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Merge branch 'positive_control_gains' into rotorcraft_positive_control_gains

Browse Source 
Conflicts:
	sw/airborne/math/pprz_algebra.h
This commit is contained in:
Felix Ruess
2012-02-02 15:49:17 +01:00
parent dd4f6b0a78 dd15598389
commit ea47766125
714 changed files with 6446 additions and 16214 deletions
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.gitignore
+10
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@@ -1,3 +1,6 @@
# ignore html dir for github pages
/doc/html
*.so
*.[oa]
*.out
@@ -17,6 +20,13 @@
*.aux
# Eclipse IDE project files
*.cproject
*.project
*.externalToolBuilders
/build.properties
/META-INF
# Debian related files
*.deb
*.dsc
Doxyfile
+272 -104
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File diff suppressed because it is too large Load Diff
README
+3 -7
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@@ -1,5 +1,4 @@
# Paparazzi $Id$
# Copyright (C) 2003-2010 The Paparazzi Team
# Copyright (C) 2003-2011 The Paparazzi Team
#
# This file is part of Paparazzi.
#
@@ -25,7 +24,7 @@ Intro
Paparazzi is an attempt to develop a free software Unmanned (Air) Vehicle System.
As of today the system is being used successfuly by a number of hobyists, universities and companies all over the world, on vehicle of various size ( 100g to 25Kg ) and of various nature ( fixed wing, rotorcrafts, boats and surface vehicles).
Up to date informations are available from the wiki website
Up to date information is available from the wiki website
http://paparazzi.enac.fr
@@ -39,8 +38,6 @@ conf: the configuration directory (airframe, radio, ... descriptions).
data: where to put read-only data (e.g. maps, terrain elevation files, icons)
hw: hardware (electronic schemas, PCBs, ...)
sw: software (onboard, ground station, simulation, ...)
var: products of compilation, cache for the map tiles, ...
@@ -64,8 +61,7 @@ For Debian or Ubuntu users, required packages are available at
- "paparazzi-dev" will provide everything needed to compile and run the ground segment and the simulator. If something is missing, please report it.
- "paparazzi-arm7" is required to compile the code for LPC21 based boards ( tiny, twog, booz, etc).
- "paparazzi-stm32" is needed for building code for STM32 based boards (lisa/L, lisa/M)
- "paparazzi-arm-multilib" is required to compile the code for LPC21 and STM32 based boards
- "paparazzi-omap" is needed for building code for the optional Gumstix Overo module available on lisa/L
- "paparazzi-jsbsim" is needed for using jsbsim as flight dynamic model for the simulator.
conf/airframes/CDW/ChimuJTinyFwSpi.xml
+195
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@@ -0,0 +1,195 @@
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<!--
YAPA + XSens + XBee
-->
<airframe name="Yapa v1">
<servos>
<servo name="THROTTLE" no="0" min="1000" neutral="1000" max="2000"/>
<servo name="AILERON_LEFT" no="1" min="1000" neutral="1500" max="2000"/>
<servo name="AILERON_RIGHT" no="2" min="2000" neutral="1500" max="1000"/>
<servo name="ELEVATOR" no="3" min="2000" neutral="1500" max="1000"/>
<servo name="RUDDER" no="4" min="1100" neutral="1500" max="1900"/>
</servos>
<commands>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="BRAKE" failsafe_value="0"/> <!-- both elerons up as butterfly brake ? -->
</commands>
<rc_commands>
<set command="THROTTLE" value="@THROTTLE"/>
<set command="ROLL" value="@ROLL"/>
<set command="PITCH" value="@PITCH"/>
<set command="BRAKE" value="@YAW"/>
</rc_commands>
<section name="SERVO_MIXER_GAINS">
<define name="AILERON_RATE_UP" value="0.50f"/>
<define name="AILERON_RATE_DOWN" value="0.25f"/>
<define name="AILERON_RATE_UP_BRAKE" value="0.5f"/>
<define name="AILERON_RATE_DOWN_BRAKE" value="0.9f"/>
<define name="PITCH_GAIN" value="0.9f"/>
<define name="YAW_THRUST" value="0.0f"/>
<define name="BRAKE_AILEVON" value="-0.68f"/>
<define name="BRAKE_PITCH" value="0.0f"/>
<define name="MAX_BRAKE_RATE" value="150"/>
<define name="LIMIT(X,XL,XH)" value="( ((X)>(XH)) ? (XH) : ( ((X)>(XL)) ? (X) : (XL) ) )"/>
</section>
<command_laws>
<!-- Differential Aileron Depending on Brake Value -->
<set servo="AILERON_LEFT" value="@ROLL"/>
<set servo="AILERON_RIGHT" value="@ROLL"/>
<!-- Differential Thurst -->
<set servo="THROTTLE" value="@THROTTLE"/>
<!-- Pitch with Brake-Trim Function -->
<set servo="ELEVATOR" value="@PITCH"/>
</command_laws>
<section name="INS" prefix="INS_">
<define name="ROLL_NEUTRAL_DEFAULT" value="0" unit="deg"/>
<define name="PITCH_NEUTRAL_DEFAULT" value="0" unit="deg"/>
</section>
<section name="AUTO1" prefix="AUTO1_">
<define name="MAX_ROLL" value="0.7"/>
<define name="MAX_PITCH" value="0.7"/>
</section>
<section name="BAT">
<define name="MilliAmpereOfAdc(adc)" value="((adc) - 505) * 124.0f"/>
<define name="LOW_BAT_LEVEL" value="10.5" unit="V"/>
<define name="CRITIC_BAT_LEVEL" value="10" unit="V"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.1" unit="V"/>
</section>
<section name="MISC">
<define name="NOMINAL_AIRSPEED" value="13." unit="m/s"/>
<define name="CARROT" value="5." unit="s"/>
<define name="CONTROL_RATE" value="60" unit="Hz"/>
<define name="XBEE_INIT" value="&quot;ATPL2\rATRN5\rATTT80\r&quot;"/>
<!-- <define name="NO_XBEE_API_INIT" value="TRUE"/> -->
<define name="ALT_KALMAN_ENABLED" value="TRUE"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="GLIDE_AIRSPEED" value="10"/>
<define name="GLIDE_VSPEED" value="3."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
</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="-0.03"/>
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="2."/>
<!-- auto throttle inner loop -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.32"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.25"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.65"/>
<define name="AUTO_THROTTLE_LOITER_TRIM" value="1500"/>
<define name="AUTO_THROTTLE_DASH_TRIM" value="-4000"/>
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.15" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PGAIN" value="-0.01"/>
<define name="AUTO_THROTTLE_IGAIN" value="0.1"/>
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.05"/>
<define name="THROTTLE_SLEW_LIMITER" value="2" unit="s"/>
</section>
