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https://github.com/paparazzi/paparazzi.git
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PPZIMU in Microjet
This commit is contained in:
Christophe De Wagter
@@ -0,0 +1,307 @@
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<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<airframe name="Microjet BR Tiny 1.1">
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<!-- commands section -->
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<servos>
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<servo name="THROTTLE" no="0" min="1100" neutral="1100" max="1700"/>
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<servo name="AILEVON_LEFT" no="1" min="2000" neutral="1500" max="1000"/>
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<servo name="AILEVON_RIGHT" no="3" min="950" neutral="1450" max="1950"/>
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<servo name="CAM_PAN" no="5" min="1950" neutral="1450" max="950"/>
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<servo name="CAM_TILT" no="2" min="1000" neutral="1550" max="2000"/>
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</servos>
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<commands>
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<axis name="THROTTLE" 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="CAM_TILT" failsafe_value="0"/>
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<axis name="CAM_PAN" failsafe_value="0"/>
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</commands>
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<rc_commands>
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<set command="THROTTLE" 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="CAM_PAN" value="@YAW"/>
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<set command="CAM_TILT" value="@YAW"/>
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</rc_commands>
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<section name="MIXER">
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<define name="AILEVON_AILERON_RATE" value="0.4"/>
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<define name="AILEVON_ELEVATOR_RATE" value="0.7"/>
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</section>
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<command_laws>
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<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/>
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<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
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<set servo="THROTTLE" value="@THROTTLE"/>
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<set servo="AILEVON_LEFT" value="$elevator + $aileron"/>
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<set servo="AILEVON_RIGHT" value="$elevator - $aileron"/>
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<set servo="CAM_PAN" value="@CAM_PAN"/>
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<set servo="CAM_TILT" value="@CAM_TILT"/>
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</command_laws>
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<!-- Local magnetic field -->
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<section name="AHRS" prefix="AHRS_">
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<define name="H_X" value="0.51562740288882"/>
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<define name="H_Y" value="-0.05707735220832"/>
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<define name="H_Z" value="0.85490967783446"/>
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</section>
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<section name="IMU" prefix="IMU_">
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<!-- Calibration Neutral -->
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<define name="GYRO_P_NEUTRAL" value="0"/>
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<define name="GYRO_Q_NEUTRAL" value="0"/>
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<define name="GYRO_R_NEUTRAL" value="0"/>
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<!-- SENS = 14.375 LSB/(deg/sec) * 57.6 deg/rad = 828 LSB/rad/sec / 12bit FRAC: 4096 / 828 -->
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<define name="GYRO_P_SENS" value="4.947" integer="16"/>
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<define name="GYRO_Q_SENS" value="4.947" integer="16"/>
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<define name="GYRO_R_SENS" value="4.947" integer="16"/>
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<define name="GYRO_P_Q" value="0."/>
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<define name="GYRO_P_R" value="0"/>
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<define name="GYRO_Q_P" value="0."/>
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<define name="GYRO_Q_R" value="0."/>
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<define name="GYRO_R_P" value="0."/>
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<define name="GYRO_R_Q" value="0."/>
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<define name="GYRO_P_SIGN" value="-1"/>
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<define name="GYRO_Q_SIGN" value="-1"/>
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<define name="GYRO_R_SIGN" value="1"/>
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<define name="ACCEL_X_NEUTRAL" value="-14"/>
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<define name="ACCEL_Y_NEUTRAL" value="0"/>
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<define name="ACCEL_Z_NEUTRAL" value="0"/>
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<!-- SENS = 256 LSB/g @ 2.5V [X&Y: 265 LSB/g @ 3.3V] / 9.81 ms2/g = 26.095 LSB/ms2 / 10bit FRAC: 1024 / 26.095 for z and 1024 / 27.01 for X&Y -->
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<define name="ACCEL_X_SENS" value="37.9" integer="16"/>
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<define name="ACCEL_Y_SENS" value="37.9" integer="16"/>
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<define name="ACCEL_Z_SENS" value="39.24" integer="16"/>
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<define name="ACCEL_X_SIGN" value="-1"/>
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<define name="ACCEL_Y_SIGN" value="-1"/>
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<define name="ACCEL_Z_SIGN" value="1"/>
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<define name="MAG_X_NEUTRAL" value="0"/>
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<define name="MAG_Y_NEUTRAL" value="0"/>
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<define name="MAG_Z_NEUTRAL" value="0"/>
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<define name="MAG_X_SENS" value="1" integer="16"/>
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<define name="MAG_Y_SENS" value="1" integer="16"/>
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<define name="MAG_Z_SENS" value="1" integer="16"/>
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<define name="MAG_X_SIGN" value="1"/>
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<define name="MAG_Y_SIGN" value="1"/>
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<define name="MAG_Z_SIGN" value="1"/>
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<define name="BODY_TO_IMU_PHI" value="0"/>
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<define name="BODY_TO_IMU_THETA" value="0"/>
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<define name="BODY_TO_IMU_PSI" value="0"/>
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</section>
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<section name="INS" prefix="INS_">
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<define name="ROLL_NEUTRAL_DEFAULT" value="0." unit="deg"/>
