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Merge pull request #209 'fixedwing_ins'
tried to clean ins xsens subsystem up a little for fixedwings * removed the AhrsEvent * removed all ahrs things from ins_xsens * added an InsEvent for fixedwings * removed some gps stuff from ins_xsens and used the normal gps callbacks instead * made baud rate for xsens configurable To use the XSens MTi-G as a full INS (with the xsens GPS): ```xml <subsystem name="ins" type="xsens"> <configure name="XSENS_UART_NR" value="3"/> <configure name="XSENS_UART_BAUD" value="B115200"/> </subsystem> ``` to use it only as an IMU (still need to add an AHRS algorithm and other GPS as usual) ```xml <subsystem name="imu" type="xsens"> <configure name="XSENS_UART_NR" value="3"/> <configure name="XSENS_UART_BAUD" value="B115200"/> </subsystem> ```
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Original file line number | Diff line number | Diff line change |
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<!DOCTYPE airframe SYSTEM "../airframe.dtd"> | ||
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<!-- Microjet Multiplex (http://www.multiplex-rc.de/) | ||
Lisa/M v1.0 board (http://paparazzi.enac.fr/wiki/Lisa/M_v10) | ||
Xsens running as IMU | ||
Xbee modem in transparent mode | ||
--> | ||
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<airframe name="Microjet Lisa/M 1.0"> | ||
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<firmware name="fixedwing"> | ||
<target name="sim" board="pc"/> | ||
<target name="ap" board="lisa_m_1.0"/> | ||
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<define name="AGR_CLIMB" /> | ||
<define name="LOITER_TRIM" /> | ||
<define name="ALT_KALMAN" /> | ||
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<subsystem name="radio_control" type="ppm"/> | ||
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<!-- Communication --> | ||
<subsystem name="telemetry" type="transparent"/> | ||
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<!-- Sensors --> | ||
<subsystem name="imu" type="xsens"> | ||
<configure name="XSENS_UART_NR" value="3"/> | ||
<configure name="XSENS_UART_BAUD" value="B115200"/> | ||
</subsystem> | ||
<subsystem name="ahrs" type="int_cmpl_quat"/> | ||
<subsystem name="gps" type="ublox"/> | ||
<subsystem name="control"/> | ||
<subsystem name="navigation"/> | ||
</firmware> | ||
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<modules> | ||
<load name="sys_mon.xml"/> | ||
</modules> | ||
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<servos> | ||
<servo name="MOTOR" no="0" min="1290" neutral="1290" max="1810"/> | ||
<servo name="AILEVON_LEFT" no="1" min="2000" neutral="1510" max="1000"/> | ||
<servo name="AILEVON_RIGHT" no="3" min="1000" neutral="1535" max="2000"/> | ||
</servos> | ||
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<commands> | ||
<axis name="THROTTLE" failsafe_value="0"/> | ||
<axis name="ROLL" failsafe_value="0"/> | ||
<axis name="PITCH" failsafe_value="0"/> | ||
</commands> | ||
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<rc_commands> | ||
<set command="THROTTLE" value="@THROTTLE"/> | ||
<set command="ROLL" value="@ROLL"/> | ||
<set command="PITCH" value="@PITCH"/> | ||
</rc_commands> | ||
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<section name="MIXER"> | ||
<define name="AILEVON_AILERON_RATE" value="0.75"/> | ||
<define name="AILEVON_ELEVATOR_RATE" value="0.75"/> | ||
</section> | ||
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<command_laws> | ||
<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/> | ||
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/> | ||
<set servo="MOTOR" value="@THROTTLE"/> | ||
<set servo="AILEVON_LEFT" value="$elevator - $aileron"/> | ||
<set servo="AILEVON_RIGHT" value="$elevator + $aileron"/> | ||
</command_laws> | ||
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<section name="IMU" prefix="IMU_"> | ||
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<define name="GYRO_P_SIGN" value="1"/> | ||
<define name="GYRO_Q_SIGN" value="1"/> | ||
<define name="GYRO_R_SIGN" value="1"/> | ||
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<define name="GYRO_P_NEUTRAL" value="0"/> | ||
<define name="GYRO_R_NEUTRAL" value="0"/> | ||
<define name="GYRO_Q_NEUTRAL" value="0"/> | ||
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<define name="GYRO_P_SENS" value="1" integer="16"/> | ||
<define name="GYRO_R_SENS" value="1" integer="16"/> | ||
<define name="GYRO_Q_SENS" value="1" integer="16"/> | ||
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<define name="ACCEL_X_SIGN" value="1"/> | ||