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="-1.20000004768"/>
<define name="COURSE_DGAIN" value="0.3"/>
<define name="COURSE_PRE_BANK_CORRECTION" value="0.2"/>
<define name="ROLL_MAX_SETPOINT" value="0.9" unit="radians"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="radians"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="radians"/>
<define name="PITCH_PGAIN" value="-12000."/>
<define name="PITCH_DGAIN" value="0"/>
<define name="ELEVATOR_OF_ROLL" value="1000."/>
<define name="ROLL_ATTITUDE_GAIN" value="-11500"/>
<define name="ROLL_RATE_GAIN" value="-600."/>
</section>
<section name="AGGRESSIVE" prefix="AGR_">
<define name="BLEND_START" value="20"/><!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
<define name="BLEND_END" value="10"/><!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
<define name="CLIMB_THROTTLE" value="1.00"/><!-- Gaz for Aggressive Climb -->
<define name="CLIMB_PITCH" value="0.3"/><!-- Pitch for Aggressive Climb -->
<define name="DESCENT_THROTTLE" value="0.1"/><!-- Gaz for Aggressive Decent -->
<define name="DESCENT_PITCH" value="-0.25"/><!-- 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="DEFAULT_THROTTLE" value="0.35" unit="%"/>
<define name="DEFAULT_ROLL" value="0.17" unit="rad"/>
<define name="DEFAULT_PITCH" value="0.08" unit="rad"/>
<define name="HOME_RADIUS" value="DEFAULT_CIRCLE_RADIUS" unit="m"/>
<define name="KILL_MODE_DISTANCE" value="(MAX_DIST_FROM_HOME*1.5)"/>
<define name="DELAY_WITHOUT_GPS" value="3" unit="s"/>
</section>
<section name="DIGITAL_CAMERA" prefix="DC_">
<define name="AUTOSHOOT_QUARTERSEC_PERIOD" value="6" unit="quarter_second"/>
<define name="AUTOSHOOT_METER_GRID" value="50" unit="meter"/>
</section>
<modules>
<load name="ins_chimu_spi.xml" >
<!-- <define name="CHIMU_BIG_ENDIAN" /> -->
</load>
</modules>
<firmware name="fixedwing">
<target name="ap" board="tiny_2.11">
<define name="STRONG_WIND"/>
<define name="WIND_INFO"/>
<define name="WIND_INFO_RET"/>
<define name="LOITER_TRIM"/>
<define name="ALT_KALMAN"/>
<!-- <define name="NB_CHANNELS" value="5" /> -->
</target>
<target name="sim" board="pc"/>
<subsystem name="radio_control" type="ppm"/>
<subsystem name="gps" type="ublox" />
<!-- Communication -->
<subsystem name="telemetry" type="xbee_api">
<configure name="MODEM_BAUD" value="B9600"/>
</subsystem>
<!-- Actuators -->
<subsystem name="control"/>
<!-- Sensors -->
<subsystem name="navigation"/>
<!-- <subsystem name="gps" type="ublox"/> -->
<subsystem name="spi_slave_hs"/>
</firmware>
</airframe>
conf/airframes/CDW/ChimuLisaFw.xml
+5 -8
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@@ -61,9 +61,6 @@
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="GLIDE_AIRSPEED" value="10"/>
<define name="GLIDE_VSPEED" value="3."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
@@ -90,9 +87,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.4"/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="12000."/>
<define name="PITCH_DGAIN" value="1.5"/>
@@ -125,8 +122,8 @@
<section name="SIMU">
<define name="JSBSIM_MODEL" value="&quot;Malolo1&quot;"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
<section name="INS" prefix="INS_">
conf/airframes/CDW/ChimuTinyFw.xml
+3 -6
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@@ -85,9 +85,6 @@
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="GLIDE_AIRSPEED" value="10"/>
<define name="GLIDE_VSPEED" value="3."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
@@ -116,9 +113,9 @@
<define name="COURSE_DGAIN" value="0.3"/>
<define name="COURSE_PRE_BANK_CORRECTION" value="0.2"/>
<define name="ROLL_MAX_SETPOINT" value="0.75" 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_MAX_SETPOINT" value="0.75" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="12000."/>
<define name="PITCH_DGAIN" value="0"/>
conf/airframes/CDW/ChimuTinyFwSpi.xml
+3 -6
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@@ -85,9 +85,6 @@
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="GLIDE_AIRSPEED" value="10"/>
<define name="GLIDE_VSPEED" value="3."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
@@ -116,9 +113,9 @@
<define name="COURSE_DGAIN" value="0.3"/>
<define name="COURSE_PRE_BANK_CORRECTION" value="0.2"/>
<define name="ROLL_MAX_SETPOINT" value="0.9" 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_MAX_SETPOINT" value="0.9" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="12000."/>
<define name="PITCH_DGAIN" value="0"/>
conf/airframes/CDW/debug_i2c.xml
+12 -13
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@@ -61,9 +61,9 @@
<define name="MAG_Y_SENS" value="4.884119848" integer="16"/>
<define name="MAG_Z_SENS" value="2.59926404993" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 0. )"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 0. )"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( 135.)"/>
<define name="BODY_TO_IMU_PHI" value="0. " unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0. " unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="135." unit="deg"/>
</section>
@@ -93,25 +93,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- gaui props
@@ -162,7 +162,6 @@
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="10." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
conf/airframes/ENAC/fixed-wing/firestorm.xml
+3 -3
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@@ -177,9 +177,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.9"/>
<define name="ROLL_MAX_SETPOINT" value="0.805000007153" 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_MAX_SETPOINT" value="0.805000007153" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="14255.3193359"/>
<define name="PITCH_DGAIN" value="1.5"/>
conf/airframes/ENAC/fixed-wing/funjet2.xml
+3 -3
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@@ -171,9 +171,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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."/>
conf/airframes/ENAC/fixed-wing/funjet2_nc.xml
+3 -3
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@@ -191,9 +191,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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."/>
conf/airframes/ENAC/fixed-wing/funjet2_new.xml
+3 -3
