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moved old booz airframe file to obsolte dir

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This commit is contained in:
Felix Ruess
2011-01-06 19:42:40 +01:00
parent ba36c61694
commit 570685e969
6 changed files with 106 additions and 106 deletions
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conf/airframes/obsolete/booz2_Aron.xml
+203
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<airframe name="BOOZ2_A2">
<servos min="0" neutral="0" max="0xff">
<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, 0x56, 0x58 }" />
</section>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2" />
<define name="MAX_MOTOR" value="210" />
<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_CHAN" value="0"/>
<define name="GYRO_Q_CHAN" value="4"/>
<define name="GYRO_R_CHAN" value="1"/>
<define name="GYRO_P_NEUTRAL" value="31799"/>
<define name="GYRO_Q_NEUTRAL" value="32338"/>
<define name="GYRO_R_NEUTRAL" value="32668"/>
<define name="GYRO_P_SENS" value=" -0.85" integer="16"/>
<define name="GYRO_Q_SENS" value=" -0.85" integer="16"/>
<define name="GYRO_R_SENS" value=" 0.85" integer="16"/>
<define name="ACCEL_X_CHAN" value="5"/>
<define name="ACCEL_Y_CHAN" value="2"/>
<define name="ACCEL_Z_CHAN" value="6"/>
<define name="ACCEL_X_SENS" value="6.23079413" integer="16"/>
<define name="ACCEL_Y_SENS" value="-6.38411981" integer="16"/>
<define name="ACCEL_Z_SENS" value="6.27271719" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="40465"/>
<define name="ACCEL_Y_NEUTRAL" value="40252"/>
<define name="ACCEL_Z_NEUTRAL" value="39820"/>
<define name="MAG_X_CHAN" value="0"/>
<define name="MAG_Y_CHAN" value="4"/>
<define name="MAG_Z_CHAN" value="2"/>
<define name="MAG_X_NEUTRAL" value="2339"/>
<define name="MAG_Y_NEUTRAL" value="2106"/>
<define name="MAG_Z_NEUTRAL" value="1902"/>
<define name="MAG_X_SENS" value="-4.4039655" integer="16"/>
<define name="MAG_Y_SENS" value="-4.2959321" integer="16"/>
<define name="MAG_Z_SENS" value="-4.0988408" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
<define name="BODY_TO_IMU_THETA" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
<define name="BODY_TO_IMU_PSI" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
</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="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(400)"/>
<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(400)"/>
<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(180.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="-400"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-400"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<define name="PSI_PGAIN" value="-380"/>
<define name="PSI_DGAIN" value="-320"/>
<define name="PSI_IGAIN" value="-75"/>
<!-- 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="14.9" 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="-250"/>
<define name="HOVER_KI" value="-100"/>
<!-- 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="GUIDANCE_H_">
<define name="PGAIN" value="-100"/>
<define name="DGAIN" value="-100"/>
<define name="IGAIN" value="-0"/>
</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"/>
<!-- <define name="BATTERY_SENS" value="1" integer="16"/>-->
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_RC_CLIMB"/>
<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_Z_HOLD"/>
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<makefile>
ARCH=lpc21
BOARD_CFG = \"twog_booz.h\"
# 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 += -DMODEM_BAUD=B57600
include $(CFG_BOOZ)/subsystems/booz2_radio_control_ppm.makefile
include $(CFG_BOOZ)/subsystems/booz2_actuators_mkk.makefile
include $(CFG_BOOZ)/subsystems/booz2_imu_crista.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
include $(CFG_BOOZ)/subsystems/booz2_fms_test_signal.makefile
</makefile>
</airframe>
conf/airframes/obsolete/booz2_NoVa.xml
+256
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<airframe name="BOOZ2_NoVa">
<!-- PPZUAV_BOOZ2_NoVa
PPZUAV_BOOZ2_MAIN_001 main board
PPZUAV_BOOZ2_IMU_001 IMU
PPZUAV_BOOZ2_GPS_001 LEA-5H GPS
Datamodems configured for 57600 baud
Modified 6A speed controllers
-->
<servos min="0" neutral="0" max="0xff">
<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="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="33008"/>
<define name="GYRO_Q_NEUTRAL" value="31899"/>
<define name="GYRO_R_NEUTRAL" value="32989"/>
<define name="GYRO_P_SENS" value=" 1.01" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.01" integer="16"/>
<define name="GYRO_R_SENS" value="-1.01" 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_SENS" value="-2.19476868" integer="16"/>
<define name="ACCEL_Y_SENS" value="-2.88368188" integer="16"/>
<define name="ACCEL_Z_SENS" value="-2.57172803" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="33160"/>
<define name="ACCEL_Y_NEUTRAL" value="32523"/>
