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LisaL_v1.1_aspirin_v1.5_rc.xml
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LisaL_v1.1_aspirin_v1.5_rc.xml
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<!--
This airframe is connected to the build server and is used for hardware testing.
The hardware configuration is
Powered via a plug 12V pack
Lisa/L v1.1 board
XBee connected to UART2 configured at 38400 (Configured for XBee API
Booz2 v1.2
-->
<airframe name="TestConfig">
<firmware name="rotorcraft">
<target name="ap" board="lisa_l_1.1">
<!--define name="NO_RC_THRUST_LIMIT"/-->
<subsystem name="radio_control" type="spektrum"/>
<define name="RADIO_MODE" value="RADIO_AUX1"/>
<define name="RADIO_KILL_SWITCH" value="RADIO_GEAR"/>
<configure name="USE_SECONDARY_SPEKTRUM_RECEIVER" value="1"/>
</target>
<target name="nps" board="pc">
<subsystem name="fdm" type="jsbsim"/>
<subsystem name="radio_control" type="ppm"/>
</target>
<subsystem name="telemetry" type="xbee_api">
<configure name="MODEM_BAUD" value="B38400"/>
</subsystem>
<subsystem name="motor_mixing"/>
<subsystem name="actuators" type="mkk"/>
<subsystem name="imu" type="aspirin_v1.5"/>
<subsystem name="gps" type="ublox">
<configure name="GPS_BAUD" value="B57600"/>
</subsystem>
<subsystem name="stabilization" type="int_euler"/>
<subsystem name="ahrs" type="int_cmpl_quat"/>
<subsystem name="ins"/>
</firmware>
<!--
<firmware name="lisa_test_progs">
<target name="test_led" board="lisa_l_1.1"/>
<target name="test_uart" board="lisa_l_1.1"/>
<target name="test_servos" board="lisa_l_1.1"/>
<target name="test_telemetry" board="lisa_l_1.1"/>
<target name="test_baro" board="lisa_l_1.1"/>
<target name="test_imu_b2" board="lisa_l_1.1"/>
<target name="test_imu_b2_2" board="lisa_l_1.1"/>
<target name="test_imu_aspirin" board="lisa_l_1.1"/>
<target name="test_rc_spektrum" board="lisa_l_1.1"/>
<target name="test_rc_ppm" board="lisa_l_1.1"/>
<target name="test_adc" board="lisa_l_1.1"/>
<target name="test_hmc5843" board="lisa_l_1.1"/>
<target name="test_itg3200" board="lisa_l_1.1"/>
<target name="test_adxl345" board="lisa_l_1.1"/>
<target name="test_esc_mkk_simple" board="lisa_l_1.1"/>
<target name="test_esc_asctecv1_simple" board="lisa_l_1.1"/>
<target name="test_actuators_mkk" board="lisa_l_1.1"/>
<target name="test_actuators_asctecv1" board="lisa_l_1.1"/>
</firmware>
<firmware name="lisa_passthrough">
<target name="overo_test_passthrough" board="lisa_l_1.1" >
<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_1.1">
<subsystem name="radio_control" type="spektrum"/>
<subsystem name="imu" type="b2_v1.2"/>
</target>
</firmware>
-->
<section name="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4"/>
<define name="ADDR" value="{ 0x52, 0x54, 0x56, 0x58 }"/>
</section>
<servos driver="Mkk">
<servo name="FRONT" no="0" min="0" neutral="2" max="210"/>
<servo name="BACK" no="1" min="0" neutral="2" max="210"/>
<servo name="RIGHT" no="2" min="0" neutral="2" max="210"/>
<servo name="LEFT" no="3" min="0" neutral="2" max="210"/>
</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="MIXING" prefix="MOTOR_MIXING_">
<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, 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>
<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="IMU" prefix="IMU_">
<define name="GYRO_P_NEUTRAL" value="32581"/>
<define name="GYRO_Q_NEUTRAL" value="32008"/>
<define name="GYRO_R_NEUTRAL" value="33207"/>
<define name="GYRO_P_SENS" value=".903" integer="16"/>
<define name="GYRO_Q_SENS" value=".905" integer="16"/>
<define name="GYRO_R_SENS" value=".893" 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="25950"/>
<define name="ACCEL_Y_NEUTRAL" value="26351"/>
<define name="ACCEL_Z_NEUTRAL" value="25696"/>
<define name="ACCEL_X_SENS" value="1.86342150011" integer="16"/>
<define name="ACCEL_Y_SENS" value="1.88378993899" integer="16"/>
<define name="ACCEL_Z_SENS" value="1.86557913201" 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="0"/>
<define name="MAG_Y_NEUTRAL" value="0"/>
<define name="MAG_Z_NEUTRAL" value="0"/>
<define name="MAG_X_SENS" value="1." integer="16"/>
<define name="MAG_Y_SENS" value="1." integer="16"/>
<define name="MAG_Z_SENS" value="1." 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="0." unit="deg"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_MANUAL" 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="12.4" unit="V"/>
<define name="MAX_BAT_LEVEL" value="16.8" unit="V" />
<define name="CRITIC_BAT_LEVEL" value="13.0" unit="V" />
<define name="LOW_BAT_LEVEL" value="14.0" 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="0.9"/>
<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="0.9"/>
<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="0.9"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="900"/>
<define name="PHI_DGAIN" value="200"/>
<define name="PHI_IGAIN" value="200"/>
<define name="THETA_PGAIN" value="900"/>
<define name="THETA_DGAIN" value="200"/>
<define name="THETA_IGAIN" value="200"/>
<define name="PSI_PGAIN" value="900"/>
<define name="PSI_DGAIN" value="200"/>
<define name="PSI_IGAIN" value="10"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value="200"/>
<define name="THETA_DDGAIN" value="200"/>
<define name="PSI_DDGAIN" value="200"/>
</section>
<section name="AHRS" prefix="AHRS_">
<define name="PROPAGATE_FREQUENCY" value="512"/>
<define name="H_X" value=" 0.3723657"/>
<define name="H_Y" value=" 0.1515225"/>
<define name="H_Z" value="-0.9156335"/>
</section>
<section name="INS" prefix="INS_">
<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="150"/>
<define name="HOVER_KD" value="80"/>
<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"/>
</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_default.h""/>
</section>
</airframe>