrough">
<target name="overo_test_passthrough" board="lisa_l_1.0" >
<configure name="HOST" value="A7"/>
<configure name="USER" value=""/>
<configure name="TARGET_DIR" value="~"/>
<configure name="PERIODIC_FREQ" value="512"/>
</target>
<target name="stm_passthrough" board="lisa_l_1.0">
<subsystem name="radio_control" type="spektrum"/>
<subsystem name="imu" type="b2_v1.1"/>
</target>
</firmware>
</airframe>