add small quad

This commit is contained in:
Gautier Hattenberger
2010-06-28 11:23:00 +00:00
parent e6b746d5c8
commit 8e0e120ef1
+237
View File
@@ -0,0 +1,237 @@
<airframe name="BOOZ2_A4">
<servos min="0" neutral="0" max="0xff">
<servo name="PITCH" no="0" min="0" neutral="0" max="255"/>
<servo name="ROLL" no="1" min="0" neutral="0" max="255"/>
<servo name="YAW" no="2" min="0" neutral="0" max="255"/>
<servo name="THRUST" 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="IMU" prefix="IMU_">
<define name="GYRO_P_CHAN" value="1"/>
<define name="GYRO_Q_CHAN" value="0"/>
<define name="GYRO_R_CHAN" value="2"/>
<define name="GYRO_P_NEUTRAL" value="33100"/>
<define name="GYRO_Q_NEUTRAL" value="32440"/>
<define name="GYRO_R_NEUTRAL" value="33033"/>
<define name="GYRO_P_SENS" value=" 1.00" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.00" integer="16"/>
<define name="GYRO_R_SENS" value="-1.00" integer="16"/>
<define name="ACCEL_X_CHAN" value="5"/>
<define name="ACCEL_Y_CHAN" value="3"/>
<define name="ACCEL_Z_CHAN" value="4"/>
<define name="ACCEL_X_NEUTRAL" value="32932"/>
<define name="ACCEL_Y_NEUTRAL" value="32251"/>
<define name="ACCEL_Z_NEUTRAL" value="32463"/>
<define name="ACCEL_X_SENS" value="-2.59502439625" integer="16"/>
<define name="ACCEL_Y_SENS" value="-2.57636806334" integer="16"/>
<define name="ACCEL_Z_SENS" value="-2.59680479039" integer="16"/>
<define name="MAG_X_CHAN" value="0"/>
<define name="MAG_Y_CHAN" value="1"/>
<define name="MAG_Z_CHAN" value="2"/>
<define name="MAG_X_NEUTRAL" value="-75"/>
<define name="MAG_Y_NEUTRAL" value="17"/>
<define name="MAG_Z_NEUTRAL" value="7"/>
<define name="MAG_X_SENS" value="5.50726991669" integer="16"/>
<define name="MAG_Y_SENS" value="-5.43740121157" integer="16"/>
<define name="MAG_Z_SENS" value="-2.60492836649" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(-1.5)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(-1.5)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(-45.)"/>
</section>
<section name="STABILIZATION_RATE" prefix="BOOZ_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="BOOZ_STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="-1000"/>
<define name="PHI_DGAIN" value="-250"/>
<define name="PHI_IGAIN" value="-40"/>
<define name="THETA_PGAIN" value="-1000"/>
<define name="THETA_DGAIN" value="-250"/>
<define name="THETA_IGAIN" value="-40"/>
<define name="PSI_PGAIN" value="-1000"/>
<define name="PSI_DGAIN" value="-350"/>
<define name="PSI_IGAIN" value="-10"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value=" 350"/>
<define name="THETA_DDGAIN" value=" 350"/>
<define name="PSI_DDGAIN" value=" 300"/>
</section>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="TRIM_A" value="0"/>
<define name="TRIM_E" value="0"/>
<define name="TRIM_R" value="0"/>
<define name="HACK_45" value="1"/>
</section>
<section name="INS" prefix="BOOZ_INS_">
<define name="BARO_SENS" value="16.5" integer="16"/>
</section>
<section name="GUIDANCE_V" prefix="BOOZ2_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="REF_MIN_ZDD" value="-1.5*9.81"/>