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<define name="PITCH_NEUTRAL_DEFAULT" value="0." unit="deg"/>
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</section>
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<section name="AUTO1" prefix="AUTO1_">
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<define name="MAX_ROLL" value="1.1"/>
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<define name="MAX_PITCH" value="0.9"/>
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</section>
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<section name="BAT">
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<define name="MILLIAMP_AT_FULL_THROTTLE" value="25000"/>
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<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
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</section>
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<section name="MISC">
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<define name="NOMINAL_AIRSPEED" value="17." unit="m/s"/>
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<define name="CARROT" value="5." unit="s"/>
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<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
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<define name="CONTROL_RATE" value="60" unit="Hz"/>
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<!-- <define name="XBEE_INIT" value=""ATPL2\rATRN5\rATTT80\r""/> -->
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<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
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<define name="ALT_KALMAN_ENABLED" value="TRUE"/>
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<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
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<define name="GLIDE_AIRSPEED" value="10"/>
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<define name="GLIDE_VSPEED" value="3."/>
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<define name="GLIDE_PITCH" value="45" unit="deg"/>
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<define name="LIGHT_LED_1" value="3"/>
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</section>
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<section name="external leds">
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<!-- ADC 4 -->
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<define name="LED_4_BANK" value="0"/>
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<define name="LED_4_PIN" value="22"/>
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</section>
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<section name="VERTICAL CONTROL" prefix="V_CTL_">
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<define name="POWER_CTL_BAT_NOMINAL" value="11.1" unit="volt"/>
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<!-- outer loop proportional gain -->
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<define name="ALTITUDE_PGAIN" value="-0.101000003517"/>
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<!-- outer loop saturation max m/s the alt tap can be-->
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<define name="ALTITUDE_MAX_CLIMB" value="4"/>
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<!-- auto throttle inner loop -->
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<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.333000004292"/>
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<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.15"/>
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<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.45"/>
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<define name="AUTO_THROTTLE_LOITER_TRIM" value="219.511993408"/>
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<define name="AUTO_THROTTLE_DASH_TRIM" value="-1200"/>
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<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.104999996722" unit="%/(m/s)"/>
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<define name="AUTO_THROTTLE_PGAIN" value="-0.00700000021607"/>
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<define name="AUTO_THROTTLE_IGAIN" value="0."/>
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<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.12800000608"/>
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<!-- auto pitch inner loop -->
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<define name="AUTO_PITCH_PGAIN" value="-0.0399999991059"/>
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<define name="AUTO_PITCH_IGAIN" value="0.019999999553"/>
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<define name="AUTO_PITCH_MAX_PITCH" value="0.35"/>
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<define name="AUTO_PITCH_MIN_PITCH" value="-0.35"/>
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<define name="THROTTLE_SLEW_LIMITER" value="2" unit="s"/>
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</section>
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<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
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<define name="COURSE_PGAIN" value="-1.54100000858"/>
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<define name="ROLL_MAX_SETPOINT" value="0.916999995708" unit="radians"/>
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<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
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<define name="PITCH_MIN_SETPOINT" value="-0.4" unit="radians"/>
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<define name="ROLL_PGAIN" value="5000."/>
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<define name="AILERON_OF_THROTTLE" value="0.0"/>
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<define name="PITCH_PGAIN" value="-7330.82714844"/>
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<define name="PITCH_DGAIN" value="1.7254999876"/>
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<define name="ELEVATOR_OF_ROLL" value="1250."/>
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<define name="ROLL_RATE_GAIN" value="-112.781997681"/>
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<define name="ROLL_ATTITUDE_GAIN" value="-4957.62695312"/>
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<!-- roll rate loop -->
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<define name="ROLL_RATE_MODE_DEFAULT" value="1"/>
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<define name="ROLL_RATE_SETPOINT_PGAIN" value="-10." unit="rad/s/rad"/>
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<define name="ROLL_RATE_MAX_SETPOINT" value="10"/>
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<define name="LO_THROTTLE_ROLL_RATE_PGAIN" value="3000."/>
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<define name="HI_THROTTLE_ROLL_RATE_PGAIN" value="3000."/>
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<define name="ROLL_RATE_IGAIN" value="0."/>
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<define name="ROLL_RATE_DGAIN" value="0."/>
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<define name="ROLL_RATE_SUM_NB_SAMPLES" value="64"/>
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<define name="ROLL_SLEW" value="0.1"/>
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<define name="SIMPLE_ROLL_PGAIN" value="-15000"/>
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<define name="SIMPLE_ROLL_DGAIN" value="-3000"/>
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</section>
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<section name="NAV">
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<define name="NAV_PITCH" value="0."/>
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<define name="NAV_GLIDE_PITCH_TRIM" value="0."/>
