mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-06-01 21:07:40 +08:00
Pascal Brisset
270 lines
9.9 KiB
XML
270 lines
9.9 KiB
XML
<!DOCTYPE airframe SYSTEM "airframe.dtd">
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<!-- Solar Storm
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Tiny 1.1
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Tilted infrared sensor
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Radiotronix modem
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MPTT tracker
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Drop servo -->
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<airframe name="SolarStorm">
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<modules>
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<load name="poles.xml"/>
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<load name="MPPT.xml"/>
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</modules>
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<!-- commands section -->
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<servos>
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<servo name="MOTOR" no="3" min="1250" neutral="1250" max="1800"/>
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<servo name="AILEVON_LEFT" no="4" min="1850" neutral="1470" max="1100"/>
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<servo name="AILEVON_RIGHT" no="5" min="1100" neutral="1545" max="1870"/>
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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="HATCH" 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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</rc_commands>
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<section name="MIXER">
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<define name="AILEVON_AILERON_RATE" value="0.75"/>
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<define name="AILEVON_ELEVATOR_RATE" value="0.75"/>
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<define name="AILERON_DIFF" value="0.5"/>
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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="MOTOR" value="@THROTTLE"/>
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<set servo="AILEVON_LEFT" value="$elevator + ($aileron > 0 ? 1 : AILERON_DIFF) * $aileron"/>
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<set servo="AILEVON_RIGHT" value="$elevator - ($aileron > 0 ? AILERON_DIFF : 1) * $aileron"/>
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</command_laws>
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<section name="AUTO1" prefix="AUTO1_">
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<define name="MAX_ROLL" value="0.85"/>
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<define name="MAX_PITCH" value="0.6"/>
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</section>
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<section name="adc" prefix="ADC_CHANNEL_">
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<define name="IR1" value="ADC_2"/>
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<define name="IR2" value="ADC_1"/>
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<define name="IR_TOP" value="ADC_0"/>
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<define name="IR_NB_SAMPLES" value="16"/>
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<define name="GYRO_ROLL" value="ADC_3"/>
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<define name="GYRO_NB_SAMPLES" value="16"/>
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</section>
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<section name="INFRARED" prefix="IR_">
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<define name="ADC_IR1_NEUTRAL" value="512"/>
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<define name="ADC_IR2_NEUTRAL" value="512"/>
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<define name="ADC_TOP_NEUTRAL" value="512"/>
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<define name="LATERAL_CORRECTION" value="1."/>
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<define name="LONGITUDINAL_CORRECTION" value="1."/>
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<define name="VERTICAL_CORRECTION" value="1.2"/>
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<define name="HORIZ_SENSOR_TILTED" value="1"/>
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<define name="IR1_SIGN" value="-1"/>
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<define name="IR2_SIGN" value="1"/>
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<define name="TOP_SIGN" value="-1"/>
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<define name="ROLL_NEUTRAL_DEFAULT" value="3.49504256248" unit="deg"/>
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<define name="PITCH_NEUTRAL_DEFAULT" value="8.42247962952" unit="deg"/>
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<define name="CORRECTION_UP" value="1."/>
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<define name="CORRECTION_DOWN" value="1."/>
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<define name="CORRECTION_LEFT" value="1."/>
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<define name="CORRECTION_RIGHT" value="1."/>
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</section>
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<section name="GYRO" prefix="GYRO_">
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<define name="ADC_ROLL_NEUTRAL" value="512"/>
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<define name="DYNAMIC_RANGE" value="300" unit="deg/s"/>
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<define name="ADXRS300_RESISTOR_BRIDGE" value="(3.3/(3.3+1.8))"/>
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<define name="ADXRS300_SENSITIVITY" value="5" unit="mV/(deg/s)"/>
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<define name="ROLL_SCALE" value="3.3*1000./1024./(GYRO_ADXRS300_SENSITIVITY*GYRO_ADXRS300_RESISTOR_BRIDGE)" unit="deg/s/adc_unit"/>
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<define name="ROLL_DIRECTION" value="-1."/>
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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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</section>
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<section name="MISC">
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<define name="MINIMUM_AIRSPEED" value="13." unit="m/s"/>
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<define name="NOMINAL_AIRSPEED" value="16." unit="m/s"/>
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<define name="MAXIMUM_AIRSPEED" value="24." 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="ALT_KALMAN_ENABLED" value="TRUE"/>
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<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
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<define name="MIN_CIRCLE_RADIUS" value="50."/>
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<define name="UNLOCKED_HOME_MODE" value="TRUE"/>
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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="-0.04"/>
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<!-- outer loop saturation -->
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<define name="ALTITUDE_MAX_CLIMB" value="2."/>
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<!-- auto throttle inner loop -->
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<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.356000006199"/>
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<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/>
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<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.80"/>
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<define name="AUTO_THROTTLE_LOITER_TRIM" value="1500"/>
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<define name="AUTO_THROTTLE_DASH_TRIM" value="-2500"/>
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<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.1" unit="%/(m/s)"/>
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<define name="AUTO_THROTTLE_PGAIN" value="-0.02"/>