<define name="ACCEL_Z_NEUTRAL" value="32418"/>
<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_SENS" value="4.73914612" integer="16"/>
<define name="MAG_Y_SENS" value="-5.34705586" integer="16"/>
<define name="MAG_Z_SENS" value="-3.57580805" integer="16"/>
<define name="MAG_X_NEUTRAL" value="-89"/>
<define name="MAG_Y_NEUTRAL" value="20"/>
<define name="MAG_Z_NEUTRAL" value="-30"/>
<define name="BODY_TO_IMU_PHI" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
<define name="BODY_TO_IMU_THETA" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
<define name="BODY_TO_IMU_PSI" value="ANGLE_BFP_OF_REAL(RadOfDeg(-90.))"/>
</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="0" />
<define name="DEADBAND_Q" value="0" />
<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="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(180.)"/><!-- Maximum speed in deg/s-->
<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(180.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<!--
<define name="PHI_PGAIN" value="-400"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-400"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<define name="PSI_PGAIN" value="-380"/>
<define name="PSI_DGAIN" value="-320"/>
<define name="PSI_IGAIN" value="-75"/>
-->
<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="-200"/>
<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="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2" />
<define name="MAX_MOTOR" value="210" />
<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="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x56, 0x54, 0x58 }" />
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="14.9" 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="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="-150"/>
<define name="HOVER_KD" value="-80"/>
<define name="HOVER_KI" value="0"/>
<!-- 1.5m/s for full stick : 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"/>
<!-- <define name="INV_M" value="0.118"/> -->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="PGAIN" value="-70"/>
<define name="DGAIN" value="-150"/>
<define name="IGAIN" value="-15"/>
<define name="NGAIN" value="-0"/>
<define name="AGAIN" value="-0"/>
</section>
<section name="BAT">
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.0" unit="V"/>
<define name="BATTERY_SENS" value="0.18" integer="16"/>
<!-- <define name="BATTERY_SENS" value="1" integer="16"/>-->
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_RATE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<makefile>
ARCH=lpc21
BOARD_CFG = \"boards/booz2_v1_0.h\"
# 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 += -DFAILSAFE_GROUND_DETECT
#ap.CFLAGS += -DMODEM_BAUD=B38400
ap.CFLAGS += -DMODEM_BAUD=B57600
include $(CFG_BOOZ)/subsystems/booz2_radio_control_ppm.makefile
include $(CFG_BOOZ)/subsystems/booz2_actuators_mkk.makefile
include $(CFG_BOOZ)/subsystems/booz2_imu_b2v1_1.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
include $(CFG_BOOZ)/subsystems/ins_hff.makefile
#set USE_GPS lag for horizontal filter
ap.CFLAGS += -DGPS_LAG=0.8 -DUSE_GPS_ACC4R
ap.CFLAGS += -DGPS_USE_LATLONG
ap.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
</makefile>
</airframe>
conf/airframes/obsolete/booz2_NoVa_001.xml
+256
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@@ -0,0 +1,256 @@
<airframe name="BOOZ2_NoVa_001">
<!-- BOOZ2_NoVa
BOOZ2_MAIN_002 main board
BOOZ2_IMU_002 IMU
BOOZ2_GPS_002 LEA-5H GPS
Datamodems configured for 57600 baud
ZEF100 Speed Controllers
-->
<servos min="0" neutral="0" max="0xff">
<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="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="31675"/>
<define name="GYRO_Q_NEUTRAL" value="31650"/>
<define name="GYRO_R_NEUTRAL" value="31475"/>
<define name="GYRO_P_SENS" value=" 1.01" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.01" integer="16"/>
<define name="GYRO_R_SENS" value="-1.01" 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_SENS" value="-2.57091959" integer="16"/>
<define name="ACCEL_Y_SENS" value="-2.55833628" integer="16"/>
<define name="ACCEL_Z_SENS" value="-2.57095664" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="32875"/>
<define name="ACCEL_Y_NEUTRAL" value="32516"/>
<define name="ACCEL_Z_NEUTRAL" value="32398"/>
<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="-22"/>
<define name="MAG_Y_NEUTRAL" value="-14"/>
<define name="MAG_Z_NEUTRAL" value="16"/>
<define name="MAG_X_SENS" value="4.79355327494" integer="16"/>
<define name="MAG_Y_SENS" value="-5.04941795802" integer="16"/>
<define name="MAG_Z_SENS" value="-2.98000294999" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(-90.)"/>
</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="0" />
<define name="DEADBAND_Q" value="0" />
<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="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(180.)"/><!-- Maximum speed in deg/s-->
