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[conf] create an examples directory for airframes

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This commit is contained in:
Gautier Hattenberger
2012-05-09 00:29:54 +02:00
parent 09490b374c
commit 093f894567
19 changed files with 656 additions and 10 deletions
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conf/airframes/examples/airframe.dtd
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../airframe.dtd
conf/airframes/examples/booz2.xml
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<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>
<!-- not needed anymore - in subsystem -->
<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_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_NEUTRAL" value="32081"/>
<define name="ACCEL_Y_NEUTRAL" value="33738"/>
<define name="ACCEL_Z_NEUTRAL" value="32441"/>
<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="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_X_SIGN" value="-1"/>
<define name="MAG_Y_SIGN" value=" 1"/>
<define name="MAG_Z_SIGN" value="-1"/>
<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="4." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="3." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
<!--
<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="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="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="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="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="GUIDANCE_H_">
<define name="PGAIN" value="100"/>
<define name="DGAIN" value="100"/>
<define name="IGAIN" value="0"/>
</section>
<section name="BAT">
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
</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="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>
<firmware name="rotorcraft">
<target name="ap" board="booz_1.0"/>
<target name="sim" board="pc">
<subsystem name="fdm" type="nps"/>
</target>
<subsystem name="radio_control" type="ppm"/>
<subsystem name="telemetry" type="transparent"/>
<subsystem name="actuators" type="mkk"/>
<subsystem name="imu" type="b2_v1.0"/>
<subsystem name="gps" type="ublox"/>
<subsystem name="stabilization" type="euler"/>
<subsystem name="ahrs" type="int_cmpl_euler"/>
<subsystem name="ins" type="hff"/>
</firmware>
</airframe>
conf/airframes/delta_wing_minimal_example.xml → conf/airframes/examples/delta_wing_minimal.xml
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conf/airframes/demo.xml → conf/airframes/examples/demo.xml
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conf/airframes/demo_module.xml → conf/airframes/examples/demo_module.xml
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conf/airframes/easy_glider_example.xml → conf/airframes/examples/easy_glider.xml
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@@ -1,4 +1,4 @@
<!DOCTYPE airframe SYSTEM "./airframe.dtd"> <!DOCTYPE airframe SYSTEM "airframe.dtd">
<airframe name="Easy Glider Tiny 0.99"> <airframe name="Easy Glider Tiny 0.99">
conf/airframes/easystar_example.xml → conf/airframes/examples/easystar.xml
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conf/airframes/easystar_ets_example.xml → conf/airframes/examples/easystar_ets.xml
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conf/airframes/funjet_example.xml → conf/airframes/examples/funjet.xml
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conf/airframes/funjet_cam_example.xml → conf/airframes/examples/funjet_cam.xml
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conf/airframes/examples/h_hex.xml
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<!-- this is a custom hexa Lisa/L#3 and mikrokopter controllers -->
<airframe name="booz2_a6">
<servos min="0" neutral="0" max="0xff">
<servo name="BACK_RIGHT" no="0" min="0" neutral="0" max="255"/>
<servo name="BACK_LEFT" no="1" min="0" neutral="0" max="255"/>
<servo name="CENTER_RIGHT" no="2" min="0" neutral="0" max="255"/>
<servo name="CENTER_LEFT" no="3" min="0" neutral="0" max="255"/>
<servo name="FRONT_RIGHT" no="4" min="0" neutral="0" max="255"/>
<servo name="FRONT_LEFT" no="5" 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="6"/>
<define name="ADDR" value="{ 0x52, 0x54, 0x56, 0x58, 0x5A, 0X5C }"/>
</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="6"/>
<define name="SCALE" value="256"/>
<define name="ROLL_COEF" value="{ -69, 69, -256, 256, -186, 186 }"/>
<define name="PITCH_COEF" value="{ -256, -256, 0, 0, 256, 256 }"/>
<define name="YAW_COEF" value="{ -153, 153, 256, -256, -115, 115 }"/>
<define name="THRUST_COEF" value="{ 256, 256, 256, 256, 256, 256 }"/>