<define name="ACCEL_Y_SIGN" value="1"/> | ||
<define name="ACCEL_Z_SIGN" value="1"/> | ||
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<define name="ACCEL_X_SENS" value="1" integer="16"/> | ||
<define name="ACCEL_Z_SENS" value="1" integer="16"/> | ||
<define name="ACCEL_Y_SENS" value="1" integer="16"/> | ||
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<define name="ACCEL_X_NEUTRAL" value="0"/> | ||
<define name="ACCEL_Z_NEUTRAL" value="0"/> | ||
<define name="ACCEL_Y_NEUTRAL" value="0"/> | ||
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<define name="MAG_X_SIGN" value="1"/> | ||
<define name="MAG_Y_SIGN" value="1"/> | ||
<define name="MAG_Z_SIGN" value="1"/> | ||
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<define name="MAG_X_NEUTRAL" value="-45"/> | ||
<define name="MAG_Y_NEUTRAL" value="334"/> | ||
<define name="MAG_Z_NEUTRAL" value="7"/> | ||
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<define name="MAG_X_SENS" value="4.47647816128" integer="16"/> | ||
<define name="MAG_Y_SENS" value="4.71085671542" integer="16"/> | ||
<define name="MAG_Z_SENS" value="4.41585354498" integer="16"/> | ||
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<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> | ||
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<section name="AHRS" prefix="AHRS_"> | ||
<!-- replace this with your local magnetic field --> | ||
<define name="H_X" value="0.3770441"/> | ||
<define name="H_Y" value="0.0193986"/> | ||
<define name="H_Z" value="0.9259921"/> | ||
</section> | ||
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<section name="INS" prefix="INS_"> | ||
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/> | ||
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/> | ||
</section> | ||
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<section name="VERTICAL CONTROL" prefix="V_CTL_"> | ||
<define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/> | ||
<!-- outer loop proportional gain --> | ||
<define name="ALTITUDE_PGAIN" value="0.03"/> | ||
<!-- outer loop saturation --> | ||
<define name="ALTITUDE_MAX_CLIMB" value="2."/> | ||
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<!-- auto throttle inner loop --> | ||
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.32"/> | ||
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/> | ||
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.65"/> | ||
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1500"/> | ||
<define name="AUTO_THROTTLE_DASH_TRIM" value="-4000"/> | ||
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.15" unit="%/(m/s)"/> | ||
<define name="AUTO_THROTTLE_PGAIN" value="0.01"/> | ||
<define name="AUTO_THROTTLE_IGAIN" value="0.1"/> | ||
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/> | ||
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<define name="THROTTLE_SLEW_LIMITER" value="2" unit="s"/> | ||
</section> | ||
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<section name="HORIZONTAL CONTROL" prefix="H_CTL_"> | ||
<define name="COURSE_PGAIN" value="1.0"/> | ||
<define name="COURSE_DGAIN" value="0.3"/> | ||
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<define name="ROLL_MAX_SETPOINT" value="35" unit="deg"/> | ||
<define name="PITCH_MAX_SETPOINT" value="30" unit="deg"/> | ||
<define name="PITCH_MIN_SETPOINT" value="-30" unit="deg"/> | ||
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<define name="PITCH_PGAIN" value="12000."/> | ||
<define name="PITCH_DGAIN" value="1.5"/> | ||
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<define name="ELEVATOR_OF_ROLL" value="1250"/> | ||
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<define name="ROLL_SLEW" value="0.1"/> | ||
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<define name="ROLL_ATTITUDE_GAIN" value="7500"/> | ||
<define name="ROLL_RATE_GAIN" value="1500"/> | ||
</section> | ||
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<section name="AGGRESSIVE" prefix="AGR_"> | ||
<define name="BLEND_START" value="20"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!--> | ||
<define name="BLEND_END" value="10"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!--> | ||
<define name="CLIMB_THROTTLE" value="1.00"/><!-- Gaz for Aggressive Climb --> | ||
<define name="CLIMB_PITCH" value="0.3"/><!-- Pitch for Aggressive Climb --> | ||
<define name="DESCENT_THROTTLE" value="0.1"/><!-- Gaz for Aggressive Decent --> | ||
<define name="DESCENT_PITCH" value="-0.25"/><!-- Pitch for Aggressive Decent --> | ||
<define name="CLIMB_NAV_RATIO" value="0.8"/><!-- Percent Navigation for Altitude Error Equal to Start Altitude --> | ||
