mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-05-23 21:36:28 +08:00
new gfi ac, moving
This commit is contained in:
Martin Mueller
@@ -6,16 +6,16 @@
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Tilted infrared sensor (http://paparazzi.enac.fr/wiki/index.php/Image:Tiny_v2_1_Funjet.jpg)
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XBee modem
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Payload: Sensirion humidity/temp, VTI pressure/temp
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K61, LEA 4 (set to POSLLH)
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K66, LEA 5
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-->
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<airframe name="Funjet GFI 5 K61">
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<airframe name="Funjet GFI 5 K66">
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<!-- commands section -->
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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="1900" neutral="1622" max="1100"/>
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<servo name="AILEVON_RIGHT" no="6" min="1100" neutral="1538" max="1900"/>
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<servo name="AILEVON_LEFT" no="2" min="1900" neutral="1520" max="1100"/>
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<servo name="AILEVON_RIGHT" no="6" min="1100" neutral="1456" max="1900"/>
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</servos>
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<commands>
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@@ -0,0 +1,247 @@
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<!DOCTYPE airframe SYSTEM "airframe.dtd">
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<!-- Funjet Multiplex (http://www.multiplex-rc.de/), Jeti ECO 25
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Tiny 2.11 board (http://paparazzi.enac.fr/wiki/index.php/Tiny_v2)
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PerkinElmer TPS334 IR Sensors
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Tilted infrared sensor (http://paparazzi.enac.fr/wiki/index.php/Image:Tiny_v2_1_Funjet.jpg)
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XBee modem
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Payload: Sensirion humidity/temp, VTI pressure/temp
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K68, LEA 5
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-->
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<airframe name="Funjet GFI 9 K68">
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<!-- commands section -->
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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="1900" neutral="1574" max="1100"/>
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<servo name="AILEVON_RIGHT" no="6" min="1100" neutral="1509" max="1900"/>
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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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</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="0.45"/>
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<define name="AILEVON_ELEVATOR_RATE" value="0.8"/>
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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_1"/>
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<define name="IR2" value="ADC_2"/>
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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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</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="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="LATERAL_CORRECTION" value="-1"/>
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<define name="LONGITUDINAL_CORRECTION" value="1"/>
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<define name="VERTICAL_CORRECTION" value="1.5"/>
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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="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="BAT">
