added a vehicle for some simulation tests

This commit is contained in:
Antoine Drouin
2010-03-15 15:37:47 +00:00
parent f23f133e58
commit 789a19d5a7
2 changed files with 403 additions and 0 deletions
+230
View File
@@ -0,0 +1,230 @@
<airframe name="BOOZ2_a1">
<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="33924"/>
<define name="GYRO_Q_NEUTRAL" value="33417"/>
<define name="GYRO_R_NEUTRAL" value="32809"/>
<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="3"/>
<define name="ACCEL_Y_CHAN" value="5"/>
<define name="ACCEL_Z_CHAN" value="6"/>
<define name="ACCEL_X_SENS" value="-2.50411474" integer="16"/>
<define name="ACCEL_Y_SENS" value="-2.48126183" integer="16"/>
<define name="ACCEL_Z_SENS" value="-2.51396167" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="32081"/>
<define name="ACCEL_Y_NEUTRAL" value="33738"/>
<define name="ACCEL_Z_NEUTRAL" value="32441"/>
<define name="MAG_X_CHAN" value="4"/>
<define name="MAG_Y_CHAN" value="0"/>
<define name="MAG_Z_CHAN" value="2"/>
<define name="MAG_X_NEUTRAL" value="2358"/>
<define name="MAG_Y_NEUTRAL" value="2362"/>
<define name="MAG_Z_NEUTRAL" value="2119"/>
<define name="MAG_X_SENS" value="-4.94075530" integer="16"/>
<define name="MAG_Y_SENS" value=" 5.10207664" integer="16"/>
<define name="MAG_Z_SENS" value="-4.90788848" integer="16"/>
<!-- <define name="MAG_45_HACK" value="1"/> -->
<!-- <define name="MAG_X_SENS" value="-4.94075530 * sqrt(2)/2" integer="16"/> -->
<!-- <define name="MAG_Y_SENS" value=" 5.10207664 * sqrt(2)/2" integer="16"/> -->
<!-- <define name="MAG_X_SENS" value="-3.4936416" integer="16"/> -->
<!-- <define name="MAG_Y_SENS" value=" 3.607713" integer="16"/> -->
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(4.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(3.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
</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="0.9"/>
<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="0.9"/>
<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="0.9"/>
<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="ARHS" prefix="AHRS_">
<define name="H_X" value="0.4912"/>
<define name="H_Y" value="0.1225"/>
<define name="H_Z" value="0.8624"/>
</section>
<section name="INS" prefix="BOOZ_INS_">
<define name="BARO_SENS" value="15." 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="HOVER_KP" value="-500"/>
<define name="HOVER_KD" value="-200"/>
<define name="HOVER_KI" value="-100"/>
<!-- 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="BOOZ2_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="BOOZ2_MODE_MANUAL" value="BOOZ2_AP_MODE_ATTITUDE_DIRECT"/>
<define name="BOOZ2_MODE_AUTO1" value="BOOZ2_AP_MODE_ATTITUDE_RC_CLIMB"/>
<define name="BOOZ2_MODE_AUTO2" value="BOOZ2_AP_MODE_ATTITUDE_Z_HOLD"/>
</section>
<section name="FMS">
</section>
<section name="MISC">
<define name="BOOZ2_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_a1p.h&quot;"/>
</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)/booz2_simulator_nps.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.makefile
include $(CFG_BOOZ)/subsystems/booz2_gps.makefile
include $(CFG_BOOZ)/subsystems/booz_ahrs_mlkf.makefile
include $(CFG_BOOZ)/subsystems/booz2_fms_test_signal.makefile
</makefile>
</airframe>
@@ -0,0 +1,173 @@
/*
* $Id$
*
* Copyright (C) 2009 Antoine Drouin
*
* This file is part of paparazzi.
*
* paparazzi is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 2, or (at your option)
* any later version.
*
* paparazzi is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
* Boston, MA 02111-1307, USA.
*
*/
#ifndef NPS_SENSORS_PARAMS_H
#define NPS_SENSORS_PARAMS_H
#include "airframe.h"
#if 1
#define NPS_BODY_TO_IMU_PHI IMU_BODY_TO_IMU_PHI
#define NPS_BODY_TO_IMU_THETA IMU_BODY_TO_IMU_THETA
#define NPS_BODY_TO_IMU_PSI IMU_BODY_TO_IMU_PSI
#else
#define NPS_BODY_TO_IMU_PHI RadOfDeg(0.)
#define NPS_BODY_TO_IMU_THETA RadOfDeg(0.)
#define NPS_BODY_TO_IMU_PSI RadOfDeg(0.)
#endif
/*
* Accelerometer
*/
#define NPS_ACCEL_RESOLUTION (65536)
/* ms-2 */
/* aka 2^10/ACCEL_X_SENS */
#define NPS_ACCEL_SENSITIVITY_XX ACCEL_BFP_OF_REAL(-1./2.50411474)
#define NPS_ACCEL_SENSITIVITY_YY ACCEL_BFP_OF_REAL(-1./2.48126183)
#define NPS_ACCEL_SENSITIVITY_ZZ ACCEL_BFP_OF_REAL(-1./2.51396167)
#define NPS_ACCEL_NEUTRAL_X 32081
#define NPS_ACCEL_NEUTRAL_Y 33738
#define NPS_ACCEL_NEUTRAL_Z 32441
/* m2s-4 */
#define NPS_ACCEL_NOISE_STD_DEV_X 5.e-2
#define NPS_ACCEL_NOISE_STD_DEV_Y 5.e-2
#define NPS_ACCEL_NOISE_STD_DEV_Z 5.e-2
/* ms-2 */
#define NPS_ACCEL_BIAS_X 0
#define NPS_ACCEL_BIAS_Y 0
#define NPS_ACCEL_BIAS_Z 0
/* s */
#define NPS_ACCEL_DT (1./512.)