<define name="DESCENT_NAV_RATIO" value="1.0"/> | ||
</section> | ||
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<section name="FAILSAFE" prefix="FAILSAFE_"> | ||
<define name="DELAY_WITHOUT_GPS" value="2" unit="s"/> | ||
<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/> | ||
<define name="DEFAULT_ROLL" value="0.3" unit="rad"/> | ||
<define name="DEFAULT_PITCH" value="0.5" unit="rad"/> | ||
</section> | ||
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<section name="AUTO1" prefix="AUTO1_"> | ||
<define name="MAX_ROLL" value="40." unit="deg"/> | ||
<define name="MAX_PITCH" value="35." unit="deg"/> | ||
</section> | ||
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<section name="BAT"> | ||
<define name="MILLIAMP_AT_FULL_THROTTLE" value="2000"/> | ||
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/> | ||
<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/> | ||
<define name="LOW_BAT_LEVEL" value="9.7" unit="V"/> | ||
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/> | ||
</section> | ||
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<section name="MISC"> | ||
<define name="NOMINAL_AIRSPEED" value="13." unit="m/s"/> | ||
<define name="CARROT" value="5." unit="s"/> | ||
<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/> | ||
<define name="CONTROL_RATE" value="60" unit="Hz"/> | ||
<define name="ALT_KALMAN_ENABLED" value="TRUE"/> | ||
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/> | ||
</section> | ||
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</airframe> |
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Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,160 @@ | ||
<!DOCTYPE airframe SYSTEM "../airframe.dtd"> | ||
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<!-- Microjet Multiplex (http://www.multiplex-rc.de/) | ||
Lisa/M v1.0 board (http://paparazzi.enac.fr/wiki/Lisa/M_v10) | ||
Xsens as full INS | ||
Xbee modem in transparent mode | ||
--> | ||
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<airframe name="Microjet Lisa/M 1.0"> | ||
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<firmware name="fixedwing"> | ||
<target name="sim" board="pc"/> | ||
<target name="ap" board="lisa_m_1.0"/> | ||
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<define name="AGR_CLIMB" /> | ||
<define name="LOITER_TRIM" /> | ||
<define name="ALT_KALMAN" /> | ||
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<subsystem name="radio_control" type="ppm"/> | ||
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<!-- Communication --> | ||
<subsystem name="telemetry" type="transparent"/> | ||
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<!-- Sensors --> | ||
<subsystem name="ins" type="xsens"> | ||
<configure name="XSENS_UART_NR" value="3"/> | ||
<configure name="XSENS_UART_BAUD" value="B115200"/> | ||
</subsystem> | ||
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<subsystem name="control"/> | ||
<subsystem name="navigation"/> | ||
</firmware> | ||
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<modules> | ||
<load name="sys_mon.xml"/> | ||
</modules> | ||
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<servos> | ||
<servo name="MOTOR" no="0" min="1290" neutral="1290" max="1810"/> | ||
<servo name="AILEVON_LEFT" no="1" min="2000" neutral="1510" max="1000"/> | ||
<servo name="AILEVON_RIGHT" no="3" min="1000" neutral="1535" max="2000"/> | ||
</servos> | ||
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<commands> | ||
<axis name="THROTTLE" failsafe_value="0"/> | ||
<axis name="ROLL" failsafe_value="0"/> | ||
<axis name="PITCH" failsafe_value="0"/> | ||
</commands> | ||
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<rc_commands> | ||
<set command="THROTTLE" value="@THROTTLE"/> | ||
<set command="ROLL" value="@ROLL"/> | ||
<set command="PITCH" value="@PITCH"/> | ||
</rc_commands> | ||
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<section name="MIXER"> | ||
<define name="AILEVON_AILERON_RATE" value="0.75"/> | ||
<define name="AILEVON_ELEVATOR_RATE" value="0.75"/> | ||
</section> | ||
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<command_laws> | ||
<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/> | ||
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/> | ||
<set servo="MOTOR" value="@THROTTLE"/> | ||
<set servo="AILEVON_LEFT" value="$elevator - $aileron"/> | ||
<set servo="AILEVON_RIGHT" value="$elevator + $aileron"/> | ||
</command_laws> | ||
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<section name="IMU" prefix="IMU_"> | ||
<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> | ||
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<section name="INS" prefix="INS_"> | ||