<define name="REF_MAX_ZDD" value=" 0.5*9.81"/>
<define name="REF_MIN_ZD" value="-1.5"/>
<define name="REF_MAX_ZD" value=" 1.5"/>
<define name="HOVER_KP" value="-500"/>
<define name="HOVER_KD" value="-250"/>
<define name="HOVER_KI" value="0"/>
<!-- SPEED_BFP_OF_REAL(1.5) / (MAX_PPRZ/2) -->
<define name="RC_CLIMB_COEF" value ="163"/>
<!-- SPEED_BFP_OF_REAL(1.5) * 20% -->
<define name="RC_CLIMB_DEAD_BAND" value ="160000"/>
</section>
<section name="GUIDANCE_H" prefix="BOOZ2_GUIDANCE_H_">
<define name="PGAIN" value="-100"/>
<define name="DGAIN" value="-100"/>
<define name="IGAIN" value="-0"/>
<define name="NGAIN" value="-0"/>
<!-- feedforward -->
<define name="AGAIN" value="100"/>
</section>
<section name="BAT">
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<define name="BATTERY_SENS" value="0.25" integer="16"/>
</section>
<section name="AUTOPILOT">
<define name="BOOZ2_MODE_MANUAL" value="BOOZ2_AP_MODE_ATTITUDE_DIRECT"/>
<define name="BOOZ2_MODE_AUTO1" value="BOOZ2_AP_MODE_ATTITUDE_Z_HOLD"/>
<define name="BOOZ2_MODE_AUTO2" value="BOOZ2_AP_MODE_NAV"/>
</section>
<section name="FMS">
<define name="BOOZ_FMS_TIMEOUT" value="0"/>
</section>
<section name="CAM" prefix="BOOZ_CAM_">
<define name="TILT_NEUTRAL" value="1500"/>
<define name="TILT_MIN" value="1000"/>
<define name="TILT_MAX" value="2000"/>
<define name="TILT_ANGLE_MIN" value="RadOfDeg(-85.)" unit="rad"/>
<define name="TILT_ANGLE_MAX" value="RadOfDeg( 30.)" unit="rad"/>
<define name="PAN_NEUTRAL" value="0"/>
<define name="PAN_MIN" value="0"/>
<define name="PAN_MAX" value="25736"/> <!-- 360 deg (2^12) -->
</section>
<section name="MISC">
<define name="BOOZ_ANALOG_BARO_THRESHOLD" value="800"/>
<define name="BOOZ2_FACE_REINJ_1" value="1024"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="10."/>
</section>
<makefile>
ARCH=lpc21
ARCHI=arm7
BOARD_CFG = \"boards/booz2_v1_0.h\"
FLASH_MODE=IAP
# prevents motors from ever starting
#ap.CFLAGS += -DKILL_MOTORS
include $(PAPARAZZI_SRC)/conf/autopilot/booz2_common.makefile
include $(CFG_BOOZ)/booz2_autopilot.makefile
include $(CFG_BOOZ)/booz2_test_progs.makefile
ap.CFLAGS += -DBOOZ_FAILSAFE_GROUND_DETECT
ap.CFLAGS += -DMODEM_BAUD=B57600
include $(CFG_BOOZ)/subsystems/booz2_actuators_asctec.makefile
include $(CFG_BOOZ)/subsystems/booz2_radio_control_ppm.makefile
include $(CFG_BOOZ)/subsystems/booz2_imu_b2v1_1.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz2_analog_bat_baro.makefile
include $(CFG_BOOZ)/subsystems/booz2_fms_datalink.makefile
include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
include $(CFG_BOOZ)/subsystems/booz2_ins_hff.makefile
ap.CFLAGS += -DUSE_GPS_ACC4R
ap.CFLAGS += -DB2_GUIDANCE_H_USE_REF
ap.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
#ap.srcs += $(SRC_BOOZ_ARCH)/booz2_pwm_hw.c
ap.CFLAGS += -DUSE_MODULES
sim.CFLAGS += -DBSM_PARAMS=\"booz_sensors_model_params_booz2_a2.h\"
sim.CFLAGS += -DNPS_NO_SUPERVISION
include $(CFG_BOOZ)/booz2_simulator_nps.makefile
sim.CFLAGS += -DB2_GUIDANCE_H_USE_REF
sim.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
sim.srcs += $(SRC_BOOZ_SIM)/booz2_pwm_hw.c
</makefile>
</airframe>