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<define name="MILLIAMP_AT_FULL_THROTTLE" value="10000."/>
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<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
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<!-- 0.0247311828 -->
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<!-- 0.02432905 -->
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<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
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</section>
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<section name="MISC">
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<define name="NOMINAL_AIRSPEED" value="15." 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="FALSE"/>
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<define name="TRIGGER_DELAY" value="1."/>
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<define name="DEFAULT_CIRCLE_RADIUS" value="120."/>
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<define name="MIN_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="-0.06"/> <!-- -0.024 -->
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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="0.45"/>
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<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.35"/>
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<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.85"/>
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<define name="AUTO_THROTTLE_LOITER_TRIM" value="1000"/>
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<define name="AUTO_THROTTLE_DASH_TRIM" value="-1200"/>
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<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.2" unit="%/(m/s)"/>
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<define name="AUTO_THROTTLE_PGAIN" value="-0.023"/> <!-- -0.012 -->
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<define name="AUTO_THROTTLE_IGAIN" value="0.01"/>
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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="-0.06"/> <!-- -0.03 -->
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<define name="AUTO_PITCH_IGAIN" value="0.0"/>
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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="0.1"/>
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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="-0.9"/>
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<define name="ROLL_MAX_SETPOINT" value="0.70" unit="radians"/> <!-- 0.5 -->
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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="6600."/>
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<define name="AILERON_OF_THROTTLE" value="0.0"/>
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<define name="PITCH_PGAIN" value="-5500."/>
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<define name="PITCH_DGAIN" value="0.4"/>
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<define name="ELEVATOR_OF_ROLL" value="2400"/>
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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="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="50"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
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<define name="BLEND_END" value="15"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
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<define name="CLIMB_THROTTLE" value="0.9"/><!-- Gaz for Aggressive Climb -->
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<define name="CLIMB_PITCH" value="0.35"/><!-- Pitch for Aggressive Climb -->
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<define name="DESCENT_THROTTLE" value="0.05"/><!-- Gaz for Aggressive Decent -->
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<define name="DESCENT_PITCH" value="-0.35"/><!-- 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="100" unit="m"/>
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</section>
