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https://github.com/paparazzi/paparazzi.git
synced 2026-05-26 08:22:43 +08:00
[airframes] MavTec auto2 fix and heli450
This commit is contained in:
Christophe De Wagter
@@ -140,12 +140,12 @@
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<define name="SP_MAX_R" value="250." unit="deg/s"/>
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<define name="DEADBAND_R" value="200"/>
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<!-- reference -->
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<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
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<define name="REF_ZETA_P" value="0.85"/>
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<define name="REF_OMEGA_P" value="600" unit="deg/s"/>
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<define name="REF_ZETA_P" value="0.87"/>
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<define name="REF_MAX_P" value="300." unit="deg/s"/>
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<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
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<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
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<define name="REF_ZETA_Q" value="0.85"/>
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<define name="REF_OMEGA_Q" value="600" unit="deg/s"/>
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<define name="REF_ZETA_Q" value="0.87"/>
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<define name="REF_MAX_Q" value="300." unit="deg/s"/>
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<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
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<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
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@@ -153,18 +153,18 @@
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<define name="REF_MAX_R" value="180." unit="deg/s"/>
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<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
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<!-- feedback -->
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<define name="PHI_PGAIN" value="500"/>
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<define name="PHI_DGAIN" value="130"/>
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<define name="PHI_IGAIN" value="20"/>
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<define name="THETA_PGAIN" value="500"/>
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<define name="THETA_DGAIN" value="130"/>
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<define name="THETA_IGAIN" value="20"/>
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<define name="PHI_PGAIN" value="400"/>
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<define name="PHI_DGAIN" value="100"/>
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<define name="PHI_IGAIN" value="10"/>
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<define name="THETA_PGAIN" value="400"/>
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<define name="THETA_DGAIN" value="100"/>
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<define name="THETA_IGAIN" value="10"/>
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<define name="PSI_PGAIN" value="500"/>
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<define name="PSI_DGAIN" value="90"/>
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<define name="PSI_IGAIN" value="10"/>
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<!-- feedforward -->
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<define name="PHI_DDGAIN" value="150"/>
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<define name="THETA_DDGAIN" value="150"/>
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<define name="PHI_DDGAIN" value="100"/>
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<define name="THETA_DDGAIN" value="100"/>
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<define name="PSI_DDGAIN" value="200"/>
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</section>
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@@ -0,0 +1,202 @@
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<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<airframe name="heli450">
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<description>450 sized helicopter without hiller bar.
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</description>
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<firmware name="rotorcraft">
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<target name="ap" board="lisa_m_2.0"/>
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<module name="radio_control" type="spektrum">
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<define name="RADIO_KILL_SWITCH" value="RADIO_AUX1"/>
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<define name="RADIO_MODE" value="RADIO_GEAR"/>
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<define name="RADIO_FMODE" value="RADIO_AUX2"/>
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</module>
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<module name="actuators" type="pwm"/>
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<module name="telemetry" type="xbee_api"/>
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<module name="imu" type="aspirin_v2.2"/>
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<module name="gps" type="ublox"/>
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<module name="stabilization" type="int_quat"/>
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<module name="stabilization" type="rate"/>
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<module name="ahrs" type="int_cmpl_quat"/>
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<module name="ins" type="hff"/>
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<module name="geo_mag"/>
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<module name="air_data"/>
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<module name="gps" type="ubx_ucenter"/>
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<module name="heli_swashplate_mixing"/>
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<module name="heli_throttle_curve"/>
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</firmware>
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<servos driver="Pwm">
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<servo name="THROTTLE" no="0" min="1000" neutral="1000" max="2000"/>
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<servo name="BACK" no="1" min="1050" neutral="1500" max="1950"/>
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<servo name="LEFTFRONT" no="2" min="1050" neutral="1500" max="1950"/>
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<servo name="RIGHTFRONT" no="3" min="1950" neutral="1500" max="1050"/>
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<servo name="TAIL" no="4" min="1850" neutral="1600" max="1350"/>
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</servos>
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<commands>
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<axis name="THRUST" failsafe_value="0"/>
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<axis name="COLLECTIVE" failsafe_value="0"/>
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<axis name="ROLL" failsafe_value="0"/>
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<axis name="PITCH" failsafe_value="0"/>
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<axis name="YAW" failsafe_value="0"/>
