mirror of
https://github.com/paparazzi/paparazzi.git
synced 2026-05-09 22:49:53 +08:00
Felix Ruess
225 lines
8.4 KiB
XML
225 lines
8.4 KiB
XML
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
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<!-- Funjet Multiplex (http://www.multiplex-rc.de/)
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Tiny 2.1 board (http://paparazzi.enac.fr/wiki/index.php/Tiny_v2)
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Tilted infrared sensor (http://paparazzi.enac.fr/wiki/index.php/Image:Tiny_v2_1_Funjet.jpg)
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Radiotronix modem
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-->
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<airframe name="JSBSim test file (from funjet file)">
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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="1130" neutral="1500" max="1880"/>
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<servo name="AILEVON_RIGHT" no="6" min="1980" neutral="1515" 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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</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_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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<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="1.5"/>
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<define name="HORIZ_SENSOR_TILTED" 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="-3.6" unit="deg"/>
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<define name="PITCH_NEUTRAL_DEFAULT" value="6" 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="520"/>
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<define name="ADC_TEMP_NEUTRAL" value="476"/>
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<define name="ADC_TEMP_SLOPE" value="0"/>
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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="MILLIAMP_AT_FULL_THROTTLE" value="20000"/>
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<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
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</section>
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<section name="MISC">
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<define name="NOMINAL_AIRSPEED" value="17." unit="m/s"/>
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<define name="MINIMUM_AIRSPEED" value="17." unit="m/s"/>
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<define name="MAXIMUM_AIRSPEED" value="17." unit="m/s"/>
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<define name="CARROT" value="5." unit="s"/>
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<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
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<define name="CONTROL_RATE" value="60" unit="Hz"/>
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<!-- <define name="XBEE_INIT" value=""ATPL2\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="150."/>
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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="0.300000011921"/>
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<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.3"/>
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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="0.37"/>
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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="-1."/>
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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="-50000"/>
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<define name="PITCH_DGAIN" value="0"/>
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<define name="ELEVATOR_OF_ROLL" value="2500"/>
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<define name="ROLL_ATTITUDE_GAIN" value="-20000"/>
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<define name="ROLL_RATE_GAIN" value="0"/>
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<define name="ROLL_KFFP" value="-500"/>
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<define name="ROLL_KFFD" value="0"/>
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<define name="ROLL_IGAIN" value="-5000"/>
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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="0.7"/><!-- Gaz for Aggressive Climb -->
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<define name="CLIMB_PITCH" value="0.25"/><!-- 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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<!--
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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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-->
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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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<section name="SIMU">
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<!--define name="JSBSIM_MODEL" value=""fulmar""/-->
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<define name="JSBSIM_MODEL" value=""Malolo1""/>
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<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
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<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
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</section>
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<makefile>
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# Config for SITL simulation with JSBSim
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include $(PAPARAZZI_SRC)/conf/autopilot/sitl_jsbsim.makefile
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sim.CFLAGS += -I/home/cocoleon/usr/include/JSBSim
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sim.LDFLAGS += -L/home/cocoleon/usr/lib/
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sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
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sim.srcs += subsystems/navigation/nav_line.c subsystems/navigation/nav_survey_rectangle.c
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sim.srcs += $(SIMDIR)/sim_ac_fw.c
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</makefile>
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</airframe>
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