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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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<section name="SIMU">
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<define name="YAW_RESPONSE_FACTOR" value="0.5"/>
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</section>
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<makefile>
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CONFIG = \"tiny_2_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_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_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
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ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
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#TRANSPARENT
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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_2
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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=B38400 -DGPS_USE_LATLONG
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# -DGPS_LED=2
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ap.srcs += gps_ubx.c gps.c latlong.c
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ap.CFLAGS += -DINFRARED -DALT_KALMAN -DWIND_INFO -DWIND_INFO_RET
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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.srcs += nav_line.c
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ap.srcs += nav_survey_rectangle.c
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|
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ap.srcs += humid_sht.c
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ap.CFLAGS += -DUSE_HUMID_SHT -DDAT_PIN=3 -DSCK_PIN=2
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|
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ap.srcs += baro_scp.c
|
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ap.CFLAGS += -DUSE_BARO_SCP
|
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|
||||
ap.srcs += joystick.c
|
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ap.CFLAGS += -DUSE_JOYSTICK
|
||||
|
||||
# Config for SITL simulation
|
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include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
|
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sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
|
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sim.srcs += nav_line.c nav_survey_rectangle.c
|
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|
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sim.srcs += joystick.c
|
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sim.CFLAGS += -DUSE_JOYSTICK
|
||||
|
||||
|
||||
</makefile>
|
||||
</airframe>
|
||||
@@ -0,0 +1,239 @@
|
||||
<!DOCTYPE airframe SYSTEM "../../airframe.dtd">
|
||||
|
||||
<!-- Merlin, Himax HC2212-1180
|
||||
Tiny 2.11
|
||||
PerkinElmer TPS334 IR Sensors
|
||||
Tilted infrared sensor
|
||||
XBee modem
|
||||
LEA 4P (set to POSLLH)
|
||||
-->
|
||||
|
||||
<airframe name="Merlin">
|
||||
|
||||
<!-- commands section -->
|
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<servos>
|
||||
<servo name="AILERON_RIGHT" no="0" min="1900" neutral="1500" max="1100"/>
|
||||
<servo name="AILERON_LEFT" no="2" min="1900" neutral="1500" max="1100"/>
|
||||
<servo name="ELEVATOR" no="6" min="1100" neutral="1500" max="1900"/>
|
||||
<servo name="MOTOR" no="7" min="1000" neutral="1000" max="2000"/>
|
||||
</servos>
|
||||
|
||||
<commands>
|
||||
<axis name="THROTTLE" failsafe_value="0"/>
|
||||
<axis name="ROLL" failsafe_value="0"/>
|
||||
<axis name="PITCH" failsafe_value="0"/>
|
||||
</commands>
|
||||
|
||||
<rc_commands>
|
||||
<set command="THROTTLE" value="@THROTTLE"/>
|
||||
<set command="ROLL" value="@ROLL"/>
|
||||
<set command="PITCH" value="@PITCH"/>
|
||||
</rc_commands>
|
||||
|
||||
<section name="MIXER">
|
||||
<define name="AILERON_DIFF" value="0.8"/>
|
||||
</section>
|
||||
|
||||
<command_laws>
|
||||
<set servo="MOTOR" value="@THROTTLE"/>
|
||||
<set servo="ELEVATOR" value="@PITCH"/>
|
||||
<let var="roll" value="@ROLL"/>
|
||||