</section>
<section name="IMU" prefix="IMU_">
<define name="GYRO_P_NEUTRAL" value="31948"/>
<define name="GYRO_Q_NEUTRAL" value="31834"/>
<define name="GYRO_R_NEUTRAL" value="32687"/>
<define name="GYRO_P_SENS" value=" 1.101357422" integer="16"/>
<define name="GYRO_Q_SENS" value=" 1.122670898" integer="16"/>
<define name="GYRO_R_SENS" value=" 1.104890137" integer="16"/>
<define name="ACCEL_X_SENS" value=" 2.58273701242" integer="16"/>
<define name="ACCEL_Y_SENS" value=" 2.54076215332" integer="16"/>
<define name="ACCEL_Z_SENS" value=" 2.57633620646" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="32857"/>
<define name="ACCEL_Y_NEUTRAL" value="32429"/>
<define name="ACCEL_Z_NEUTRAL" value="32593"/>
<define name="MAG_X_SENS" value=" 5.32718104135" integer="16"/>
<define name="MAG_Y_SENS" value=" 4.87857821202" integer="16"/>
<define name="MAG_Z_SENS" value=" 3.11986612709" integer="16"/>
<define name="MAG_X_NEUTRAL" value="-43"/>
<define name="MAG_Y_NEUTRAL" value=" 49"/>
<define name="MAG_Z_NEUTRAL" value="-66"/>
<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_DIRECT"/>
<define name="MODE_AUTO2" value="AP_MODE_ATTITUDE_DIRECT"/>
</section>
<section name="BAT">
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" 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="0.85"/>
<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="0.85"/>
<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="0.85"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="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="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="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="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>
<firmware name="rotorcraft">
<target name="ap" board="lisa_l_1.0">
<!-- <define name="ACTUATORS_START_DELAY" value="1"/> -->
<subsystem name="radio_control" type="spektrum"/>
<subsystem name="actuators" type="mkk"/>
</target>
<subsystem name="telemetry" type="transparent"/>
<!-- <subsystem name="imu" type="b2_v1.1"/> -->
<subsystem name="imu" type="aspirin_v1.0"/>
<subsystem name="gps" type="ublox"/>
<subsystem name="stabilization" type="euler"/>
<subsystem name="ahrs" type="int_cmpl_euler"/>
</firmware>
<firmware name="lisa_test_progs">
<target name="test_telemetry" board="lisa_l_1.0"/>
<target name="test_baro" board="lisa_l_1.0"/>
<target name="test_imu_b2" board="lisa_l_1.0"/>
<target name="test_imu_aspirin" board="lisa_l_1.0"/>
<target name="test_rc_spektrum" board="lisa_l_1.0"/>
<target name="test_rc_ppm" board="lisa_l_1.0"/>
<target name="test_adc" board="lisa_l_1.0"/>
<target name="test_hmc5843" board="lisa_l_1.0"/>
<target name="test_itg3200" board="lisa_l_1.0"/>
<target name="test_adxl345" board="lisa_l_1.0"/>
<target name="test_esc_mkk_simple" board="lisa_l_1.0"/>
<target name="test_esc_asctecv1_simple" board="lisa_l_1.0"/>
<target name="test_actuators_mkk" board="lisa_l_1.0"/>
<target name="test_actuators_asctecv1" board="lisa_l_1.0"/>
</firmware>
</airframe>
conf/airframes/examples/lisa_asctec.xml
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<!-- this is an asctec frame equiped with Lisa/L#3 and asctec V2 controllers -->
<airframe name="lisa_asctec">
<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="LEFT" no="2" min="0" neutral="0" max="255"/>
<servo name="RIGHT" 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>
<!-- for the sim -->
<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="3"/>
<define name="MAX_MOTOR" value="200"/>
<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_NEUTRAL" value="32276"/>
<define name="GYRO_Q_NEUTRAL" value="33987"/>
<define name="GYRO_R_NEUTRAL" value="32801"/>
<define name="GYRO_P_SENS" value="0.92466" integer="16"/>
<define name="GYRO_Q_SENS" value="0.93226" integer="16"/>
<define name="GYRO_R_SENS" value="0.92943" 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="25875"/>
<define name="ACCEL_Y_NEUTRAL" value="26273"/>
<define name="ACCEL_Z_NEUTRAL" value="26152"/>
<define name="ACCEL_X_SENS" value="1.8788156268" integer="16"/>
<define name="ACCEL_Y_SENS" value="1.88941543145" integer="16"/>
<define name="ACCEL_Z_SENS" value="1.90349115464" 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="45. " 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_">
<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="0.85"/>
<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="0.85"/>
<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="0.85"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="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="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="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="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="{&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>
