Files
paparazzi/conf/airframes/ENAC/fixed-wing/overview.xml
T
Felix Ruess dd15598389 Merge branch 'dev' into positive_control_gains
Conflicts:
	conf/airframes/ENAC/fixed-wing/funjet2.xml
	conf/airframes/ENAC/fixed-wing/funjet2_nc.xml
	conf/airframes/ENAC/fixed-wing/funjet2_new.xml
	conf/airframes/ENAC/fixed-wing/funjet3.xml
	conf/airframes/ENAC/fixed-wing/merlin.xml
	conf/airframes/ENAC/fixed-wing/minimag1.xml
	conf/airframes/ENAC/fixed-wing/obsolete/drops.xml
	conf/airframes/ENAC/fixed-wing/overview.xml
	conf/airframes/ENAC/fixed-wing/soarzi.xml
	conf/airframes/ENAC/fixed-wing/weasel.xml
	conf/airframes/LAAS/mmlaas_N1.xml
	conf/airframes/LAAS/mmlaas_N2.xml
	conf/airframes/LAAS/mmlaas_N3.xml
	conf/airframes/Poine/funjet42.xml
	conf/airframes/Poine/swift_1.xml
	conf/airframes/TU_Delft/MicrojetBR.xml
	conf/airframes/delta_wing_minimal_example.xml
	conf/airframes/easystar_ets_example.xml
	conf/airframes/easystar_example.xml
	conf/airframes/example_twog_analogimu.xml
	conf/airframes/funjet_cam_example.xml
	conf/airframes/funjet_example.xml
	conf/airframes/mm/extra/press_t.xml
	conf/airframes/mm/extra/probe_t.xml
	conf/airframes/mm/extra/turbine_trigger.xml
	conf/airframes/mm/fixed-wing/drops.xml
	conf/airframes/mm/fixed-wing/funjet43.xml
	conf/airframes/mm/fixed-wing/funjetdca.xml
	conf/airframes/mm/fixed-wing/funjetdcb.xml
	conf/airframes/mm/fixed-wing/funjetdcc.xml
	conf/airframes/mm/fixed-wing/funjeteth1.xml
	conf/airframes/mm/fixed-wing/funjeteth2.xml
	conf/airframes/mm/fixed-wing/funjetfmi1.xml
	conf/airframes/mm/fixed-wing/funjetfmi2.xml
	conf/airframes/mm/fixed-wing/funjetfmi3.xml
	conf/airframes/mm/fixed-wing/funjetgfi1.xml
	conf/airframes/mm/fixed-wing/funjetgfi3.xml
	conf/airframes/mm/fixed-wing/funjetgfi4.xml
	conf/airframes/mm/fixed-wing/funjetgfi5.xml
	conf/airframes/mm/fixed-wing/funjetgfi6.xml
	conf/airframes/mm/fixed-wing/funjetgfi7.xml
	conf/airframes/mm/fixed-wing/funjetgfi8.xml
	conf/airframes/mm/fixed-wing/funjetgfi9.xml
	conf/airframes/mm/fixed-wing/funjetlisa.xml
	conf/airframes/mm/fixed-wing/funjetlisam.xml
	conf/airframes/mm/fixed-wing/funjetmm.xml
	conf/airframes/mm/fixed-wing/funjetmm2.xml
	conf/airframes/mm/fixed-wing/fw_ins_arduimu.xml
	conf/airframes/mm/fixed-wing/merlin.xml
	conf/airframes/mm/fixed-wing/miniwing.xml
	conf/airframes/mm/fixed-wing/slowfast.xml
	conf/airframes/mm/fixed-wing/slowfast2.xml
	conf/airframes/mm/fixed-wing/twinstarmm.xml
	conf/airframes/mm/hangar/black_one.xml
	conf/airframes/mm/hangar/glass_one1.xml
	conf/airframes/mm/hangar/glass_one2.xml
	conf/airframes/mm/hangar/glass_one3.xml
	conf/airframes/mm/hangar/lila.xml
	conf/airframes/mm/hangar/mac06a.xml
	conf/airframes/mm/hangar/red_one.xml
	conf/airframes/obsolete/easystar2.xml
	conf/airframes/obsolete/kalscott_easystar.xml
	conf/airframes/obsolete/microjet5_tp_auto.xml
	conf/airframes/obsolete/microjet6.xml
	conf/airframes/obsolete/microjetII.xml
	conf/airframes/obsolete/minimag1.xml
	conf/airframes/obsolete/minimag_fs.xml
	conf/airframes/obsolete/mmlaas_N1_carto_cam.xml
	conf/airframes/obsolete/storm1.xml
	conf/airframes/obsolete/tiny2.xml
	conf/airframes/obsolete/xxx1.xml
	conf/airframes/test_hb.xml
	conf/airframes/twinstar_example.xml
	conf/airframes/usb_test.xml
	conf/settings/tuning_ctl_adaptive.xml
	sw/airborne/firmwares/fixedwing/stabilization/stabilization_adaptive.c
2012-02-02 15:44:09 +01:00

188 lines
6.9 KiB
XML