<set servo="AILERON_LEFT" value="($roll > 0 ? 1 : AILERON_DIFF) * $roll"/>
|
||||
<set servo="AILERON_RIGHT" value="($roll > 0 ? AILERON_DIFF : 1) * $roll"/>
|
||||
</command_laws>
|
||||
|
||||
<section name="AUTO1" prefix="AUTO1_">
|
||||
<define name="MAX_ROLL" value="0.85"/>
|
||||
<define name="MAX_PITCH" value="0.6"/>
|
||||
</section>
|
||||
|
||||
<section name="adc" prefix="ADC_CHANNEL_">
|
||||
<define name="IR1" value="ADC_1"/>
|
||||
<define name="IR2" value="ADC_2"/>
|
||||
<define name="IR_TOP" value="ADC_0"/>
|
||||
<define name="IR_NB_SAMPLES" value="16"/>
|
||||
</section>
|
||||
|
||||
<section name="INFRARED" prefix="IR_">
|
||||
<define name="ADC_IR1_NEUTRAL" value="512"/>
|
||||
<define name="ADC_IR2_NEUTRAL" value="512"/>
|
||||
<define name="ADC_TOP_NEUTRAL" value="512"/>
|
||||
|
||||
<define name="CORRECTION_UP" value="1."/>
|
||||
<define name="CORRECTION_DOWN" value="1."/>
|
||||
<define name="CORRECTION_LEFT" value="1."/>
|
||||
<define name="CORRECTION_RIGHT" value="1."/>
|
||||
|
||||
<define name="LATERAL_CORRECTION" value="-1"/>
|
||||
<define name="LONGITUDINAL_CORRECTION" value="1"/>
|
||||
<define name="VERTICAL_CORRECTION" value="1.7"/>
|
||||
|
||||
<define name="HORIZ_SENSOR_TILTED" value="1"/>
|
||||
<define name="IR1_SIGN" value="-1"/>
|
||||
<define name="IR2_SIGN" value="1"/>
|
||||
<define name="TOP_SIGN" value="1"/>
|
||||
|
||||
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/>
|
||||
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/>
|
||||
</section>
|
||||
|
||||
<section name="BAT">
|
||||
<define name="MILLIAMP_AT_FULL_THROTTLE" value="20000"/>
|
||||
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
|
||||
<!-- 0.0247311828 -->
|
||||
<!-- 0.02432905 -->
|
||||
<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
|
||||
</section>
|
||||
|
||||
<section name="MISC">
|
||||
<define name="MINIMUM_AIRSPEED" value="10." unit="m/s"/>
|
||||
<define name="NOMINAL_AIRSPEED" value="12." unit="m/s"/>
|
||||
<define name="MAXIMUM_AIRSPEED" value="18." 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="XBEE_INIT" value=""ATPL2\rATRN1\rATTT80\r""/> -->
|
||||
<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
|
||||
<define name="ALT_KALMAN_ENABLED" value="FALSE"/>
|
||||
|
||||
<define name="TRIGGER_DELAY" value="1."/>
|
||||
<define name="DEFAULT_CIRCLE_RADIUS" value="120."/>
|
||||
<define name="MIN_CIRCLE_RADIUS" value="50."/>
|
||||
</section>
|
||||
|
||||
|
||||
<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="-0.06"/>
|
||||
<!-- outer loop saturation -->
|
||||
<define name="ALTITUDE_MAX_CLIMB" value="2."/>
|
||||
|
||||
<!-- auto throttle inner loop -->
|
||||
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.45"/>
|
||||
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/>
|
||||
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.85"/>
|
||||
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1000"/>
|
||||
<define name="AUTO_THROTTLE_DASH_TRIM" value="-1200"/>
|
||||
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.2" unit="%/(m/s)"/>
|
||||
<define name="AUTO_THROTTLE_PGAIN" value="-0.023"/>
|
||||
<define name="AUTO_THROTTLE_IGAIN" value="0.1"/>
|
||||
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/>
|
||||
|
||||
<!-- auto pitch inner loop -->
|
||||
<define name="AUTO_PITCH_PGAIN" value="-0.06"/>
|
||||
<define name="AUTO_PITCH_IGAIN" value="0.08"/>
|
||||
<define name="AUTO_PITCH_MAX_PITCH" value="0.35"/>
|
||||
<define name="AUTO_PITCH_MIN_PITCH" value="-0.35"/>
|
||||
|
||||
<define name="THROTTLE_SLEW" value="0.1"/>
|
||||
|
||||
</section>
|
||||
|
||||
|
||||
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
|
||||
<define name="COURSE_PGAIN" value="-1.0"/>
|
||||
<define name="ROLL_MAX_SETPOINT" value="0.60" unit="radians"/>
|
||||
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
|
||||
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="radians"/>
|
||||
|
||||
<define name="ROLL_PGAIN" value="6000."/>
|
||||
<define name="AILERON_OF_THROTTLE" value="0.0"/>
|
||||
<define name="PITCH_PGAIN" value="-9000."/>
|
||||
<define name="PITCH_DGAIN" value="1.5"/>