<modules main_freq="512">
<!--load name="vehicle_interface_overo_link.xml"/-->
</modules>
<firmware name="rotorcraft">
<target name="ap" board="lisa_l_1.1">
<!-- <define name="ACTUATORS_START_DELAY" value="1"/> -->
<subsystem name="radio_control" type="spektrum"/>
<subsystem name="actuators" type="asctec_v2"/>
<subsystem name="telemetry" type="transparent"/>
<define name="RADIO_MODE" value="RADIO_AUX2"/>
<define name="RADIO_KILL_SWITCH" value="RADIO_GEAR"/>
<define name="RADIO_CONTROL_SPEKTRUM_SIGNS" value="\{1,1,-1,1,-1,-1,-1,1,1,1,1,1\}"/>
</target>
<target name="sim" board="pc">
<subsystem name="fdm" type="nps"/>
<subsystem name="radio_control" type="ppm"/>
<subsystem name="actuators" type="mkk"/>
</target>
<subsystem name="imu" type="b2_v1.1"/>
<subsystem name="gps" type="ublox"/>
<subsystem name="stabilization" type="euler"/>
<subsystem name="ahrs" type="int_cmpl_euler"/>
</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>
</airframe>
conf/airframes/microjet_example.xml → conf/airframes/examples/microjet.xml
View File
conf/airframes/quadrotor_lisa_m_2_pwm_example.xml → conf/airframes/examples/quadrotor_lisa_m_2_pwm.xml
View File
conf/airframes/quadrotor_lisa_m_mkk_example.xml → conf/airframes/examples/quadrotor_lisa_m_mkk.xml
View File
conf/airframes/twinjet_example.xml → conf/airframes/examples/twinjet.xml
View File
conf/airframes/twinstar_example.xml → conf/airframes/examples/twinstar.xml
View File
conf/airframes/example_twog_analogimu.xml → conf/airframes/examples/twog_analogimu.xml
View File
conf/conf.xml.example
+9 -9
View File
@@ -4,9 +4,9 @@
<!-- booz2 --> <!-- booz2 -->
<aircraft <aircraft
name="BOOZ2_A1" name="BOOZ2"
ac_id="150" ac_id="150"
airframe="airframes/Poine/booz2_a1.xml" airframe="airframes/examples/booz2.xml"
radio="radios/cockpitSX.xml" radio="radios/cockpitSX.xml"
telemetry="telemetry/default_rotorcraft.xml" telemetry="telemetry/default_rotorcraft.xml"
flight_plan="flight_plans/dummy.xml" flight_plan="flight_plans/dummy.xml"
@@ -18,7 +18,7 @@
<aircraft <aircraft
name="Hexa_LisaL" name="Hexa_LisaL"
ac_id="153" ac_id="153"
airframe="airframes/Poine/h_hex.xml" airframe="airframes/examples/h_hex.xml"
radio="radios/cockpitSX.xml" radio="radios/cockpitSX.xml"
telemetry="telemetry/default_rotorcraft.xml" telemetry="telemetry/default_rotorcraft.xml"
flight_plan="flight_plans/dummy.xml" flight_plan="flight_plans/dummy.xml"
@@ -26,9 +26,9 @@
gui_color="white" gui_color="white"
/> />
<aircraft <aircraft
name="LISA_ASCTEC_PIOTR" name="LISA_ASCTEC"
ac_id="161" ac_id="161"
airframe="airframes/esden/lisa_asctec.xml" airframe="airframes/examples/lisa_asctec.xml"
radio="radios/cockpitSX.xml" radio="radios/cockpitSX.xml"
telemetry="telemetry/default_rotorcraft.xml" telemetry="telemetry/default_rotorcraft.xml"
flight_plan="flight_plans/dummy.xml" flight_plan="flight_plans/dummy.xml"
@@ -40,7 +40,7 @@
<aircraft <aircraft
name="Microjet" name="Microjet"
ac_id="5" ac_id="5"
airframe="airframes/microjet_example.xml" airframe="airframes/examples/microjet.xml"
radio="radios/cockpitMM.xml" radio="radios/cockpitMM.xml"
telemetry="telemetry/default_fixedwing.xml" telemetry="telemetry/default_fixedwing.xml"
flight_plan="flight_plans/basic.xml" flight_plan="flight_plans/basic.xml"
@@ -50,7 +50,7 @@
<aircraft <aircraft
name="Tiny_IMU" name="Tiny_IMU"
ac_id="7" ac_id="7"
airframe="airframes/example_twog_analogimu.xml" airframe="airframes/examples/twog_analogimu.xml"
radio="radios/cockpitSX.xml" radio="radios/cockpitSX.xml"
telemetry="telemetry/default_fixedwing_imu.xml" telemetry="telemetry/default_fixedwing_imu.xml"
flight_plan="flight_plans/versatile.xml" flight_plan="flight_plans/versatile.xml"
@@ -60,7 +60,7 @@
<aircraft <aircraft
name="Twinjet" name="Twinjet"
ac_id="6" ac_id="6"
airframe="airframes/twinjet_example.xml" airframe="airframes/examples/twinjet.xml"
radio="radios/cockpitMM.xml" radio="radios/cockpitMM.xml"
telemetry="telemetry/default_fixedwing.xml" telemetry="telemetry/default_fixedwing.xml"
flight_plan="flight_plans/versatile.xml" flight_plan="flight_plans/versatile.xml"
@@ -70,7 +70,7 @@
<aircraft <aircraft
name="EasyStar_ETS" name="EasyStar_ETS"
ac_id="8" ac_id="8"
airframe="airframes/easystar_ets_example.xml" airframe="airframes/examples/easystar_ets.xml"
radio="radios/cockpitSX.xml" radio="radios/cockpitSX.xml"
telemetry="telemetry/default_fixedwing.xml" telemetry="telemetry/default_fixedwing.xml"
flight_plan="flight_plans/versatile.xml" flight_plan="flight_plans/versatile.xml"