<!DOCTYPE airframe SYSTEM "../../airframe.dtd">
<!-- Twinstar II, 2x Jeti 18 advance plus, AXI 2212/26
Tiny 2.11
ArduIMU
XBee modem with API Mode
LEA 5H GPS
-->
<airframe name="Twinstar">
<modules>
<load name="ins_arduimu_basic.xml">
<define name="USE_HIGH_ACCEL_FLAG"/>
</load>
<load name="cam_point.xml">
<define name="POINT_CAM_ROLL"/>
</load>
<!--load name="cam_segment.xml"/-->
</modules>
<firmware name="fixedwing">
<target name="ap" board="tiny_2.11"/>
<target name="sim" board="pc"/>
<define name="LOITER_TRIM"/>
<define name="ALT_KALMAN"/>
<define name="AGR_CLIMB"/>
<define name="USE_I2C0"/>
<subsystem name="radio_control" type="ppm"/>
<subsystem name="telemetry" type="xbee_api"/>
<subsystem name="control"/>
<subsystem name="gps" type="ublox"/>
<subsystem name="navigation"/>
</firmware>
<firmware name="setup">
<target name="tunnel" board="tiny_2.11"/>
<target name="setup_actuators" board="tiny_2.11"/>
</firmware>
<!-- commands section -->
<servos>
<servo name="MOTOR" no="2" min="1000" neutral="1000" max="2000"/>
<servo name="AILERON_RIGHT" no="7" min="1000" neutral="1500" max="2000"/>
<servo name="AILERON_LEFT" no="6" min="1000" neutral="1500" max="2000"/>
<servo name="ELEVATOR" no="3" min="2000" neutral="1500" max="1000"/>
<servo name="RUDDER" no="4" min="1000" neutral="1500" max="2000"/>
<servo name="CAM_TILT" no="1" min="1000" neutral="1500" max="2000"/>
</servos>
<commands>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="CAM_TILT" failsafe_value="0"/>
</commands>
<rc_commands>
<set command="THROTTLE" value="@THROTTLE"/>
<set command="ROLL" value="@ROLL"/>
<set command="PITCH" value="@PITCH"/>
<set command="YAW" value="@YAW"/>
<set command="CAM_TILT" value="@GAIN1"/>
</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"/>
<set servo="RUDDER" value="@YAW"/>
<set servo="CAM_TILT" value="@CAM_TILT"/>
</command_laws>
<section name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.85"/>
<define name="MAX_PITCH" value="0.6"/>
</section>
<section name="INS" prefix="INS_">
<define name="ROLL_NEUTRAL_DEFAULT" value="0." unit="rad"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="0." unit="rad"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="20000"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
</section>
<section name="CAM" prefix="CAM_">
<define name="TILT_MAX" value="45" unit="deg" code_unit="deg"/>
<define name="TILT_NEUTRAL" value="0" unit="deg" code_unit="deg"/>
<define name="TILT_MIN" value="-45" unit="deg" code_unit="deg"/>
<define name="TILT0" value="0" unit="deg" code_unit="deg"/>
</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="ALT_KALMAN_ENABLED" value="FALSE"/>
<define name="TRIGGER_DELAY" value="1."/>
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
</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="0.0"/>
<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="1.0"/>
<define name="ROLL_MAX_SETPOINT" value="0.60" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="ROLL_ATTITUDE_GAIN" value="9000."/>
<define name="ROLL_RATE_GAIN" value="3000."/>
<define name="PITCH_PGAIN" value="9000."/>
<define name="PITCH_DGAIN" value="0.4"/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<define name="ELEVATOR_OF_ROLL" 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="0.17" unit="rad"/>
<define name="DEFAULT_PITCH" value="0.08" unit="rad"/>
<define name="HOME_RADIUS" value="100" unit="m"/>
</section>
</airframe>