|
||||
|
||||
<define name="ELEVATOR_OF_ROLL" value="1500"/>
|
||||
|
||||
<!--define name="ROLL_ATTITUDE_GAIN" value="-5900"/>
|
||||
<define name="ROLL_RATE_GAIN" value="-2900"/-->
|
||||
</section>
|
||||
|
||||
<section name="NAV">
|
||||
<define name="NAV_PITCH" value="0."/>
|
||||
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
|
||||
</section>
|
||||
|
||||
<section name="AGGRESSIVE" prefix="AGR_">
|
||||
<define name="BLEND_START" value="50"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
|
||||
<define name="BLEND_END" value="15"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
|
||||
<define name="CLIMB_THROTTLE" value="0.9"/><!-- Gaz for Aggressive Climb -->
|
||||
<define name="CLIMB_PITCH" value="0.35"/><!-- Pitch for Aggressive Climb -->
|
||||
<define name="DESCENT_THROTTLE" value="0.05"/><!-- Gaz for Aggressive Decent -->
|
||||
<define name="DESCENT_PITCH" value="-0.35"/><!-- 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>
|
||||
|
||||
<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="0.17" unit="rad"/>
|
||||
<define name="DEFAULT_PITCH" value="0.08" unit="rad"/>
|
||||
<define name="HOME_RADIUS" value="100" unit="m"/>
|
||||
</section>
|
||||
|
||||
<section name="DATALINK" prefix="DATALINK_">
|
||||
<define name="DEVICE_TYPE" value="XBEE"/>
|
||||
<define name="DEVICE_ADDRESS" value="...."/>
|
||||
</section>
|
||||
<makefile>
|
||||
CONFIG = \"tiny_2_1.h\"
|
||||
|
||||
include $(PAPARAZZI_SRC)/conf/autopilot/tiny.makefile
|
||||
|
||||
FLASH_MODE=IAP
|
||||
|
||||
ap.CFLAGS += -DFBW -DAP -DBOARD_CONFIG=$(CONFIG) -DLED -DTIME_LED=1
|
||||
ap.srcs = sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c main_fbw.c main_ap.c main.c
|
||||
|
||||
ap.srcs += commands.c
|
||||
|
||||
ap.CFLAGS += -DACTUATORS=\"servos_4017_hw.h\" -DSERVOS_4017
|
||||
ap.srcs += $(SRC_ARCH)/servos_4017_hw.c actuators.c
|
||||
|
||||
ap.CFLAGS += -DRADIO_CONTROL -DUSE_RC_TELEMETRY
|
||||
ap.srcs += radio_control.c ppm_telemetry.c
|
||||
|
||||
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
|
||||
ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
|
||||
|
||||
#TRANSPARENT
|
||||
#ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart1 -#DDOWNLINK_AP_DEVICE=Uart1 -DPPRZ_UART=Uart1 -DDATALINK=PPRZ -DUART1_BAUD=B9600
|
||||
#ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c pprz_transport.c
|
||||
|
||||
ap.CFLAGS += -DINTER_MCU
|
||||
ap.srcs += inter_mcu.c
|
||||
|
||||
ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2 -DUSE_ADC_3
|
||||
ap.srcs += $(SRC_ARCH)/adc_hw.c
|
||||
|
||||
ap.CFLAGS += -DGPS -DUBX -DUSE_UART0 -DGPS_LINK=Uart0 -DUART0_BAUD=B38400
|
||||
# -DGPS_USE_LATLONG
|
||||
ap.srcs += gps_ubx.c gps.c latlong.c
|
||||
|
||||
ap.CFLAGS += -DINFRARED -DALT_KALMAN -DWIND_INFO -DWIND_INFO_RET
|
||||
ap.srcs += infrared.c estimator.c
|
||||
|
||||
ap.CFLAGS += -DNAV -DAGR_CLIMB -DLOITER_TRIM
|
||||
ap.srcs += nav.c fw_h_ctl.c fw_v_ctl.c
|
||||
|
||||
ap.srcs += nav_line.c
|
||||
ap.srcs += nav_survey_rectangle.c
|
||||
|
||||
ap.srcs += snav.c
|
||||
|
||||
# Config for SITL simulation
|
||||
# include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
|
||||
sim.ARCHDIR = $(ARCHI)
|
||||
sim.ARCH = sitl
|
||||
sim.TARGET = autopilot
|
||||
sim.TARGETDIR = autopilot
|
||||
sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DINFRARED -DNAV -DLED -DWIND_INFO
|
||||
sim.srcs = latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl.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 $(SRC_ARCH)/led_hw.c
|
||||
|
||||
sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
|
||||
sim.srcs += nav_line.c nav_survey_rectangle.c
|
||||
|
||||
</makefile>
|
||||
</airframe>
|
||||
|
||||
@@ -0,0 +1,227 @@
|
||||
<!DOCTYPE airframe SYSTEM "airframe.dtd">
|
||||
|
||||
<!-- mini wing, 3A brushless
|
||||
Tiny 2.11 board, LEA 5H
|
||||
PerkinElmer TPS334 IR Sensors
|
||||
Tilted infrared sensor
|
||||
XBee modem
|
||||
-->
|
||||
|
||||
<airframe name="mini wing">
|
||||
|
||||
<!-- commands section -->
|
||||
<servos>
|
||||
<servo name="MOTOR" no="0" min="1000" neutral="1000" max="2000"/>
|
||||