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@@ -191,9 +191,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.7"/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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."/>
conf/airframes/ENAC/fixed-wing/funjet3.xml
+5 -5
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@@ -168,9 +168,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.699999988079"/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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="6000."/>
<define name="ROLL_RATE_GAIN" value="1000."/>
@@ -208,8 +208,8 @@
<define name="JSBSIM_MODEL" value="&quot;Malolo1&quot;"/>
<!--define name="JSBSIM_INIT" value="&quot;Malolo1-IC&quot;"/-->
<define name="JSBSIM_LAUNCHSPEED" value="15.0"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
</airframe>
conf/airframes/ENAC/fixed-wing/merlin.xml
+3 -3
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@@ -152,9 +152,9 @@
<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_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="5900"/>
<define name="ROLL_RATE_GAIN" value="2900"/>
conf/airframes/ENAC/fixed-wing/minimag1.xml
+3 -3
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@@ -157,9 +157,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.2"/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" 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_PGAIN" value="12000."/>
conf/airframes/ENAC/fixed-wing/obsolete/drops.xml
+6 -6
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@@ -159,9 +159,9 @@ on<!DOCTYPE airframe SYSTEM "airframe.dtd">
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.0340000391"/>
<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_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_PGAIN" value="6000."/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
@@ -229,11 +229,11 @@ ap.CFLAGS += -DRADIO_CONTROL -DRADIO_CONTROL_AUTO1
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c xbee.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/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)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
#ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c
@@ -264,7 +264,7 @@ ap.srcs += subsystems/navigation/snav.c
# Config for SITL simulation
# include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.ARCHDIR = $(ARCHI)
sim.srcs = latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl.c subsystems/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.srcs = latlong.c radio_control.c subsystems/datalink/downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl.c subsystems/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 += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DUSE_INFRARED -DNAV -DUSE_LED -DWIND_INFO
sim.CFLAGS += -DBOARD_CONFIG=\"tiny.h\" -DAGR_CLIMB -DLOITER_TRIM -DALT_KALMAN
conf/airframes/ENAC/fixed-wing/obsolete/funjet1.xml
+7 -7
View File
@@ -144,9 +144,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.20599997044"/>
<define name="ROLL_MAX_SETPOINT" value="0.805000007153" 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_MAX_SETPOINT" value="0.805000007153" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="14814.8154297"/>
<define name="PITCH_DGAIN" value="1.5"/>
@@ -233,11 +233,11 @@ ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
#ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B9600
#ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c xbee.c
#ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/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)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
@@ -288,7 +288,7 @@ ap.CFLAGS += -DUSE_I2C0 -DI2C0_SCLL=150 -DI2C0_SCLH=150
#include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.ARCHDIR = $(ARCHI)
sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DUSE_INFRARED -DNAV -DUSE_LED -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 subsystems/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.srcs = latlong.c radio_control.c subsystems/datalink/downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl.c fw_v_ctl.c subsystems/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
@@ -307,7 +307,7 @@ sim.srcs += subsystems/navigation/nav_line.c subsystems/navigation/nav_survey_re
setup_actuators.ARCHDIR = $(ARCHI)
setup_actuators.CFLAGS += -DFBW -DBOARD_CONFIG=\"tiny.h\" -DUSE_LED -DTIME_LED=1 -DACTUATORS=\"servos_4015_hw.h\" -DSERVOS_4015 -DUSE_UART1 -DUART1_BAUD=B9600 -DDATALINK=PPRZ -DPPRZ_UART=Uart1
setup_actuators.srcs += sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c pprz_transport.c setup_actuators.c $(SRC_ARCH)/mcu_periph/uart_arch.c $(SRC_ARCH)/servos_4015_hw.c main.c
setup_actuators.srcs += sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c subsystems/datalink/pprz_transport.c setup_actuators.c $(SRC_ARCH)/mcu_periph/uart_arch.c $(SRC_ARCH)/servos_4015_hw.c main.c
</makefile>
</airframe>
conf/airframes/ENAC/fixed-wing/obsolete/malolo_sim.xml
+5 -5
View File
@@ -141,9 +141,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.7" 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_MAX_SETPOINT" value="0.7" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="50000"/>
<define name="PITCH_DGAIN" value="0"/>
@@ -197,8 +197,8 @@
<section name="SIMU">
<!--define name="JSBSIM_MODEL" value="&quot;fulmar&quot;"/-->
<define name="JSBSIM_MODEL" value="&quot;Malolo1&quot;"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
<makefile>
conf/airframes/ENAC/fixed-wing/obsolete/slayer2.xml
+6 -9
View File
@@ -107,9 +107,6 @@
<define name="UNLOCKED_HOME_MODE" value="TRUE"/>
<define name="RC_LOST_MODE" value="PPRZ_MODE_AUTO2"/>
<define name="GLIDE_AIRSPEED" value="12.5"/>
<define name="GLIDE_VSPEED" value="2."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
<define name="TELEMETRY_MODE_AP" value="1"/>
</section>
@@ -146,9 +143,9 @@
<define name="COURSE_PGAIN" value="2.6"/>
<define name="COURSE_DGAIN" value="1"/>
<define name="COURSE_PRE_BANK_CORRECTION" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.73" 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_MAX_SETPOINT" value="0.73" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="9000."/>
<define name="PITCH_DGAIN" value="0."/>
@@ -206,7 +203,7 @@ ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
#ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=XBeeTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DXBEE_UART=Uart0 -DDATALINK=XBEE -DUART0_BAUD=B9600
#ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c xbee.c
#ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/xbee.c
# AEROCOMM
# ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DPPRZ_UART=Uart0 -DDATALINK=PPRZ -DUART0_BAUD=B57600
@@ -214,7 +211,7 @@ ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
# RADIOTRONIX
ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DPPRZ_UART=Uart0 -DDATALINK=PPRZ -DUART0_BAUD=B9600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
@@ -265,7 +262,7 @@ ap.CFLAGS += -D BARO_MS5534A_W1=0xAC20 -D BARO_MS5534A_W2=0x87D9 -D BARO_MS5534A
#include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.ARCHDIR = $(ARCHI)
sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DUSE_INFRARED -DNAV -DUSE_LED -DWIND_INFO
sim.srcs = latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c infrared.c fw_v_ctl.c subsystems/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.srcs = latlong.c radio_control.c subsystems/datalink/downlink.c commands.c gps.c inter_mcu.c infrared.c fw_v_ctl.c subsystems/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 -DUSE_BARO_MS5534A
conf/airframes/ENAC/fixed-wing/obsolete/solarstorm.xml
+5 -5
View File
@@ -146,9 +146,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.885999977589"/>
<define name="ROLL_MAX_SETPOINT" value="0.7" 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_MAX_SETPOINT" value="0.7" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="14255.3193359"/>
<define name="PITCH_DGAIN" value="1.5"/>
@@ -218,7 +218,7 @@ ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DPPRZ_UART=Uart0 -DDATALINK=PPRZ -DUART0_BAUD=B9600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c
@@ -254,7 +254,7 @@ ap.CFLAGS += -DUSE_MODULES
#include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.ARCHDIR = $(ARCHI)
sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DUSE_INFRARED -DNAV -DUSE_LED -DWIND_INFO
sim.srcs = latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl.c subsystems/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.srcs = latlong.c radio_control.c subsystems/datalink/downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl.c subsystems/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
conf/airframes/ENAC/fixed-wing/obsolete/spocII.xml
+8 -8
View File
@@ -148,9 +148,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.20599997044"/>
<define name="ROLL_MAX_SETPOINT" value="0.805000007153" 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_MAX_SETPOINT" value="0.805000007153" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="7627.11914062"/>
<define name="PITCH_DGAIN" value="1.5"/>
@@ -201,8 +201,8 @@
<section name="SIMU">
<define name="JSBSIM_MODEL" value="&quot;Corsica&quot;"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
<makefile>
@@ -225,7 +225,7 @@ ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.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=B57600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c
@@ -254,7 +254,7 @@ ap.CFLAGS += -DUSE_ADC_3 -DADC_CHANNEL_CURRENT=ADC_3
#include $(PAPARAZZI_SRC)/conf/autopilot/sitl.makefile
sim.ARCHDIR = $(ARCHI)
sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DUSE_INFRARED -DNAV -DUSE_LED -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 subsystems/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.srcs = latlong.c radio_control.c subsystems/datalink/downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl.c fw_v_ctl.c subsystems/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
@@ -275,7 +275,7 @@ jsbsim.srcs += $(SIMDIR)/sim_ac_fw.c
setup_actuators.ARCHDIR = $(ARCHI)
setup_actuators.CFLAGS += -DFBW -DBOARD_CONFIG=\"tiny.h\" -DUSE_LED -DTIME_LED=1 -DACTUATORS=\"servos_4015_hw.h\" -DSERVOS_4015 -DUSE_UART1 -DUART1_BAUD=B9600 -DDATALINK=PPRZ -DPPRZ_UART=Uart1
setup_actuators.srcs += sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c pprz_transport.c setup_actuators.c $(SRC_ARCH)/mcu_periph/uart_arch.c $(SRC_ARCH)/servos_4015_hw.c main.c
setup_actuators.srcs += sys_time.c $(SRC_ARCH)/sys_time_hw.c $(SRC_ARCH)/armVIC.c subsystems/datalink/pprz_transport.c setup_actuators.c $(SRC_ARCH)/mcu_periph/uart_arch.c $(SRC_ARCH)/servos_4015_hw.c main.c
</makefile>
</airframe>
conf/airframes/ENAC/fixed-wing/overview.xml
+7 -7
View File
@@ -96,10 +96,10 @@
</section>
<section name="CAM" prefix="CAM_">
<define name="TILT_MAX" value="45" unit="deg"/>
<define name="TILT_NEUTRAL" value="0" unit="deg"/>
<define name="TILT_MIN" value="-45" unit="deg"/>
<define name="TILT0" value="0" unit="deg"/>
<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">
@@ -146,9 +146,9 @@
<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_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."/>
conf/airframes/ENAC/fixed-wing/soarzi.xml
+5 -5
View File
@@ -137,9 +137,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.2"/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" 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_PGAIN" value="12000."/>
@@ -191,10 +191,10 @@ ap.CFLAGS += -DRADIO_CONTROL
ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
#XBEE ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=XBeeTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DXBEE_UART=Uart0 -DDATALINK=XBEE -DUART0_BAUD=B9600
#XBEE ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c xbee.c
#XBEE ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/xbee.c
ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DPPRZ_UART=Uart0 -DDATALINK=PPRZ -DUART0_BAUD=B9600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
conf/airframes/ENAC/fixed-wing/spocIII-1.xml
+5 -5
View File
@@ -149,9 +149,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.20599997044"/>
<define name="ROLL_MAX_SETPOINT" value="0.805000007153" 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_MAX_SETPOINT" value="0.805000007153" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="8200"/>
<define name="PITCH_DGAIN" value="1.5"/>
@@ -181,8 +181,8 @@
<section name="SIMU">
<define name="JSBSIM_MODEL" value="&quot;Corsica&quot;"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