<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(180.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<!--
<define name="PHI_PGAIN" value="-400"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-400"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<define name="PSI_PGAIN" value="-380"/>
<define name="PSI_DGAIN" value="-320"/>
<define name="PSI_IGAIN" value="-75"/>
-->
<define name="PHI_PGAIN" value="-1000"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-1000"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<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="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2" />
<define name="MAX_MOTOR" value="210" />
<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="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x58, 0x54, 0x56 }" />
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="14.9" 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="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="-150"/>
<define name="HOVER_KD" value="-80"/>
<define name="HOVER_KI" value="0"/>
<!-- 1.5m/s for full stick : 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"/>
<!-- <define name="INV_M" value="0.118"/> -->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="PGAIN" value="-50"/>
<define name="DGAIN" value="-60"/>
<define name="IGAIN" value="-15"/>
<define name="NGAIN" value="-0"/>
<define name="AGAIN" value="-0"/>
</section>
<section name="BAT">
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.0" unit="V"/>
<define name="BATTERY_SENS" value="0.18" integer="16"/>
<!-- <define name="BATTERY_SENS" value="1" integer="16"/>-->
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_HOVER_Z_HOLD"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<makefile>
ARCH=lpc21
FLASH_MODE=IAP
BOARD_CFG = \"boards/booz2_v1_0.h\"
# 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 += -DFAILSAFE_GROUND_DETECT
ap.CFLAGS += -DMODEM_BAUD=B57600
include $(CFG_BOOZ)/subsystems/booz2_radio_control_ppm.makefile
include $(CFG_BOOZ)/subsystems/booz2_actuators_mkk.makefile
include $(CFG_BOOZ)/subsystems/booz2_imu_b2v1_1.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
include $(CFG_BOOZ)/subsystems/ins_hff.makefile
#set USE_GPS lag for horizontal filter
ap.CFLAGS += -DGPS_LAG=0.8 -DUSE_GPS_ACC4R
ap.CFLAGS += -DGPS_USE_LATLONG
ap.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
</makefile>
</airframe>
conf/airframes/obsolete/booz2_NoVa_002.xml
+257
View File
@@ -0,0 +1,257 @@
<airframe name="BOOZ2_NoVa_002">
<!-- BOOZ2_NoVa
BOOZ2_MAIN_001 main board
BOOZ2_IMU_001 IMU
BOOZ2_GPS_001 LEA-5H GPS
Datamodems configured for 57600 baud
ZEF100 Speed Controllers
-->
<servos min="0" neutral="0" max="0xff">
<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="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="33008"/>
<define name="GYRO_Q_NEUTRAL" value="31899"/>
<define name="GYRO_R_NEUTRAL" value="32989"/>
<define name="GYRO_P_SENS" value=" 1.01" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.01" integer="16"/>
<define name="GYRO_R_SENS" value="-1.01" 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_SENS" value="-2.19476868" integer="16"/>
<define name="ACCEL_Y_SENS" value="-2.88368188" integer="16"/>
<define name="ACCEL_Z_SENS" value="-2.57172803" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="33160"/>
<define name="ACCEL_Y_NEUTRAL" value="32523"/>
<define name="ACCEL_Z_NEUTRAL" value="32418"/>
<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_SENS" value="4.73914612" integer="16"/>
<define name="MAG_Y_SENS" value="-5.34705586" integer="16"/>
<define name="MAG_Z_SENS" value="-3.57580805" integer="16"/>
<define name="MAG_X_NEUTRAL" value="-89"/>
<define name="MAG_Y_NEUTRAL" value="20"/>
<define name="MAG_Z_NEUTRAL" value="-30"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(-90.)"/>
</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="0" />
<define name="DEADBAND_Q" value="0" />
<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="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(180.)"/><!-- Maximum speed in deg/s-->
<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(180.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<!--
<define name="PHI_PGAIN" value="-400"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-400"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<define name="PSI_PGAIN" value="-380"/>
<define name="PSI_DGAIN" value="-320"/>
<define name="PSI_IGAIN" value="-75"/>
-->
<define name="PHI_PGAIN" value="-1000"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-1000"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<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="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2" />
<define name="MAX_MOTOR" value="210" />
