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YAPA
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dewagter
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<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<!--
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YAPA + XSens + XBee
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-->
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<airframe name="Yapa v1">
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<modules>
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<load name="TUDelft/blink_led_3.xml"/>
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</modules>
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<servos>
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<servo name="MOTOR" no="0" min="1000" neutral="1000" max="2000"/>
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<servo name="AILEVON_LEFT" no="2" min="1130" neutral="1575" max="1880"/>
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<servo name="AILEVON_RIGHT" no="6" min="1980" neutral="1465" max="1170"/>
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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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<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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</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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</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 + $aileron"/>
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<set servo="AILEVON_RIGHT" value="$elevator - $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_0"/>
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<define name="IR2" value="ADC_1"/>
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<define name="IR_TOP" value="ADC_2"/>
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<define name="IR_NB_SAMPLES" value="16"/>
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<define name="ONBOARDCAMA" value="ADC_4"/>
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<define name="ONBOARDCAMA_NB_SAMPLES" value="16"/>
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<define name="ONBOARDCAMB" value="ADC_5"/>
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<define name="ONBOARDCAMB_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="CAMERA" prefix="CAM_">
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<define name="TILT0" value="0" unit="deg"/>
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<define name="TILT_MIN" value="-20" unit="deg"/>
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<define name="TILT_NEUTRAL" value="0" unit="deg"/>
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<define name="TILT_MAX" value="20" unit="deg"/>
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<define name="PAN0" value="0" unit="deg"/>
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<define name="PAN_MIN" value="-20" unit="deg"/>
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<define name="PAN_NEUTRAL" value="0" unit="deg"/>
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<define name="PAN_MAX" value="20" unit="deg"/>
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</section>
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<section name="BAT">
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<define name="MILLIAMP_AT_FULL_THROTTLE" value="2000"/>
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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="12." unit="m/s"/>
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<define name="NOMINAL_AIRSPEED" value="15." unit="m/s"/>
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<define name="MAXIMUM_AIRSPEED" value="25." 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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<!--uncommant API protocol in makefile uncommant after programed
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<define name="XBEE_INIT" value=""ATCHC\rATID3332\rATPL4\rATRN1\rATTT80\rATBD3\rATWR\r""/>
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<define name="NO_XBEE_API_INIT" value="TRUE"/> -->
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</section>
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<section name="VERTICAL CONTROL" prefix="V_CTL_">
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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="0.35"/>
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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="-1000"/>
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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="0.1"/>
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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="-0.8"/>
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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="-10000."/>
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<define name="PITCH_DGAIN" value="1.5"/>
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<define name="ELEVATOR_OF_ROLL" value="2500"/>
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<define name="ROLL_ATTITUDE_GAIN" value="-7500"/>
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<define name="ROLL_RATE_GAIN" value="-1500"/>
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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="0.6"/><!-- 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="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_2_1_1.h\"
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include $(PAPARAZZI_SRC)/conf/autopilot/tiny.makefile
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FLASH_MODE=IAP
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XSENS_UART_NR = 0
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ap.CFLAGS += -DFBW -DAP -DBOARD_CONFIG=$(CONFIG) -DLED
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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_4017_hw.h\" -DSERVOS_4017
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ap.srcs += $(SRC_ARCH)/servos_4017_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=B57600
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#ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c pprz_transport.c
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# Maxstream API protocol
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ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B9600 -DTELEMETRY_MODE_FBW=1
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ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
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ap.CFLAGS += -DINTER_MCU -DUSE_MODULES
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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_4 -DUSE_ADC_5
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ap.srcs += $(SRC_ARCH)/adc_hw.c
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ap.srcs += gps_xsens.c gps.c latlong.c
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ap.CFLAGS += -DALT_KALMAN
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ap.srcs += 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.srcs += nav_line.c nav_survey_rectangle.c
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# Config for SITL simulation
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include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
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sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN -DTRAFFIC_INFO
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sim.srcs += nav_survey_rectangle.c traffic_info.c nav_line.c
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</makefile>
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</airframe>
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