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<define name="AUTO_THROTTLE_IGAIN" value="0.1"/>
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<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.15"/>
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<!-- auto pitch inner loop -->
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<define name="AUTO_PITCH_PGAIN" value="-0.05"/>
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<define name="AUTO_PITCH_IGAIN" value="0.075"/>
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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" value="0.5"/>
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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="-0.885999977589"/>
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<define name="ROLL_MAX_SETPOINT" value="0.7" 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="-0.5" unit="radians"/>
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<define name="PITCH_PGAIN" value="-14255.3193359"/>
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<define name="PITCH_DGAIN" value="1.5"/>
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<define name="ELEVATOR_OF_ROLL" value="2000."/>
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<define name="ROLL_ATTITUDE_GAIN" value="-12000"/>
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<define name="ROLL_RATE_GAIN" value="-2500"/>
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<define name="ROLL_KFF" value="-500"/>
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<define name="ROLL_IGAIN" value="-00"/>
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<define name="PITCH_IGAIN" value="-500"/>
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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="-0.01"/>
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</section>
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<section name="AGGRESSIVE" prefix="AGR_">
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<define name="BLEND_START" value="20"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
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<define name="BLEND_END" value="10"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
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<define name="CLIMB_THROTTLE" value="0.75"/><!-- Gaz for Aggressive Climb -->
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<define name="CLIMB_PITCH" value="0.20"/><!-- Pitch for Aggressive Climb -->
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<define name="DESCENT_THROTTLE" value="0.1"/><!-- Gaz for Aggressive Decent -->
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<define name="DESCENT_PITCH" value="-0.15"/><!-- 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="GYRO_GAINS">
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<define name="GYRO_MAX_RATE" value="200."/>
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<define name="ROLLRATESUM_NB_SAMPLES" value="64"/>
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<define name="ALT_ROLL__PGAIN" value="1.0"/>
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<define name="ROLL_RATE_PGAIN" value="1000.0"/>
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<define name="ROLL_RATE_IGAIN" value="0.0"/>
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<define name="ROLL_RATE_DGAIN" value="0.0"/>
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</section>
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<section name="FAILSAFE" prefix="FAILSAFE_">
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<define name="DELAY_WITHOUT_GPS" value="1" 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="100" unit="m"/>
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</section>
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<makefile>
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CONFIG = \"tiny_1_1.h\"
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include $(PAPARAZZI_SRC)/conf/autopilot/tiny.makefile
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FLASH_MODE=IAP
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ap.CFLAGS += -DFBW -DAP -DBOARD_CONFIG=$(CONFIG) -DLED -DTIME_LED=1
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ap.srcs = sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c main_fbw.c main_ap.c main.c
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ap.srcs += commands.c
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ap.CFLAGS += -DACTUATORS=\"servos_4015_MAT_hw.h\" -DSERVOS_4015_MAT
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ap.srcs += $(SRC_ARCH)/servos_4015_MAT_hw.c actuators.c
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ap.CFLAGS += -DRADIO_CONTROL
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ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
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ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DPPRZ_UART=Uart0 -DDATALINK=PPRZ -DUART0_BAUD=B9600
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ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c pprz_transport.c
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ap.CFLAGS += -DINTER_MCU
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ap.srcs += inter_mcu.c
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ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2 -DUSE_ADC_3
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ap.srcs += $(SRC_ARCH)/adc_hw.c
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ap.CFLAGS += -DGPS -DUBX -DUSE_UART1 -DGPS_LINK=Uart1 -DUART1_BAUD=B9600 -DGPS_LED=2
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#ap.CFLAGS += -DGPS -DUBX -DUSE_UART1 -DGPS_LINK=Uart1 -DUART1_BAUD=B9600 -DGPS_LED=2
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ap.CFLAGS += -DGPS_CONFIGURE -DGPS_BAUD=38400
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ap.srcs += gps_ubx.c gps.c latlong.c
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ap.CFLAGS += -DINFRARED -DALT_KALMAN
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ap.srcs += infrared.c estimator.c
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ap.CFLAGS += -DNAV -DAGR_CLIMB -DLOITER_TRIM
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ap.srcs += nav.c fw_h_ctl.c fw_v_ctl.c
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ap.CFLAGS += -DGYRO -DADXRS150
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ap.srcs += gyro.c nav_line.c
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ap.srcs += nav_survey_rectangle.c
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########## MPTT
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ap.srcs += i2c.c $(SRC_ARCH)/i2c_hw.c
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ap.CFLAGS += -DUSE_I2C0 -DI2C0_SCLL=150 -DI2C0_SCLH=150
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ap.CFLAGS += -DUSE_MODULES
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# Config for SITL simulation
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#include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
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sim.ARCHDIR = $(ARCHI)
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sim.ARCH = sitl
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sim.TARGET = autopilot
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sim.TARGETDIR = autopilot
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sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DINFRARED -DNAV -DLED -DWIND_INFO
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sim.srcs = latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl.c nav.c estimator.c sys_time.c main_fbw.c main_ap.c datalink.c $(SRC_ARCH)/ppm_hw.c $(SRC_ARCH)/sim_gps.c $(SRC_ARCH)/sim_ir.c $(SRC_ARCH)/sim_ap.c $(SRC_ARCH)/ivy_transport.c $(SRC_ARCH)/sim_adc_generic.c $(SRC_ARCH)/led_hw.c
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sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
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sim.srcs += nav_line.c nav_survey_rectangle.c
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sim.CFLAGS += -DUSE_MODULES
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</makefile>
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</airframe>
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