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<!-- <define name="NAV_GROUND_SPEED_PGAIN" value="-0.015"/> NOG niet in de nav.c file
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<define name="NAV_FOLLOW_PGAIN" value="-0.05"/> -->
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</section>
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<section name="AGGRESSIVE" prefix="AGR_">
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<define name="BLEND_START" value="50"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
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<define name="BLEND_END" value="25"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
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<define name="CLIMB_THROTTLE" value="0.55"/><!-- Gaz for Aggressive Climb -->
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<define name="CLIMB_PITCH" value="0.5"/><!-- Pitch for Aggressive Climb -->
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<define name="DESCENT_THROTTLE" value="0.0"/><!-- Gaz for Aggressive Decent -->
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<define name="DESCENT_PITCH" value="-0.3"/><!-- Pitch for Aggressive Decent -->
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<define name="CLIMB_NAV_RATIO" value="0.8"/><!-- Percent Navigation for Altitude Error Equal to Start Altitude -->
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<define name="DESCENT_NAV_RATIO" value="1.0"/>
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</section>
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<section name="FAILSAFE" prefix="FAILSAFE_">
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<define name="DELAY_WITHOUT_GPS" value="2" unit="s"/>
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<define name="DEFAULT_THROTTLE" value="0.3" unit="%"/>
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<define name="DEFAULT_ROLL" value="0.3" unit="rad"/>
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<define name="DEFAULT_PITCH" value="0.5" unit="rad"/>
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<define name="HOME_RADIUS" value="80" unit="m"/>
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</section>
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<section name="CAM" prefix="CAM_">
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<define name="TILT_MAX" value="30" unit="deg"/>
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<define name="TILT_NEUTRAL" value="0" unit="deg"/>
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<define name="TILT_MIN" value="-30" unit="deg"/>
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<define name="TILT0" value="0" unit="deg"/>
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<define name="PAN_MAX" value="45" unit="deg"/>
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<define name="PAN_NEUTRAL" value="0" unit="deg"/>
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<define name="PAN_MIN" value="-45" unit="deg"/>
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<define name="PAN0" value="0" unit="deg"/>
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</section>
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<!--moet nog in tuning-->
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<section name="Takeoff" prefix="Takeoff_">
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<define name="Height" value="30" unit="m"/>
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<define name="Speed" value="15" unit="m/s"/>
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<define name="MinSpeed" value="5" unit="m/s"/>
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<define name="Distance" value="10" unit="m"/>
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</section>
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<section name="Landing" prefix="Landing_">
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<define name="FinalHeight" value="30" unit="m"/>
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<define name="AFHeight" value="10" unit="m"/>
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<define name="FinalStageTime" value="10" unit="s"/>
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</section>
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<section name="SIMU">
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<define name="YAW_RESPONSE_FACTOR" value="0.5"/> <!-- ?????????????????????????? -->
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</section>
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<modules>
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<load name="light.xml">
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<define name="LIGHT_LED_STROBE" value="3"/>
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<define name="STROBE_LIGHT_MODE_DEFAULT" value="6"/>
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</load>
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</modules>
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<firmware name="fixedwing">
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<target name="ap" board="tiny_1.1">
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<configure name="FLASH_MODE" value="IAP"/>
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<configure name="PERIODIC_FREQUENCY" value="120"/>
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<configure name="AHRS_PROPAGATE_FREQUENCY" value="100"/>
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<configure name="AHRS_CORRECT_FREQUENCY" value="100"/>
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<define name="AHRS_TRIGGERED_ATTITUDE_LOOP"/>
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<configure name="AHRS_ALIGNER_LED" value="2"/>
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<define name="STRONG_WIND" />
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<define name="LOITER_TRIM" />
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<define name="ALT_KALMAN" />
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<define name="AGR_CLIMB" />
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<define name="TUNE_AGRESSIVE_CLIMB" />
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</target>
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<target name="sim" board="pc" >
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<define name="STRONG_WIND" />
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<define name="TUNE_AGRESSIVE_CLIMB" />
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<define name="LOITER_TRIM" />
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<define name="AGR_CLIMB" />
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</target>
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<subsystem name="radio_control" type="ppm"/>
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<!-- Communication -->
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<subsystem name="telemetry" type="transparent">
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<configure name="MODEM_BAUD" value="B57600"/>
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</subsystem>
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<!-- Sensors -->
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<subsystem name="imu" type="ppzuav"/>
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<subsystem name="attitude" type="dcm"/>
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<subsystem name="i2c"/>
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<subsystem name="gps" type="ublox_lea4p"/>
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<subsystem name="control" />
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<subsystem name="navigation" />
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</firmware>
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</airframe>
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