<servo name="AILEVON_LEFT" no="2" min="1720" neutral="1341" max="1000"/>
|
||||
<servo name="AILEVON_RIGHT" no="6" min="1220" neutral="1523" max="1840"/>
|
||||
</servos>
|
||||
|
||||
<commands>
|
||||
<axis name="THROTTLE" failsafe_value="0"/>
|
||||
<axis name="ROLL" failsafe_value="0"/>
|
||||
<axis name="PITCH" failsafe_value="0"/>
|
||||
</commands>
|
||||
|
||||
<rc_commands>
|
||||
<set command="THROTTLE" value="@THROTTLE"/>
|
||||
<set command="ROLL" value="@ROLL"/>
|
||||
<set command="PITCH" value="@PITCH"/>
|
||||
</rc_commands>
|
||||
|
||||
<section name="MIXER">
|
||||
<define name="AILEVON_AILERON_RATE" value="0.45"/>
|
||||
<define name="AILEVON_ELEVATOR_RATE" value="0.8"/>
|
||||
</section>
|
||||
|
||||
<command_laws>
|
||||
<let var="aileron" value="@ROLL * AILEVON_AILERON_RATE"/>
|
||||
<let var="elevator" value="@PITCH * AILEVON_ELEVATOR_RATE"/>
|
||||
<set servo="MOTOR" value="@THROTTLE"/>
|
||||
<set servo="AILEVON_LEFT" value="$elevator + $aileron"/>
|
||||
<set servo="AILEVON_RIGHT" value="$elevator - $aileron"/>
|
||||
</command_laws>
|
||||
|
||||
<section name="AUTO1" prefix="AUTO1_">
|
||||
<define name="MAX_ROLL" value="0.85"/>
|
||||
<define name="MAX_PITCH" value="0.6"/>
|
||||
</section>
|
||||
|
||||
<section name="adc" prefix="ADC_CHANNEL_">
|
||||
<define name="IR1" value="ADC_1"/>
|
||||
<define name="IR2" value="ADC_2"/>
|
||||
<define name="IR_TOP" value="ADC_0"/>
|
||||
<define name="ACC_X" value="ADC_3"/>
|
||||
<define name="ACC_Y" value="ADC_4"/>
|
||||
<define name="IR_NB_SAMPLES" value="16"/>
|
||||
</section>
|
||||
|
||||
<section name="INFRARED" prefix="IR_">
|
||||
<define name="ADC_IR1_NEUTRAL" value="512"/>
|
||||
<define name="ADC_IR2_NEUTRAL" value="512"/>
|
||||
<define name="ADC_TOP_NEUTRAL" value="512"/>
|
||||
|
||||
<define name="CORRECTION_UP" value="1."/>
|
||||
<define name="CORRECTION_DOWN" value="1."/>
|
||||
<define name="CORRECTION_LEFT" value="1."/>
|
||||
<define name="CORRECTION_RIGHT" value="1."/>
|
||||
|
||||
<define name="LATERAL_CORRECTION" value="-1"/>
|
||||
<define name="LONGITUDINAL_CORRECTION" value="1"/>
|
||||
<define name="VERTICAL_CORRECTION" value="1.5"/>
|
||||
|
||||
<define name="HORIZ_SENSOR_TILTED" value="1"/>
|
||||
<define name="IR1_SIGN" value="-1"/>
|
||||
<define name="IR2_SIGN" value="1"/>
|
||||
<define name="TOP_SIGN" value="-1"/>
|
||||
|
||||
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/>
|
||||
<define name="PITCH_NEUTRAL_DEFAULT" value="3.4" unit="deg"/>
|
||||
</section>
|
||||
|
||||
<section name="BAT">
|
||||
<define name="MILLIAMP_AT_FULL_THROTTLE" value="2100."/>
|
||||
<define name="CATASTROPHIC_BAT_LEVEL" value="6.2" unit="V"/>
|
||||
<define name="VoltageOfAdc(adc)" value="(0.02454*adc)"/>
|
||||
</section>
|
||||
|
||||
<section name="MISC">
|
||||
<define name="NOMINAL_AIRSPEED" value="12." 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="XBEE_INIT" value=""ATPL2\rATRN1\rATTT80\r""/> -->
|
||||
<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
|
||||
<define name="ALT_KALMAN_ENABLED" value="FALSE"/>
|
||||
|
||||
<define name="TRIGGER_DELAY" value="1."/>
|
||||
<define name="DEFAULT_CIRCLE_RADIUS" value="60."/>
|
||||
<define name="MIN_CIRCLE_RADIUS" value="50."/>
|
||||
</section>
|
||||
|
||||
<section name="VERTICAL CONTROL" prefix="V_CTL_">
|
||||
|
||||
<define name="POWER_CTL_BAT_NOMINAL" value="7.4" unit="volt"/>
|
||||
<!-- outer loop proportional gain -->
|
||||
<define name="ALTITUDE_PGAIN" value="-0.06"/> <!-- -0.024 -->
|
||||
<!-- outer loop saturation -->
|
||||
<define name="ALTITUDE_MAX_CLIMB" value="2."/>
|
||||
|
||||
<!-- auto throttle inner loop -->
|
||||
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.7"/>
|
||||
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.35"/>
|
||||
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.80"/>
|
||||
<define name="AUTO_THROTTLE_LOITER_TRIM" value="50"/>
|
||||
<define name="AUTO_THROTTLE_DASH_TRIM" value="-60"/>
|
||||
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.2" unit="%/(m/s)"/>
|
||||
<define name="AUTO_THROTTLE_PGAIN" value="-0.023"/> <!-- -0.012 -->
|
||||