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<axis name="FMODE" failsafe_value="0"/>
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</commands>
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<rc_commands>
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<set command="THRUST" value="@THROTTLE"/>
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<set command="ROLL" value="@ROLL"/>
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<set command="PITCH" value="@PITCH"/>
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<set command="YAW" value="@YAW"/>
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<set command="FMODE" value="@AUX2"/>
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</rc_commands>
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<section name="MIXING" prefix="SW_MIXING_">
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<!-- front left (CW), front right (CCW), back right (CW), back left (CCW) -->
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<define name="TYPE" value="HR120"/>
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<define name="TRIM_ROLL" value="0"/>
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<define name="TRIM_PITCH" value="0"/>
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<define name="TRIM_COLL" value="0"/>
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</section>
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<command_laws>
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<call fun="swashplate_mixing_run(values)"/>
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<set servo="THROTTLE" value="throttle_curve.throttle"/>
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<set servo="BACK" value="swashplate_mixing.commands[SW_BACK]"/>
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<set servo="LEFTFRONT" value="swashplate_mixing.commands[SW_LEFTFRONT]"/>
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<set servo="RIGHTFRONT" value="swashplate_mixing.commands[SW_RIGHTFRONT]"/>
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<set servo="TAIL" value="@YAW + throttle_curve.throttle*2800/7000"/>
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</command_laws>
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<heli_curves>
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<curve throttle="0,4800,7200,8400,9600" collective="-1000,750,2500,4250,6000"/>
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<curve throttle="9600,7200,9600" collective="-7500,0,7500"/>
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</heli_curves>
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<section name="MISC">
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<define name="NAV_CLIMB_VSPEED" value="2.5"/>
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<define name="NAV_DESCEND_VSPEED" value="-1.0"/>
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<define name="NO_RC_THRUST_LIMIT" value="TRUE"/>
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</section>
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<section name="IMU" prefix="IMU_">
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<define name="ACCEL_X_NEUTRAL" value="11"/>
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<define name="ACCEL_Y_NEUTRAL" value="11"/>
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<define name="ACCEL_Z_NEUTRAL" value="-25"/>
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<!-- replace this with your own calibration -->
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<define name="MAG_X_NEUTRAL" value="14"/>
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<define name="MAG_Y_NEUTRAL" value="116"/>
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<define name="MAG_Z_NEUTRAL" value="119"/>
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<define name="MAG_X_SENS" value="5.09245681612" integer="16"/>
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<define name="MAG_Y_SENS" value="5.29702744632" integer="16"/>
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<define name="MAG_Z_SENS" value="5.65287938992" integer="16"/>
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<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
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<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
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<define name="BODY_TO_IMU_PSI" value="-90." unit="deg"/>
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</section>
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<section name="AHRS" prefix="AHRS_">
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<!--This airframe vibrates a lot, which causes accel measurements in excess of 1g continuously-->
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<define name="GRAVITY_HEURISTIC_FACTOR" value="0"/>
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<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
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<define name="H_X" value="0.3770441"/>
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<define name="H_Y" value="0.0193986"/>
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<define name="H_Z" value="0.9259921"/>
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</section>
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<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
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<!-- setpoints -->
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<define name="SP_MAX_P" unit="deg/s" value="280"/>
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<define name="SP_MAX_Q" unit="deg/s" value="280"/>
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<define name="SP_MAX_R" unit="deg/s" value="140"/>
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<define name="DEADBAND_P" value="20"/>
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<define name="DEADBAND_Q" value="20"/>
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<define name="DEADBAND_R" value="200"/>
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<!-- feedback -->
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<define name="GAIN_P" value="800"/>
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<define name="GAIN_Q" value="800"/>
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<define name="GAIN_R" value="700"/>
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<define name="IGAIN_P" value="240"/>
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<define name="IGAIN_Q" value="240"/>
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<define name="IGAIN_R" value="160"/>
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</section>
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<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
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<!-- setpoints -->
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<define name="SP_MAX_PHI" value="65." unit="deg"/>
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<define name="SP_MAX_THETA" value="65." unit="deg"/>
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<define name="SP_MAX_R" value="250." unit="deg/s"/>
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<define name="DEADBAND_R" value="200"/>
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<!-- reference -->
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<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
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<define name="REF_ZETA_P" value="0.85"/>