<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="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x54, 0x58, 0x56, 0x52 }" />
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="14.9" 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="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="-150"/>
<define name="HOVER_KD" value="-80"/>
<define name="HOVER_KI" value="0"/>
<!-- 1.5m/s for full stick : 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"/>
<!-- <define name="INV_M" value="0.118"/> -->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="PGAIN" value="-70"/>
<define name="DGAIN" value="-150"/>
<define name="IGAIN" value="-15"/>
<define name="NGAIN" value="-0"/>
<define name="AGAIN" value="-0"/>
</section>
<section name="BAT">
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.0" unit="V"/>
<define name="BATTERY_SENS" value="0.18" integer="16"/>
<!-- <define name="BATTERY_SENS" value="1" integer="16"/>-->
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_RATE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<makefile>
ARCH=lpc21
FLASH_MODE=IAP
BOARD_CFG = \"boards/booz2_v1_0.h\"
# 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 += -DFAILSAFE_GROUND_DETECT
#ap.CFLAGS += -DMODEM_BAUD=B38400
ap.CFLAGS += -DMODEM_BAUD=B57600
include $(CFG_BOOZ)/subsystems/booz2_radio_control_ppm.makefile
include $(CFG_BOOZ)/subsystems/booz2_actuators_mkk.makefile
include $(CFG_BOOZ)/subsystems/booz2_imu_b2v1_1.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
include $(CFG_BOOZ)/subsystems/ins_hff.makefile
#set USE_GPS lag for horizontal filter
ap.CFLAGS += -DGPS_LAG=0.8 -DUSE_GPS_ACC4R
ap.CFLAGS += -DGPS_USE_LATLONG
ap.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
</makefile>
</airframe>
conf/airframes/obsolete/booz2_s1.xml
+216
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@@ -0,0 +1,216 @@
<airframe name="BOOZ2_s1">
<servos min="0" neutral="0" max="0xff">
<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="BUSS_BLMC" prefix="BUSS_BLMC_">
<define name="ADDR" value="{ 0x58, 0x52, 0x54, 0x56 }"/>
</section>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2"/>
<define name="MAX_MOTOR" value="210"/>
<define name="TRIM_A" value="0"/>
<define name="TRIM_E" value="0"/>
<define name="TRIM_R" value="0"/>
</section>
<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="31550"/>
<define name="GYRO_Q_NEUTRAL" value="32958"/>
<define name="GYRO_R_NEUTRAL" value="32908"/>
<define name="GYRO_P_SENS" value=" 1.01" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.01" integer="16"/>
<define name="GYRO_R_SENS" value="-1.01" 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_SENS" value="-3.60757190" integer="16"/>
<define name="ACCEL_Y_SENS" value="-3.54533328" integer="16"/>
<define name="ACCEL_Z_SENS" value="-3.50331273" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="28649"/>
<define name="ACCEL_Y_NEUTRAL" value="29153"/>
<define name="ACCEL_Z_NEUTRAL" value="28559"/>
<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="-54"/>
<define name="MAG_Y_NEUTRAL" value="28"/>
<define name="MAG_Z_NEUTRAL" value="39"/>
<define name="MAG_X_SENS" value=" 5.08070238" integer="16"/>
<define name="MAG_Y_SENS" value="-4.99213794" integer="16"/>
<define name="MAG_Z_SENS" value="-2.82215800" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
<define name="BODY_TO_IMU_THETA" value="ANGLE_BFP_OF_REAL(RadOfDeg(-11.))"/>
<define name="BODY_TO_IMU_PSI" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
</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="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(180.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="-1200"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-1200"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<define name="PSI_PGAIN" value="-800"/>
<define name="PSI_DGAIN" value="-300"/>
<define name="PSI_IGAIN" value="-200"/>
<!-- 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"/>
</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="HOVER_KP" value="-300"/>
<define name="HOVER_KD" value="-200"/>
<define name="HOVER_KI" value="-0"/>
<!-- 1.5m/s for full stick : 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"/>
<!-- NDJD : Valeur mesurée 10/09/2009 -->
<define name="INV_M" value="0.111"/>
</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="BAT">
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<define name="BATTERY_SENS" value="0.245" integer="16"/>
</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_NAV"/>
</section>
<section name="FMS">
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="{&quot;front_motor&quot;, &quot;back_motor&quot;, &quot;right_motor&quot;, &quot;left_motor&quot;}"/>
<define name="INITIAL_CONDITITONS" value="&quot;reset00&quot;"/>
<define name="SENSORS_PARAMS" value="&quot;nps_sensors_params_booz2_a1.h&quot;"/>
</section>
<makefile>
ARCH=lpc21
BOARD_CFG = \"boards/booz2_v1_0.h\"
