Hello
paparazzi community
After 8h of trying to get rid of my drift on phi you are my last hope.
Every hint is useful!
I think it has something to do with the AHRS.
Compensation of psi drift with MAG
The plot shows a fast 90° turn clockwise and back again.
In the lower plot you also can that the bias changes a lot, is that
"normal"?
Lisa M 1.0 + Aspirin IMU 1.5
(I did the calibration of Accel and mag a few time with similar
results)
Thx for any hint!
Bruzzlee
<airframe name="Odonata_LisaM">
<firmware name="rotorcraft">
<target name="ap" board="lisa_m_1.0">
<subsystem name="radio_control" type="spektrum">
<!--define name="RADIO_CONTROL_SPEKTRUM_SIGNS" value="\{1,1,-1,1,-1,-1\}"/-->
<define name="RADIO_MODE" value="RADIO_GEAR"/>
<define name="RADIO_KILL_SWITCH" value="RADIO_AUX1"/>
<configure name="USE_SECONDARY_SPEKTRUM_RECEIVER" value="0"/>
<configure name="USE_KILL_SWITCH_FOR_MOTOR_ARMING" value="1"/>
<!--configure name="AUTOPILOT_DISABLE_AHRS_KILL" value="0"/-->
</subsystem>
</target>
<target name="nps" board="pc">
<subsystem name="fdm" type="jsbsim"/>
<subsystem name="radio_control" type="ppm"/>
</target>
<subsystem name="motor_mixing"/>
<subsystem name="actuators" type="pwm">
<define name="SERVO_HZ" value="400"/>
<!--define name="USE_SERVOS_7AND8"/-->
</subsystem>
<subsystem name="telemetry" type="transparent"/>
<configure name="MODEM_BAUD" value="B9600"/>
<subsystem name="imu" type="aspirin_v1.5"/>
<subsystem name="gps" type="ublox"/>
<subsystem name="stabilization" type="int_quat"/>
<subsystem name="ahrs" type="int_cmpl_quat"/>
<subsystem name="ins"/>
<!--define name="USE_INS_NAV_INIT"/-->
<!--subsystem name="stabilization" type="int_euler"/>
<subsystem name="ahrs" type="int_cmpl_euler"/-->
</firmware>
<firmware name="lisa_test_progs">
<target name="test_led" board="lisa_m_1.0">
<configure name="SYS_TIME_LED" value="none"/>
</target>
<target name="test_uart" board="lisa_m_1.0"/>
<target name="test_imu_aspirin" board="lisa_m_1.0"/>
<target name="test_rc_spektrum" board="lisa_m_1.0"/>
<target name="test_baro" board="lisa_m_1.0"/>
</firmware>
<servos driver="Pwm">
<servo name="FRONT" no="0" min="1000" neutral="1100" max="1900"/>
<servo name="BACK" no="1" min="1000" neutral="1100" max="1900"/>
<servo name="RIGHT" no="2" min="1000" neutral="1100" max="1900"/>
<servo name="LEFT" no="3" min="1000" neutral="1100" max="1900"/>
</servos>
<commands>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="0"/>
</commands>
<command_laws>
<call fun="motor_mixing_run(autopilot_motors_on,FALSE,values)"/>
<set servo="FRONT" value="motor_mixing.commands[SERVO_FRONT]"/>
<set servo="BACK" value="motor_mixing.commands[SERVO_BACK]"/>
<set servo="RIGHT" value="motor_mixing.commands[SERVO_RIGHT]"/>
<set servo="LEFT" value="motor_mixing.commands[SERVO_LEFT]"/>
</command_laws>
<section name="MIXING" prefix="MOTOR_MIXING_">
<define name="STOP_MOTOR" value="0"/>
<define name="TRIM_ROLL" value="0"/>
<define name="TRIM_PITCH" value="0"/>
<define name="TRIM_YAW" value="0"/>
<define name="NB_MOTOR" value="4"/>
<define name="SCALE" value="256"/>
<!--define name="ROLL_COEF" value="{ 0, -256, 0, 256 }"/>
<define name="PITCH_COEF" value="{ 256, 0, -256, 0 }"/>
<define name="YAW_COEF" value="{ -256, 256, -256, 256 }"/>
<define name="THRUST_COEF" value="{ 256, 256, 256, 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="-60"/>
<define name="GYRO_Q_NEUTRAL" value="1"/>
<define name="GYRO_R_NEUTRAL" value="-40"/-->
<!--define name="GYRO_P_SENS" value="4.359" integer="16"/>
<define name="GYRO_Q_SENS" value="4.359" integer="16"/>
<define name="GYRO_R_SENS" value="4.359" integer="16"/-->
<!--define name="GYRO_P_SENS" value="4.967" integer="16"/>
<define name="GYRO_Q_SENS" value="4.967" integer="16"/>
<define name="GYRO_R_SENS" value="8.967" integer="16"/>
<define name="GYRO_PQ_SENS" value="0.0" integer="16"/>
<define name="GYRO_PR_SENS" value="0.0" integer="16"/>
<define name="GYRO_QR_SENS" value="0.0" integer="16"/-->
<define name="ACCEL_X_NEUTRAL" value="2"/>