</airframe>
conf/airframes/ENAC/fixed-wing/spocIII-2.xml
+5 -5
View File
@@ -176,9 +176,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.20599997044"/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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="8500."/>
<define name="ROLL_RATE_GAIN" value="2400."/>
@@ -212,8 +212,8 @@
<section name="SIMU">
<define name="JSBSIM_MODEL" value="&quot;Corsica&quot;"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
</airframe>
conf/airframes/ENAC/fixed-wing/spocIII-3.xml
+5 -5
View File
@@ -179,9 +179,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.20599997044"/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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="8500."/>
<define name="ROLL_RATE_GAIN" value="2400."/>
@@ -215,8 +215,8 @@
<section name="SIMU">
<define name="JSBSIM_MODEL" value="&quot;Corsica&quot;"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
</airframe>
conf/airframes/ENAC/fixed-wing/twinjet2.xml
+6 -6
View File
@@ -166,9 +166,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.995000004768"/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" 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="3553.89208984"/>
<define name="ROLL_RATE_GAIN" value="0."/>
@@ -242,11 +242,11 @@ ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
########## Modems
ap.CFLAGS += -DDOWNLINK -DUSE_UART1 -DDOWNLINK_TRANSPORT=XBeeTransport -DXBEE_UART=Uart1 -DDATALINK=XBEE -DUART1_BAUD=B57600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c xbee.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/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)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
#ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
########## ADC
ap.CFLAGS += -DADC -DUSE_ADC_0 -DUSE_ADC_1 -DUSE_ADC_2 -DUSE_ADC_3
@@ -299,7 +299,7 @@ ap.CFLAGS += -DUSE_MODULES
sim.ARCHDIR = $(ARCHI)
sim.CFLAGS += -DSITL -DAP -DFBW -DRADIO_CONTROL -DINTER_MCU -DDOWNLINK -DDOWNLINK_TRANSPORT=IvyTransport -DUSE_INFRARED -DNAV -DUSE_LED -DWIND_INFO
sim.srcs = latlong.c radio_control.c downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl_n.c subsystems/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.srcs = latlong.c radio_control.c subsystems/datalink/downlink.c commands.c gps.c inter_mcu.c infrared.c fw_h_ctl_a.c fw_v_ctl_n.c subsystems/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 -DPITCH_TRIM -DALT_KALMAN
conf/airframes/ENAC/fixed-wing/weasel.xml
+5 -5
View File
@@ -192,9 +192,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="0.7"/>
<define name="ROLL_MAX_SETPOINT" value="0.8" 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_MAX_SETPOINT" value="0.8" 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="3800."/>
<define name="ROLL_RATE_GAIN" value="500."/>
@@ -232,8 +232,8 @@
<define name="JSBSIM_MODEL" value="&quot;Malolo1&quot;"/>
<!--define name="JSBSIM_INIT" value="&quot;Malolo1-IC&quot;"/-->
<define name="JSBSIM_LAUNCHSPEED" value="15.0"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="RadOfDeg(0.)"/>
<define name="JSBSIM_IR_ROLL_NEUTRAL" value="0." unit="deg"/>
<define name="JSBSIM_IR_PITCH_NEUTRAL" value="0." unit="deg"/>
</section>
</airframe>
conf/airframes/ENAC/quadrotor/blender.xml
+17 -18
View File
@@ -12,13 +12,12 @@
<firmware name="rotorcraft">
<define name="USE_INS_NAV_INIT"/>
<define name="USE_ADAPT_HOVER"/>
<define name="NO_FUCKING_STARTUP_DELAY"/>
<!--define name="GUIDANCE_H_USE_REF"/-->
<target name="ap" board="booz_1.0">
<define name="FAILSAFE_GROUND_DETECT"/>
<define name="USE_GPS_ACC4R"/>
<define name="BOOZ_START_DELAY" value="3"/>
<define name="ACTUATORS_START_DELAY" value="3"/>
</target>
<target name="sim" board="pc">
<subsystem name="fdm" type="nps"/>
@@ -130,10 +129,10 @@
<define name="MAG_Y_SENS" value="5.43740121157" integer="16"/>
<define name="MAG_Z_SENS" value="2.60492836649" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<!--define name="BODY_TO_IMU_PSI" value="RadOfDeg(45.)"/-->
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<!--define name="BODY_TO_IMU_PSI" value="45." unit="deg"/-->
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -152,25 +151,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -246,8 +245,8 @@
<define name="TILT_NEUTRAL" value="1500"/>
<define name="TILT_MIN" value="1060"/>
<define name="TILT_MAX" value="2250"/>
<define name="TILT_ANGLE_MIN" value="RadOfDeg(-90.)" unit="rad"/>
<define name="TILT_ANGLE_MAX" value="RadOfDeg( 0.)" unit="rad"/>
<define name="TILT_ANGLE_MIN" value="-90." unit="deg"/>
<define name="TILT_ANGLE_MAX" value=" 0." unit="deg"/>
<define name="PAN_NEUTRAL" value="0"/>
<define name="PAN_MIN" value="0"/>
<define name="PAN_MAX" value="25736"/> <!-- 360 deg (2^12) -->
@@ -261,7 +260,7 @@
<define name="FACE_REINJ_1" value="1024"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="10."/>
<define name="BoozDropPwm(_v)" value="BoozSetPwm0Value(_v)"/>
<define name="IMU_MAG_OFFSET" value="-9."/>
<define name="IMU_MAG_OFFSET" value="RadOfDeg(-9.)"/>
</section>
<section name="GCS">
conf/airframes/ENAC/quadrotor/booz2_g1.xml
+16 -18
View File
@@ -16,13 +16,12 @@
<firmware name="rotorcraft">
<define name="USE_INS_NAV_INIT"/>
<define name="USE_ADAPT_HOVER"/>
<define name="NO_FUCKING_STARTUP_DELAY"/>
<!--define name="GUIDANCE_H_USE_REF"/-->
<target name="ap" board="booz_1.0">
<define name="FAILSAFE_GROUND_DETECT"/>
<define name="USE_GPS_ACC4R"/>
<define name="BOOZ_START_DELAY" value="3"/>
<define name="ACTUATORS_START_DELAY" value="3"/>
</target>
<target name="sim" board="pc">
<subsystem name="fdm" type="nps"/>
@@ -94,9 +93,9 @@
<define name="MAG_Y_SENS" value="21.79885" integer="16"/>
<define name="MAG_Z_SENS" value="14.675745" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(1.3)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(-2.6)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="1.3" unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="-2.6" unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -115,25 +114,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -158,7 +157,6 @@
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="15." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