<define name="AUTO_THROTTLE_IGAIN" value="0.11"/>
|
||||
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.1"/>
|
||||
|
||||
<!-- auto pitch inner loop -->
|
||||
<define name="AUTO_PITCH_PGAIN" value="-0.06"/> <!-- -0.03 -->
|
||||
<define name="AUTO_PITCH_IGAIN" value="0.0"/>
|
||||
<define name="AUTO_PITCH_MAX_PITCH" value="0.35"/>
|
||||
<define name="AUTO_PITCH_MIN_PITCH" value="-0.35"/>
|
||||
|
||||
<define name="THROTTLE_SLEW" value="0.1"/>
|
||||
|
||||
</section>
|
||||
|
||||
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
|
||||
<define name="COURSE_PGAIN" value="-0.8"/>
|
||||
<define name="ROLL_MAX_SETPOINT" value="0.62" unit="radians"/> <!-- 0.5 -->
|
||||
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
|
||||
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="radians"/>
|
||||
|
||||
<define name="ROLL_PGAIN" value="6600."/>
|
||||
<define name="AILERON_OF_THROTTLE" value="0.0"/>
|
||||
<define name="PITCH_PGAIN" value="-5500."/>
|
||||
<define name="PITCH_DGAIN" value="0.4"/>
|
||||
|
||||
<define name="ELEVATOR_OF_ROLL" value="1200"/>
|
||||
|
||||
<!--define name="ROLL_ATTITUDE_GAIN" value="-7500"/>
|
||||
<define name="ROLL_RATE_GAIN" value="-1500"/-->
|
||||
|
||||
</section>
|
||||
|
||||
<section name="NAV">
|
||||
<define name="NAV_PITCH" value="0."/>
|
||||
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
|
||||
</section>
|
||||
|
||||
<section name="AGGRESSIVE" prefix="AGR_">
|
||||
<define name="BLEND_START" value="50"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
|
||||
<define name="BLEND_END" value="15"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
|
||||
<define name="CLIMB_THROTTLE" value="0.9"/><!-- Gaz for Aggressive Climb -->
|
||||
<define name="CLIMB_PITCH" value="0.35"/><!-- Pitch for Aggressive Climb -->
|
||||
<define name="DESCENT_THROTTLE" value="0.05"/><!-- Gaz for Aggressive Decent -->
|
||||
<define name="DESCENT_PITCH" value="-0.35"/><!-- 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>
|
||||
|
||||
<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"/>
|
||||
<define name="HOME_RADIUS" value="100" unit="m"/>
|
||||
</section>
|
||||
|
||||
<section name="DATALINK" prefix="DATALINK_">
|
||||
<define name="DEVICE_TYPE" value="XBEE"/>
|
||||
<define name="DEVICE_ADDRESS" value="...."/>
|
||||
</section>
|
||||
|
||||
<makefile>
|
||||
CONFIG = \"tiny_2_1.h\"
|
||||
|
||||
include $(PAPARAZZI_SRC)/conf/autopilot/tiny.makefile
|
||||
|
||||
FLASH_MODE=IAP
|
||||
|
||||
ap.CFLAGS += -DFBW -DAP -DBOARD_CONFIG=$(CONFIG) -DLED -DTIME_LED=1
|
||||
ap.srcs = sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c main_fbw.c main_ap.c main.c
|
||||
|
||||
ap.srcs += commands.c
|
||||
|
||||
ap.CFLAGS += -DACTUATORS=\"servos_4017_hw.h\" -DSERVOS_4017
|
||||
ap.srcs += $(SRC_ARCH)/servos_4017_hw.c actuators.c
|
||||
|
||||
ap.CFLAGS += -DRADIO_CONTROL -DUSE_RC_TELEMETRY
|
||||
ap.srcs += radio_control.c ppm_telemetry.c
|
||||
|
||||
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
|
||||
ap.srcs += downlink.c $(SRC_ARCH)/uart_hw.c datalink.c xbee.c
|
||||
|
||||
ap.CFLAGS += -DINTER_MCU
|
||||
ap.srcs += inter_mcu.c
|
||||
|
||||
ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2
|
||||
ap.srcs += $(SRC_ARCH)/adc_hw.c
|
||||
|
||||
ap.CFLAGS += -DGPS -DUBX -DUSE_UART0 -DGPS_LINK=Uart0 -DUART0_BAUD=B38400 -DGPS_USE_LATLONG
|
||||
# -DGPS_LED=2
|
||||
ap.srcs += gps_ubx.c gps.c latlong.c
|
||||
|
||||
ap.CFLAGS += -DINFRARED -DALT_KALMAN -DWIND_INFO -DWIND_INFO_RET
|
||||
ap.srcs += infrared.c estimator.c
|
||||
|
||||
ap.CFLAGS += -DNAV -DAGR_CLIMB -DLOITER_TRIM
|
||||
ap.srcs += nav.c fw_h_ctl.c fw_v_ctl.c
|
||||
|
||||
ap.srcs += nav_line.c
|
||||
ap.srcs += nav_survey_rectangle.c
|
||||
|
||||
#ap.CFLAGS += -DTELEMETRY_MODE_FBW=1
|
||||
|
||||
ap.CFLAGS += -DUSE_ACCEL_MEMSIC -DUSE_ADC_3 -DUSE_ADC_4
|
||||
|
||||
# Config for SITL simulation
|
||||
include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
|
||||
sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
|
||||
sim.srcs += nav_line.c nav_survey_rectangle.c
|
||||
|
||||
</makefile>
|
||||
</airframe>
|
||||
Reference in New Issue
Block a user