/*
* Gyrometer
*/
#define NPS_GYRO_RESOLUTION 65536
/* 2^12/GYRO_X_SENS */
#define NPS_GYRO_SENSITIVITY_PP RATE_BFP_OF_REAL( 1./1.01)
#define NPS_GYRO_SENSITIVITY_QQ RATE_BFP_OF_REAL(-1./1.01)
#define NPS_GYRO_SENSITIVITY_RR RATE_BFP_OF_REAL(-1./1.01)
#define NPS_GYRO_NEUTRAL_P 33924
#define NPS_GYRO_NEUTRAL_Q 33417
#define NPS_GYRO_NEUTRAL_R 32809
#define NPS_GYRO_NOISE_STD_DEV_P RadOfDeg(0.1)
#define NPS_GYRO_NOISE_STD_DEV_Q RadOfDeg(0.1)
#define NPS_GYRO_NOISE_STD_DEV_R RadOfDeg(0.1)
#define NPS_GYRO_BIAS_INITIAL_P RadOfDeg( 2.0)
#define NPS_GYRO_BIAS_INITIAL_Q RadOfDeg( 1.0)
#define NPS_GYRO_BIAS_INITIAL_R RadOfDeg(-5.0)
#define NPS_GYRO_BIAS_RANDOM_WALK_STD_DEV_P RadOfDeg(0.0)
#define NPS_GYRO_BIAS_RANDOM_WALK_STD_DEV_Q RadOfDeg(0.0)
#define NPS_GYRO_BIAS_RANDOM_WALK_STD_DEV_R RadOfDeg(0.0)
/* s */
#define NPS_GYRO_DT (1./512.)
/*
* Magnetometer
*/
//#define BSM_MAG_RESOLUTION 65536
#define NPS_MAG_IMU_TO_SENSOR_PHI 0.
#define NPS_MAG_IMU_TO_SENSOR_THETA 0.
#define NPS_MAG_IMU_TO_SENSOR_PSI 0.
#define NPS_MAG_SENSITIVITY_XX MAG_BFP_OF_REAL(-1./4.94075530)
#define NPS_MAG_SENSITIVITY_YY MAG_BFP_OF_REAL( 1./5.10207664)
#define NPS_MAG_SENSITIVITY_ZZ MAG_BFP_OF_REAL(-1./4.90788848)
#define NPS_MAG_NEUTRAL_X 2358
#define NPS_MAG_NEUTRAL_Y 2362
#define NPS_MAG_NEUTRAL_Z 2119
#define NPS_MAG_NOISE_STD_DEV_X 2e-3
#define NPS_MAG_NOISE_STD_DEV_Y 2e-3
#define NPS_MAG_NOISE_STD_DEV_Z 2e-3
#define NPS_MAG_DT (1./100.)
/*
* Range meter
*/
#define BSM_RANGEMETER_RESOLUTION (1024)
#define BSM_RANGEMETER_SENSITIVITY (1024. / 12.)
#define BSM_RANGEMETER_MAX_RANGE (6. * BSM_RANGEMETER_SENSITIVITY)
#define BSM_RANGEMETER_DT (1./20.)
/*
* Barometer
*/
/* m */
/* aka 2^8/INS_BARO_SENS */
#define NPS_BARO_QNH 900.
#define NPS_BARO_SENSITIVITY 17.066667
#define NPS_BARO_DT (1./100.)
#define NPS_BARO_NOISE_STD_DEV 5.e-2
/*
* GPS
*/
#ifdef GPS_PERFECT
#define NPS_GPS_SPEED_NOISE_STD_DEV 0.
#define NPS_GPS_SPEED_LATENCY 0.
#define NPS_GPS_POS_NOISE_STD_DEV 0.001
#define NPS_GPS_POS_BIAS_INITIAL_X 0.
#define NPS_GPS_POS_BIAS_INITIAL_Y 0.
#define NPS_GPS_POS_BIAS_INITIAL_Z 0.
#define NPS_GPS_POS_BIAS_RANDOM_WALK_STD_DEV_X 0.
#define NPS_GPS_POS_BIAS_RANDOM_WALK_STD_DEV_Y 0.
#define NPS_GPS_POS_BIAS_RANDOM_WALK_STD_DEV_Z 0.
#define NPS_GPS_POS_LATENCY 0.
#else
#define NPS_GPS_SPEED_NOISE_STD_DEV 1
#define NPS_GPS_SPEED_LATENCY 0.8
#define NPS_GPS_POS_NOISE_STD_DEV 2
#define NPS_GPS_POS_BIAS_INITIAL_X 0e-1
#define NPS_GPS_POS_BIAS_INITIAL_Y -0e-1
#define NPS_GPS_POS_BIAS_INITIAL_Z -0e-1
#define NPS_GPS_POS_BIAS_RANDOM_WALK_STD_DEV_X 1e-3
#define NPS_GPS_POS_BIAS_RANDOM_WALK_STD_DEV_Y 1e-3
#define NPS_GPS_POS_BIAS_RANDOM_WALK_STD_DEV_Z 1e-3
#define NPS_GPS_POS_LATENCY 0.8
#endif /* GPS_PERFECT */
#define NPS_GPS_DT (1./4.)
#endif /* NPS_SENSORS_PARAMS_H */