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/> | ||
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/> | ||
</section> | ||
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<section name="VERTICAL CONTROL" prefix="V_CTL_"> | ||
<define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/> | ||
<!-- outer loop proportional gain --> | ||
<define name="ALTITUDE_PGAIN" value="0.03"/> | ||
<!-- outer loop saturation --> | ||
<define name="ALTITUDE_MAX_CLIMB" value="2."/> | ||
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<!-- auto throttle inner loop --> | ||
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.32"/> | ||
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/> | ||
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.65"/> | ||
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1500"/> | ||
<define name="AUTO_THROTTLE_DASH_TRIM" value="-4000"/> | ||
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.15" unit="%/(m/s)"/> | ||
<define name="AUTO_THROTTLE_PGAIN" value="0.01"/> | ||
<define name="AUTO_THROTTLE_IGAIN" value="0.1"/> | ||
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/> | ||
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<define name="THROTTLE_SLEW_LIMITER" value="2" unit="s"/> | ||
</section> | ||
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<section name="HORIZONTAL CONTROL" prefix="H_CTL_"> | ||
<define name="COURSE_PGAIN" value="1.0"/> | ||
<define name="COURSE_DGAIN" value="0.3"/> | ||
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<define name="ROLL_MAX_SETPOINT" value="35" unit="deg"/> | ||
<define name="PITCH_MAX_SETPOINT" value="30" unit="deg"/> | ||
<define name="PITCH_MIN_SETPOINT" value="-30" unit="deg"/> | ||
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<define name="PITCH_PGAIN" value="12000."/> | ||
<define name="PITCH_DGAIN" value="1.5"/> | ||
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<define name="ELEVATOR_OF_ROLL" value="1250"/> | ||
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<define name="ROLL_SLEW" value="0.1"/> | ||
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<define name="ROLL_ATTITUDE_GAIN" value="7500"/> | ||
<define name="ROLL_RATE_GAIN" value="1500"/> | ||
</section> | ||
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<section name="AGGRESSIVE" prefix="AGR_"> | ||
<define name="BLEND_START" value="20"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!--> | ||
<define name="BLEND_END" value="10"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!--> | ||
<define name="CLIMB_THROTTLE" value="1.00"/><!-- Gaz for Aggressive Climb --> | ||
<define name="CLIMB_PITCH" value="0.3"/><!-- Pitch for Aggressive Climb --> | ||
<define name="DESCENT_THROTTLE" value="0.1"/><!-- Gaz for Aggressive Decent --> | ||
<define name="DESCENT_PITCH" value="-0.25"/><!-- Pitch for Aggressive Decent --> | ||
<define name="CLIMB_NAV_RATIO" value="0.8"/><!-- Percent Navigation for Altitude Error Equal to Start Altitude --> | ||
<define name="DESCENT_NAV_RATIO" value="1.0"/> | ||
</section> | ||
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<section name="FAILSAFE" prefix="FAILSAFE_"> | ||
<define name="DELAY_WITHOUT_GPS" value="2" unit="s"/> | ||
<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/> | ||
<define name="DEFAULT_ROLL" value="0.3" unit="rad"/> | ||
<define name="DEFAULT_PITCH" value="0.5" unit="rad"/> | ||
</section> | ||
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<section name="AUTO1" prefix="AUTO1_"> | ||
<define name="MAX_ROLL" value="40." unit="deg"/> | ||
<define name="MAX_PITCH" value="35." unit="deg"/> | ||
</section> | ||
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<section name="BAT"> | ||
<define name="MILLIAMP_AT_FULL_THROTTLE" value="2000"/> | ||
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/> | ||
<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/> | ||
<define name="LOW_BAT_LEVEL" value="9.7" unit="V"/> | ||
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/> | ||
</section> | ||
|
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<section name="MISC"> | ||
<define name="NOMINAL_AIRSPEED" value="13." unit="m/s"/> | ||
<define name="CARROT" value="5." unit="s"/> | ||
<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/> | ||
<define name="CONTROL_RATE" value="60" unit="Hz"/> | ||
<define name="ALT_KALMAN_ENABLED" value="TRUE"/> | ||
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/> | ||
</section> | ||
|
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</airframe> |
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