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<define name="REF_MAX_P" value="300." unit="deg/s"/>
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<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
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<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
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<define name="REF_ZETA_Q" value="0.85"/>
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<define name="REF_MAX_Q" value="300." unit="deg/s"/>
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<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
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<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
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<define name="REF_ZETA_R" value="0.85"/>
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<define name="REF_MAX_R" value="180." unit="deg/s"/>
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<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
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<!-- feedback -->
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<define name="PHI_PGAIN" value="900"/>
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<define name="PHI_DGAIN" value="200"/>
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<define name="PHI_IGAIN" value="200"/>
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<define name="THETA_PGAIN" value="900"/>
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<define name="THETA_DGAIN" value="200"/>
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<define name="THETA_IGAIN" value="200"/>
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<define name="PSI_PGAIN" value="900"/>
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<define name="PSI_DGAIN" value="200"/>
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<define name="PSI_IGAIN" value="10"/>
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<!-- feedforward -->
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<define name="PHI_DDGAIN" value=" 200"/>
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<define name="THETA_DDGAIN" value=" 200"/>
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<define name="PSI_DDGAIN" value=" 200"/>
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</section>
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<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
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<define name="HOVER_KP" value="150"/>
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<define name="HOVER_KD" value="80"/>
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<define name="HOVER_KI" value="20"/>
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<define name="NOMINAL_HOVER_THROTTLE" value="0.5"/>
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<define name="ADAPT_THROTTLE_ENABLED" value="TRUE"/>
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</section>
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<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
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<define name="MAX_BANK" value="35" unit="deg"/>
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<define name="USE_SPEED_REF" value="TRUE"/>
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<define name="PGAIN" value="50"/>
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<define name="DGAIN" value="100"/>
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<define name="AGAIN" value="70"/>
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<define name="IGAIN" value="20"/>
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</section>
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<section name="AUTOPILOT">
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<define name="MODE_MANUAL" value="AP_MODE_RC_DIRECT"/>
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<define name="MODE_AUTO1" value="AP_MODE_HOVER_Z_HOLD"/>
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<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
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</section>
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<section name="BAT">
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<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
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<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/>
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<define name="LOW_BAT_LEVEL" value="10.1" unit="V"/>
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<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/>
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</section>
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</airframe>
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@@ -179,6 +179,17 @@
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gui_color="white"
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release="65aa9a711dc4a66ed2d7cf73c0f5872bbeeb821d"
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/>
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<aircraft
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name="Heli450"
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ac_id="8"
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airframe="airframes/tudelft/heli450.xml"
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radio="radios/dummy.xml"
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telemetry="telemetry/default_rotorcraft.xml"
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flight_plan="flight_plans/rotorcraft_basic.xml"
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settings=""
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settings_modules="modules/heli_throttle_curve.xml modules/gps_ubx_ucenter.xml modules/air_data.xml modules/geo_mag.xml modules/ahrs_int_cmpl_quat.xml modules/stabilization_rate.xml modules/stabilization_int_quat.xml modules/nav_basic_rotorcraft.xml modules/guidance_rotorcraft.xml modules/gps.xml modules/imu_common.xml"
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gui_color="blue"
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/>
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<aircraft
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name="Iris"
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ac_id="66"
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@@ -232,7 +243,7 @@
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airframe="airframes/CDW/cdw_mavtec.xml"
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radio="radios/R6107SP_7ch.xml"
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telemetry="telemetry/default_rotorcraft.xml"
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flight_plan="flight_plans/tudelft/rotorcraft_survey_imav2015_competition.xml"
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flight_plan="flight_plans/rotorcraft_basic.xml"
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settings="settings/rotorcraft_basic.xml settings/modules/config_asctec_v2.xml"
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settings_modules="modules/geo_mag.xml modules/nav_survey_poly_rotorcraft.xml modules/nav_survey_rectangle_rotorcraft.xml modules/gps_ubx_ucenter.xml modules/switch_servo.xml modules/ahrs_float_mlkf.xml modules/stabilization_int_quat.xml modules/nav_basic_rotorcraft.xml modules/guidance_rotorcraft.xml modules/gps.xml modules/imu_common.xml"
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gui_color="blue"
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