<define name="SONAR_SENS" value="2.146" integer="16"/>
</section>
@@ -212,8 +210,8 @@
<define name="TILT_NEUTRAL" value="1500"/>
<define name="TILT_MAX" value="1000"/>
<define name="TILT_MIN" value="2300"/>
<define name="TILT_ANGLE_MIN" value="RadOfDeg(-90.)" unit="rad"/>
<define name="TILT_ANGLE_MAX" value="RadOfDeg( 10.)" unit="rad"/>
<define name="TILT_ANGLE_MIN" value="-90." unit="deg"/>
<define name="TILT_ANGLE_MAX" value=" 10." unit="deg"/>
<define name="PAN_NEUTRAL" value="0"/>
<define name="PAN_MIN" value="0"/>
<define name="PAN_MAX" value="25736"/> <!-- 360 deg (2^12) -->
@@ -230,7 +228,7 @@
<define name="BOOZ_ANALOG_BARO_THRESHOLD" value="800"/>
<define name="FACE_REINJ_1" value="1024"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="10."/>
<!--define name="IMU_MAG_OFFSET" value="-5.8"/-->
<!--define name="IMU_MAG_OFFSET" value="RadOfDeg(-5.8)"/-->
</section>
<section name="GCS">
conf/airframes/ENAC/quadrotor/g1_vision.xml
+14 -15
View File
@@ -67,9 +67,9 @@
<define name="MAG_Y_SENS" value="21.79885" integer="16"/>
<define name="MAG_Z_SENS" value="14.675745" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(1.3)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(-2.6)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="1.3" unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="-2.6" unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -88,25 +88,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="BOOZ_STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -131,7 +131,6 @@
<section name="INS" prefix="BOOZ_INS_">
<define name="BARO_SENS" value="15." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
<define name="SONAR_SENS" value="2.146" integer="16"/>
</section>
@@ -231,8 +230,8 @@ include $(CFG_BOOZ)/subsystems/booz2_ahrs_cmpl.makefile
#include $(CFG_BOOZ)/subsystems/booz2_ins_hff.makefile
#ap.CFLAGS += -DR_POS=0.1
ap.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
sim.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DBOOZ_START_DELAY=3
ap.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DACTUATORS_START_DELAY=3
sim.CFLAGS += -DUSE_ADAPT_HOVER -DUSE_INS_NAV_INIT -DACTUATORS_START_DELAY=3
ap.CFLAGS += -DUSE_MODULES
conf/airframes/ENAC/quadrotor/mkk1-vision.xml
+12 -13
View File
@@ -87,9 +87,9 @@
<define name="MAG_Y_SENS" value="-21.79885" integer="16"/>
<define name="MAG_Z_SENS" value="-14.675745" integer="16"/-->
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -121,25 +121,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="BOOZ_STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -164,7 +164,6 @@
<section name="INS" prefix="BOOZ_INS_">
<define name="BARO_SENS" value="15." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
<!--define name="SONAR_SENS" value="2.146" integer="16"/-->
<define name="SONAR_SENS" value="3." integer="16"/>
</section>
conf/airframes/ENAC/quadrotor/mkk1.xml
+12 -13
View File
@@ -117,9 +117,9 @@
<define name="MAG_Y_SENS" value="-21.79885" integer="16"/>
<define name="MAG_Z_SENS" value="-14.675745" integer="16"/-->
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -151,25 +151,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -194,7 +194,6 @@
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="15." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
conf/airframes/ENAC/quadrotor/navgo.xml
+18 -19
View File
@@ -11,7 +11,6 @@
<firmware name="rotorcraft">
<define name="USE_INS_NAV_INIT"/>
<define name="USE_ADAPT_HOVER"/>
<define name="NO_FUCKING_STARTUP_DELAY"/>
<define name="USE_ATTITUDE_REF" value="0"/>
<!--define name="GUIDANCE_H_USE_REF"/-->
@@ -99,9 +98,9 @@
<define name="MAG_Y_SENS" value="4.8961742578" integer="16"/>
<define name="MAG_Z_SENS" value="5.31527656902" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/> <!-- -10 -->
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/> <!-- -10 -->
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/> <!-- -10 -->
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/> <!-- -10 -->
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -133,9 +132,9 @@
<define name="MAG_Y_SENS" value="4.49687342915" integer="16"/>
<define name="MAG_Z_SENS" value="4.93138019221" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(-10.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(-10.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="-10." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="-10." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -168,25 +167,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -257,8 +256,8 @@
<define name="TILT_NEUTRAL" value="1500"/>
<define name="TILT_MIN" value="1060"/>
<define name="TILT_MAX" value="2250"/>
<define name="TILT_ANGLE_MIN" value="RadOfDeg(-90.)" unit="rad"/>
<define name="TILT_ANGLE_MAX" value="RadOfDeg( 0.)" unit="rad"/>
<define name="TILT_ANGLE_MIN" value="-90." unit="deg"/>
<define name="TILT_ANGLE_MAX" value=" 0." unit="deg"/>
<define name="PAN_NEUTRAL" value="0"/>
<define name="PAN_MIN" value="0"/>
<define name="PAN_MAX" value="25736"/> <!-- 360 deg (2^12) -->
@@ -272,7 +271,7 @@
<define name="FACE_REINJ_1" value="1024"/>
<define name="DEFAULT_CIRCLE_RADIUS" value="10."/>
<define name="BoozDropPwm(_v)" value="BoozSetPwm1Value(_v)"/>
<define name="IMU_MAG_OFFSET" value="-9."/>
<define name="IMU_MAG_OFFSET" value="RadOfDeg(-9.)"/>
</section>
<section name="GCS">
conf/airframes/ENAC/quadrotor/nova1.xml
+12 -13
View File
@@ -88,9 +88,9 @@
<define name="MAG_Y_SENS" value="6.95371185551" integer="16"/>
<define name="MAG_Z_SENS" value="3.12322557454" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(-135.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="-135." unit="deg"/>
</section>
@@ -122,25 +122,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="RadOfDeg(90.)"/>
<define name="REF_MAX_R" value="90." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(900.)"/>
<!-- feedback -->
@@ -165,7 +165,6 @@
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="15." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
conf/airframes/LAAS/mmlaas_N1.xml
+3 -3
View File
@@ -167,9 +167,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" 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="10000"/>
conf/airframes/LAAS/mmlaas_N2.xml
+3 -3
View File
