mirror of
https://github.com/paparazzi/paparazzi.git
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254 lines
9.6 KiB
XML
254 lines
9.6 KiB
XML
<!DOCTYPE airframe SYSTEM "airframe.dtd">
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<airframe name="Test Tiny 2.1">
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<!-- commands section -->
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<servos>
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<servo name="THROTTLE" no="0" min="1200" neutral="1200" max="2000"/>
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<!-- Servo aileron gauche = couleur blanche -->
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<!-- Aileron gauche oppose de l'aileron droit -->
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<servo name="AILERON_LEFT" no="1" min="1775" neutral="1500" max="1050"/>
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<!-- max = valeur aileron vers le bas-->
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<servo name="AILERON_RIGHT" no="3" min="1875" neutral="1475" max="1225"/>
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<!-- Rudder = Couleur rouge droite gauche -->
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<servo name="RUDDER" no="4" min="1875" neutral="1500" max="1250"/>
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<servo name="ELEVATOR" no="5" min="1850" neutral="1586" max="1150"/>
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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="YAW" 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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<set command="YAW" value="@YAW"/>
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</rc_commands>
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<section name="MIXER">
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<define name="AILERON_DIFF" value="0.66"/>
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<define name="COMBI_SWITCH" value="1.0"/>
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</section>
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<command_laws>
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<set servo="THROTTLE" value="@THROTTLE"/>
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<set servo="ELEVATOR" value="@PITCH"/>
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<set servo="RUDDER" value="@YAW + @ROLL*COMBI_SWITCH"/>
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<let var="roll" value="@ROLL"/>
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<set servo="AILERON_LEFT" value="($roll > 0 ? 1 : AILERON_DIFF) * $roll"/>
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<set servo="AILERON_RIGHT" value="($roll > 0 ? AILERON_DIFF : 1) * $roll"/>
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</command_laws>
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<section name="AUTO1" prefix="AUTO1_">
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<define name="MAX_ROLL" value="0.6"/>
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<define name="MAX_PITCH" value="0.6"/>
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</section>
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<!-- Serial n°0637446 . ADC_CHANNEL n°2,3 et 7 HS -->
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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_4"/>
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<define name="IR_NB_SAMPLES" value="16"/>
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</section>
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<section name="INFRARED" prefix="IR_">
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<define name="ROLL_NEUTRAL_DEFAULT" value="-6" unit="deg"/>
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<define name="PITCH_NEUTRAL_DEFAULT" value="12" unit="deg"/>
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<define name="DEFAULT_CONTRAST" value="200"/>
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<define name="RAD_OF_IR_CONTRAST" value="0.75"/>
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<linear name="RollOfIrs" arity="2" coeff1="0.7" coeff2="0.7"/>
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<linear name="PitchOfIrs" arity="2" coeff1="-0.7" coeff2="0.7"/>
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<linear name="TopOfIr" arity="1" coeff1="1"/>
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<define name="RAD_OF_IR_MAX_VALUE" value="0.0045"/>
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<define name="RAD_OF_IR_MIN_VALUE" value="0.00075"/>
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<define name="ADC_ROLL_NEUTRAL" value="716"/>
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<define name="ADC_PITCH_NEUTRAL" value="0"/>
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<define name="ADC_TOP_NEUTRAL" value="512"/>
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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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<define name="ESTIMATED_PHI_PI_4" value="0.9"/>
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<define name="360_LATERAL_CORRECTION" value="1."/>
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<define name="360_LONGITUDINAL_CORRECTION" value="1."/>
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<define name="360_VERTICAL_CORRECTION" value="1."/>
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</section>
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<section name="BAT">
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<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
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<define name="LOW_BATTERY" 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="11." 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\rATRN1\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="TRIGGER_DELAY" value="1."/>
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<define name="DEFAULT_CIRCLE_RADIUS" value="50."/>
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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="-0.07"/>
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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="0.55"/>
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<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.30"/>
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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="-500"/>
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<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.15" unit="%/(m/s)"/>
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<define name="AUTO_THROTTLE_PGAIN" value="-0.025"/>
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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="0.05"/>
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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="0.05"/>
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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="-1.2"/>
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<define name="ROLL_MAX_SETPOINT" value="0.6" 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="ROLL_PGAIN" value="12000."/>
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<define name="AILERON_OF_THROTTLE" value="0.0"/>
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<define name="PITCH_PGAIN" value="-9000."/>
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<define name="PITCH_DGAIN" value="1.5"/>
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<define name="ELEVATOR_OF_ROLL" value="1250"/>
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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="-5." 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="1000."/>
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<define name="HI_THROTTLE_ROLL_RATE_PGAIN" value="1000."/>
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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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</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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</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="0.8"/><!-- Gaz for Aggressive Climb -->
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<define name="CLIMB_PITCH" value="0.3"/><!-- 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="-0.25"/><!-- 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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<!--
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<section name="DATALINK" prefix="DATALINK_">
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<define name="DEVICE_TYPE" value="XBEE"/>
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<define name="DEVICE_ADDRESS" value="...."/>
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</section>
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-->
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<makefile>
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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 -DCONFIG=\"tiny_2_1.h\" -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_4017_hw.h\" -DSERVOS_4017 -DSERVOS_4017_CLOCK_FALLING
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ap.srcs += $(SRC_ARCH)/servos_4017_hw.c actuators.c
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ap.CFLAGS += -DRADIO_CONTROL -DRADIO_CONTROL_TYPE=RC_FUTABA
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ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
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#XBEE ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DDOWNLINK_FBW_DEVICE=Uart1 -DDOWNLINK_AP_DEVICE=Uart1 -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
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#XBEE ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
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ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart1 -DDOWNLINK_AP_DEVICE=Uart1 -DPPRZ_UART=Uart1 -DDATALINK=PPRZ -DUART1_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_4
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ap.srcs += $(SRC_ARCH)/adc_hw.c
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ap.CFLAGS += -DGPS -DUBX -DUSE_UART0 -DGPS_LINK=Uart0 -DUART0_BAUD=B19200
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ap.srcs += gps_ubx.c gps.c latlong.c
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ap.CFLAGS += -DINFRARED -DALT_KALMAN -DIR_360
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ap.srcs += infrared.c estimator.c
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ap.CFLAGS += -DNAV -DH_CTL_RATE_LOOP -DAGR_CLIMB -DLOITER_TRIM
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ap.srcs += nav.c fw_h_ctl.c fw_v_ctl.c nav_survey_rectangle.c
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# Harware In The Loop
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#ap.CFLAGS += -DHITL
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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 += -DCONFIG=\"tiny.h\" -DAGR_CLIMB -DH_CTL_RATE_LOOP -DLOITER_TRIM -DALT_KALMAN -DIR_360
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sim.srcs += nav_survey_rectangle.c
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</makefile>
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</airframe>
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