# prevents motors from ever starting
# ap.CFLAGS += -DKILL_MOTORS
# Enables Canon Hack Development Kit features.
ap.CFLAGS += -DUSE_LED -DCANON_CHDK
ap.srcs += $(PAPARAZZI_SRC)/sw/airborne/chdk.c
include $(PAPARAZZI_SRC)/conf/autopilot/booz2_common.makefile
include $(CFG_BOOZ)/booz2_autopilot.makefile
include $(CFG_BOOZ)/booz2_test_progs.makefile
ap.CFLAGS += -DMODEM_BAUD=B57600
include $(CFG_BOOZ)/subsystems/booz2_actuators_buss.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_ahrs_cmpl.makefile
</makefile>
</airframe>
conf/airframes/obsolete/booz2_x1.xml
+216
View File
@@ -0,0 +1,216 @@
<!-- Xavier Paris booz2 mikrokopter -->
<airframe name="BOOZ2_x1">
<servos min="0" neutral="0" max="0xff">
<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, 0x56, 0x58 }"/>
</section>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2"/>
<define name="MAX_MOTOR" value="210"/>
<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_CHAN" value="1"/>
<define name="GYRO_Q_CHAN" value="0"/>
<define name="GYRO_R_CHAN" value="2"/>
<define name="GYRO_P_NEUTRAL" value="31489"/>
<define name="GYRO_Q_NEUTRAL" value="31814"/>
<define name="GYRO_R_NEUTRAL" value="32752"/>
<define name="GYRO_P_SENS" value=" 1.01" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.01" integer="16"/>
<define name="GYRO_R_SENS" value="-1.01" 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_SENS" value="-3.49637365" integer="16"/>
<define name="ACCEL_Y_SENS" value="-3.48686012" integer="16"/>
<define name="ACCEL_Z_SENS" value="-3.55363744" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="29174"/>
<define name="ACCEL_Y_NEUTRAL" value="29720"/>
<define name="ACCEL_Z_NEUTRAL" value="28629"/>
<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_SENS" value="5.20834273" integer="16"/>
<define name="MAG_Y_SENS" value="-5.22061499" integer="16"/>
<define name="MAG_Z_SENS" value="-2.69279936" integer="16"/>
<define name="MAG_X_NEUTRAL" value="-164"/>
<define name="MAG_Y_NEUTRAL" value="3"/>
<define name="MAG_Z_NEUTRAL" value="42"/>
<define name="BODY_TO_IMU_PHI" value="ANGLE_BFP_OF_REAL(RadOfDeg(-3.))"/>
<define name="BODY_TO_IMU_THETA" value="ANGLE_BFP_OF_REAL(RadOfDeg(-11.))"/>
<define name="BODY_TO_IMU_PSI" value="ANGLE_BFP_OF_REAL(RadOfDeg(0.))"/>
</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="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(180.)"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="-400"/>
<define name="PHI_DGAIN" value="-300"/>
<define name="PHI_IGAIN" value="-100"/>
<define name="THETA_PGAIN" value="-400"/>
<define name="THETA_DGAIN" value="-300"/>
<define name="THETA_IGAIN" value="-100"/>
<define name="PSI_PGAIN" value="-380"/>
<define name="PSI_DGAIN" value="-320"/>
<define name="PSI_IGAIN" value="-75"/>
<!-- 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="19." 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="-100"/>
<!-- 1.5m/s for full stick : 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="GUIDANCE_H_">
<define name="PGAIN" value="-100"/>
<define name="DGAIN" value="-100"/>
<define name="IGAIN" value="-0"/>
</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="0.48" integer="16"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_RC_CLIMB"/>
<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_RC_CLIMB"/>
</section>
<section name="FMS">
</section>
<section name="MISC">
<define name="FACE_REINJ_1" value="1024"/>
</section>
<makefile>
ARCH=lpc21
BOARD_CFG = \"boards/booz2_v1_0.h\"
# prevents motors from ever starting
#ap.CFLAGS += -DKILL_MOTORS
ap.CFLAGS += -DMODEM_BAUD=B57600
include $(PAPARAZZI_SRC)/conf/autopilot/booz2_common.makefile
include $(CFG_BOOZ)/booz2_autopilot.makefile
include $(CFG_BOOZ)/booz2_test_progs.makefile
include $(CFG_BOOZ)/subsystems/booz2_radio_control_ppm.makefile
include $(CFG_BOOZ)/subsystems/booz2_actuators_mkk.makefile
include $(CFG_BOOZ)/subsystems/booz2_imu_b2v1_1.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
</makefile>
</airframe>