@@ -163,9 +163,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" 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="10000"/>
conf/airframes/LAAS/mmlaas_N3.xml
+3 -3
View File
@@ -163,9 +163,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1."/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" 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="10000"/>
conf/airframes/NoVa_L.xml
+12 -13
View File
@@ -81,9 +81,9 @@
<define name="MAG_Y_CHAN" value="0"/>
<define name="MAG_Z_CHAN" value="2"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 4.5)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 6.8)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( -45.)"/>
<define name="BODY_TO_IMU_PHI" value="4.5" unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="6.8" unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="-45." unit="deg"/>
<define name="GYRO_P_CHAN" value="0"/>
<define name="GYRO_Q_CHAN" value="4"/>
@@ -121,25 +121,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(180.)"/><!-- Maximum speed in deg/s-->
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="180." unit="deg/s"/><!-- Maximum speed in deg/s-->
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- gaui props
@@ -190,7 +190,6 @@
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="10." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
conf/airframes/PPZUAV/fixed-wing/ppzimu_tiny.xml
+3 -6
View File
@@ -122,9 +122,6 @@
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="GLIDE_AIRSPEED" value="10"/>
<define name="GLIDE_VSPEED" value="3."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
@@ -153,9 +150,9 @@
<define name="COURSE_DGAIN" value="0.3"/>
<define name="COURSE_PRE_BANK_CORRECTION" value="0.2"/>
<define name="ROLL_MAX_SETPOINT" value="0.75" 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_MAX_SETPOINT" value="0.75" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="12000."/>
<define name="PITCH_DGAIN" value="1.5"/>
conf/airframes/PPZUAV/quadrotor/ppzuav_booz2_asctec_example.xml
+9 -9
View File
@@ -85,25 +85,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback gains for better endurance -->
conf/airframes/PPZUAV/quadrotor/ppzuav_booz2_mkk_example.xml
+9 -9
View File
@@ -86,25 +86,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback gains for better endurance -->
conf/airframes/Poine/antenna.xml
+1 -1
View File
@@ -29,7 +29,7 @@ ant.CFLAGS += -DUSE_UART0 -DUART0_BAUD=B38400
ant.srcs += $(SRC_ARCH)/mcu_periph/uart_arch.c
ant.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_DEVICE=Uart0
ant.srcs += downlink.c pprz_transport.c
ant.srcs += subsystems/datalink/downlink.c subsystems/datalink/pprz_transport.c
ant.CFLAGS += -DDOWNLINK_AP_DEVICE=Uart0 -DAP
ant.CFLAGS += -DDATALINK=PPRZ -DPPRZ_UART=Uart0
conf/airframes/Poine/beth.xml
+12 -12
View File
@@ -67,9 +67,9 @@
<define name="MAG_Z_SENS" value="-3.11986612709" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( 45.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="45." unit="deg"/>
<!-- 3 -->
<define name="GYRO_P_CHAN" value="0"/>
@@ -116,7 +116,7 @@ main_stm32.srcs += sys_time.c $(SRC_ARCH)/sys_time_hw.c
main_stm32.CFLAGS += -DUSE_UART2 -DUART2_BAUD=B57600
main_stm32.srcs += $(SRC_ARCH)/mcu_periph/uart_arch.c
main_stm32.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_DEVICE=Uart2
main_stm32.srcs += downlink.c pprz_transport.c
main_stm32.srcs += subsystems/datalink/downlink.c subsystems/datalink/pprz_transport.c
main_stm32.CFLAGS += -DUSE_OVERO_LINK
@@ -136,7 +136,7 @@ main_stm32.srcs += lisa/lisa_overo_link.c lisa/arch/stm32/lisa_overo_link_arch.c
#crista IMU
main_stm32.srcs += math/pprz_trig_int.c
main_stm32.CFLAGS += -DIMU_TYPE_H=\"imu/imu_crista.h\" -DIMU_OVERRIDE_CHANNELS
main_stm32.CFLAGS += -DIMU_TYPE_H=\"imu/imu_crista.h\"
main_stm32.srcs += subsystems/imu.c \
subsystems/imu/imu_crista.c \
arch/$(ARCH)/subsystems/imu/imu_crista_arch.c
@@ -147,7 +147,7 @@ main_stm32.srcs += firmwares/rotorcraft/actuators/actuators_asctec.c
#\
# $(SRC_BOOZ_ARCH)/actuators/actuators_asctec_arch.c
main_stm32.CFLAGS += -DACTUATORS_ASCTEC_DEVICE=i2c1
# -DBOOZ_START_DELAY=3 -DUSE_TIM2_IRQ
# -DACTUATORS_START_DELAY=3 -DUSE_TIM2_IRQ
main_stm32.CFLAGS += -DUSE_I2C1
main_stm32.srcs += i2c.c $(SRC_ARCH)/i2c_hw.c
@@ -188,7 +188,7 @@ main_coders.srcs += sys_time.c $(SRC_ARCH)/sys_time_hw.c
main_coders.CFLAGS += -DUSE_UART1 -DUART1_BAUD=B57600
main_coders.srcs += $(SRC_ARCH)/mcu_periph/uart_arch.c
main_coders.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_DEVICE=Uart1
main_coders.srcs += downlink.c pprz_transport.c
main_coders.srcs += subsystems/datalink/downlink.c subsystems/datalink/pprz_transport.c
#main_coders.CFLAGS += -DUSE_I2C2
#main_coders.srcs += $(SRC_ARCH)/i2c_hw.c
@@ -229,7 +229,7 @@ main_overo.srcs += $(SRC_FMS)/fms_spi_link.c
main_overo.CFLAGS += -DOVERO_LINK_MSG_UP=AutopilotMessageBethUp -DOVERO_LINK_MSG_DOWN=AutopilotMessageBethDown
main_overo.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=UdpTransport
main_overo.srcs += $(SRC_FMS)/udp_transport2.c downlink.c
main_overo.srcs += $(SRC_FMS)/udp_transport2.c subsystems/datalink/downlink.c
main_overo.srcs += $(SRC_FMS)/fms_network.c
main_overo.LDFLAGS += -levent -lm
@@ -252,7 +252,7 @@ overo_test_uart.srcs += $(SRC_FMS)/fms_periodic.c
overo_test_uart.srcs += $(SRC_FMS)/fms_serial_port.c
overo_test_uart.LDFLAGS += -lrt
overo_test_uart.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=UdpTransport
overo_test_uart.srcs += $(SRC_FMS)/udp_transport2.c downlink.c
overo_test_uart.srcs += $(SRC_FMS)/udp_transport2.c subsystems/datalink/downlink.c
overo_test_uart.srcs += $(SRC_FMS)/fms_network.c
overo_test_uart.LDFLAGS += -levent -lm
overo_test_uart.srcs += $(SRC_BETH)/overo_gcs_com.c
@@ -261,7 +261,7 @@ overo_test_uart.srcs += $(SRC_BETH)/overo_gcs_com.c
overo_test_uart.CFLAGS += -DUBX -DUSE_GPS -DUSE_UART0 -DUART0_BAUD=B38400 -DGPS_LINK=Uart0 -DGPS_USE_LATLONG
overo_test_uart.srcs += gps_ubx.c gps.c latlong.c $(SRC_BETH)/uart_hw.c
overo_test_uart.CFLAGS +=-DUSE_UART1 -DUART1_BAUD=B57600 -DDOWNLINK_DEVICE=Uart1 -DPPRZ_UART=Uart1 -DDATALINK=PPRZ
overo_test_uart.srcs += pprz_transport.c $(SRC_BETH)/rcv_telemetry.c
overo_test_uart.srcs += subsystems/datalink/pprz_transport.c $(SRC_BETH)/rcv_telemetry.c