<define name="ACCEL_Y_NEUTRAL" value="-2"/>
<define name="ACCEL_Z_NEUTRAL" value="-18"/>
<define name="ACCEL_X_SENS" value="38.364291532" integer="16"/>
<define name="ACCEL_Y_SENS" value="37.412848171" integer="16"/>
<define name="ACCEL_Z_SENS" value="39.5532801506" integer="16"/>
<!--define name="ACCEL_XY_SENS" value="0.0" integer="16"/>
<define name="ACCEL_XZ_SENS" value="0.0" integer="16"/>
<define name="ACCEL_YZ_SENS" value="0.0" integer="16"/-->
<define name="MAG_X_NEUTRAL" value="-101"/>
<define name="MAG_Y_NEUTRAL" value="32"/>
<define name="MAG_Z_NEUTRAL" value="-42"/>
<define name="MAG_X_SENS" value="4.04547589416" integer="16"/>
<define name="MAG_Y_SENS" value="4.57546806101" integer="16"/>
<define name="MAG_Z_SENS" value="4.01214304094" integer="16"/>
<!--define name="MAG_XY_SENS" value="0.0" integer="16"/>
<define name="MAG_XZ_SENS" value="0.0" integer="16"/>
<define name="MAG_YZ_SENS" value="0.0" 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="90." unit="deg"/>
</section>
<section name="AUTOPILOT">
<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_HOVER_Z_HOLD"/>
</section>
<section name="BAT">
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
</section>
<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
<!-- setpoints -->
<define name="SP_MAX_P" value="10000"/>
<define name="SP_MAX_Q" value="10000"/>
<define name="SP_MAX_R" value="10000"/>
<define name="DEADBAND_P" value="20"/>
<define name="DEADBAND_Q" value="20"/>
<define name="DEADBAND_R" value="200"/>
<define name="REF_TAU" value="4"/>
<!-- feedback -->
<define name="GAIN_P" value="400"/>
<define name="GAIN_Q" value="400"/>
<define name="GAIN_R" value="350"/>
<define name="IGAIN_P" value="75"/>
<define name="IGAIN_Q" value="75"/>
<define name="IGAIN_R" value="50"/>
<!-- feedforward -->
<define name="DDGAIN_P" value="300"/>
<define name="DDGAIN_Q" value="300"/>
<define name="DDGAIN_R" value="300"/>
</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_PSI" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="SP_MAX_P" value="90." unit="deg/s"/>
<define name="DEADBAND_E" value="0"/>
<define name="DEADBAND_A" value="250"/>
<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="400." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="400." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(8000.)"/>
<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="750"/>
<define name="PHI_DGAIN" value="500"/>
<define name="PHI_IGAIN" value="100"/>
<define name="THETA_PGAIN" value="750"/>
<define name="THETA_DGAIN" value="500"/>
<define name="THETA_IGAIN" value="100"/>
<define name="PSI_PGAIN" value="1500"/>
<define name="PSI_DGAIN" value="1000"/>
<define name="PSI_IGAIN" value="10"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value=" 150"/>
<define name="THETA_DDGAIN" value=" 150"/>
<define name="PSI_DDGAIN" value=" 300"/>
</section>
<section name="INS" prefix="INS_">
</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="400"/>
<define name="HOVER_KD" value="350"/>
<define name="HOVER_KI" value="144"/>
<define name="GUIDANCE_V_NOMINAL_HOVER_THROTTLE" value ="0.9"/>
</section>
<section name="AHRS" prefix="AHRS_">
<define name="H_X" value=" 0.03075352"/>
<define name="H_Y" value=" 0.99765715"/>
<define name="H_Z" value=" 0.06111"/>
<!--define name="H_X" value=" 0.460452"/>
<define name="H_Y" value=" 0.0031046"/>
<define name="H_Z" value=" 0.8876792"/-->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="PGAIN" value="50"/>
<define name="DGAIN" value="50"/>
<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="JSBSIM_INIT" value=""reset00""/>
<define name="SENSORS_PARAMS" value=""nps_sensors_params_booz2_a1.h""/>
<!-- mode switch on joystick channel 5 (axis numbering starting at zero) -->
<define name="JS_AXIS_MODE" value="4"/>
</section>
<!--modules main_freq="512">
<!--load name="vehicle_interface_overo_link.xml"/->
<load name="gps_ubx_ucenter.xml"/>
</modules-->
</airframe>
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