#
# Overo twisting
@@ -278,7 +278,7 @@ overo_twist.srcs += $(SRC_FMS)/fms_spi_link.c
overo_twist.CFLAGS += -DOVERO_LINK_MSG_UP=AutopilotMessageBethUp -DOVERO_LINK_MSG_DOWN=AutopilotMessageBethDown
overo_twist.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=UdpTransport
overo_twist.srcs += $(SRC_FMS)/udp_transport2.c downlink.c
overo_twist.srcs += $(SRC_FMS)/udp_transport2.c subsystems/datalink/downlink.c
overo_twist.srcs += $(SRC_FMS)/fms_network.c
overo_twist.LDFLAGS += -levent -lm
@@ -304,7 +304,7 @@ overo_sfb.srcs += $(SRC_FMS)/fms_spi_link.c
overo_sfb.CFLAGS += -DOVERO_LINK_MSG_UP=AutopilotMessageBethUp -DOVERO_LINK_MSG_DOWN=AutopilotMessageBethDown
overo_sfb.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=UdpTransport
overo_sfb.srcs += $(SRC_FMS)/udp_transport2.c downlink.c
overo_sfb.srcs += $(SRC_FMS)/udp_transport2.c subsystems/datalink/downlink.c
overo_sfb.srcs += $(SRC_FMS)/fms_network.c
overo_sfb.LDFLAGS += -levent
overo_sfb.LDFLAGS += -lm
conf/airframes/Poine/bl_mc.xml
+1 -1
View File
@@ -33,7 +33,7 @@ main.CFLAGS += -DUSE_UART1 -DUART1_BAUD=B38400
main.srcs += $(SRC_ARCH)/mcu_periph/uart_arch.c
main.CFLAGS += -DDOWNLINK -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_DEVICE=Uart1
main.srcs += downlink.c pprz_transport.c
main.srcs += subsystems/datalink/downlink.c subsystems/datalink/pprz_transport.c
main.srcs += $(SRC_ARCH)/bl_mc_power.c
conf/airframes/Poine/booz2_a1.xml
+15 -15
View File
@@ -73,13 +73,13 @@
<define name="MAG_X_SENS" value=" 3.4936416" integer="16"/>
<define name="MAG_Y_SENS" value=" 3.607713" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(4.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(3.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="4." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="3." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
<!--
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
-->
</section>
@@ -100,25 +100,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
conf/airframes/Poine/booz2_a1p.xml
+12 -12
View File
@@ -76,9 +76,9 @@
<!-- <define name="MAG_X_SENS" value="-3.4936416" integer="16"/> -->
<!-- <define name="MAG_Y_SENS" value=" 3.607713" integer="16"/> -->
<define name="BODY_TO_IMU_PHI" value="RadOfDeg(4.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg(3.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg(0.)"/>
<define name="BODY_TO_IMU_PHI" value="4." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="3." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
@@ -98,25 +98,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
conf/airframes/Poine/booz2_a7.xml
+12 -13
View File
@@ -61,9 +61,9 @@
<define name="MAG_Y_SENS" value="4.884119848" integer="16"/>
<define name="MAG_Z_SENS" value="2.59926404993" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 0. )"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 0. )"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( 135.)"/>
<define name="BODY_TO_IMU_PHI" value="0. " unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0. " unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="135." unit="deg"/>
</section>
@@ -93,25 +93,25 @@
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="RadOfDeg(45.)"/>
<define name="SP_MAX_THETA" value="RadOfDeg(45.)"/>
<define name="SP_MAX_R" value="RadOfDeg(90.)"/>
<define name="SP_MAX_PHI" value="45." unit="deg"/>
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="RadOfDeg(300.)"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="RadOfDeg(800)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="RadOfDeg(300.)"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="RadOfDeg(500)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="RadOfDeg(180.)"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- gaui props
@@ -162,7 +162,6 @@
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="10." integer="16"/>
<define name="UNTILT_ACCEL" value="1"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
conf/airframes/Poine/booz2_a8.xml
+9 -9
View File
@@ -74,9 +74,9 @@
<define name="MAG_Z_SENS" value="-3.11986612709" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( 45.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="45." unit="deg"/>
<define name="GYRO_P_CHAN" value="0"/>
<define name="GYRO_Q_CHAN" value="4"/>
@@ -118,9 +118,9 @@
<define name="MAG_Y_NEUTRAL" value=" 49"/>
<define name="MAG_Z_NEUTRAL" value="-66"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( 45.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="45." unit="deg"/>
</section>
-->
@@ -167,9 +167,9 @@
<define name="MAG_Z_SENS" value="-3.11986612709" integer="16"/>
<define name="BODY_TO_IMU_PHI" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_THETA" value="RadOfDeg( 0.)"/>
<define name="BODY_TO_IMU_PSI" value="RadOfDeg( 45.)"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="45." unit="deg"/>
<define name="GYRO_P_CHAN" value="0"/>
<define name="GYRO_Q_CHAN" value="4"/>
conf/airframes/Poine/easy_glider1.xml
+4 -7
View File
@@ -88,9 +88,6 @@
<define name="DEFAULT_CIRCLE_RADIUS" value="80."/>
<define name="GLIDE_AIRSPEED" value="10"/>
<define name="GLIDE_VSPEED" value="3."/>
<define name="GLIDE_PITCH" value="45" unit="deg"/>
</section>
<section name="VERTICAL CONTROL" prefix="V_CTL_">
@@ -118,9 +115,9 @@
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.10800004005"/>
<define name="ROLL_MAX_SETPOINT" value="0.6" 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_MAX_SETPOINT" value="0.6" unit="rad"/>
<define name="PITCH_MAX_SETPOINT" value="0.5" unit="rad"/>
<define name="PITCH_MIN_SETPOINT" value="-0.5" unit="rad"/>
<define name="PITCH_PGAIN" value="15184.5644531"/>
<define name="PITCH_DGAIN" value="1.5"/>
@@ -176,7 +173,7 @@ ap.srcs += radio_control.c $(SRC_ARCH)/ppm_hw.c
# transparent
ap.CFLAGS += -DDOWNLINK -DUSE_UART0 -DDOWNLINK_TRANSPORT=PprzTransport -DDOWNLINK_FBW_DEVICE=Uart0 -DDOWNLINK_AP_DEVICE=Uart0 -DPPRZ_UART=Uart0 -DDATALINK=PPRZ -DUART0_BAUD=B9600
ap.srcs += downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c pprz_transport.c
ap.srcs += subsystems/datalink/downlink.c $(SRC_ARCH)/mcu_periph/uart_arch.c datalink.c subsystems/datalink/pprz_transport.c
ap.CFLAGS += -DINTER_MCU
ap.srcs += inter_mcu.c

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