[conf] drop discovery boards

if test board from ST should be used, better use the more recent
nucleo144
This commit is contained in:
Gautier Hattenberger
2021-02-02 18:37:24 +01:00
parent 095bb75e49
commit 2e7ba37cf6
12 changed files with 0 additions and 3545 deletions
-11
View File
@@ -32,17 +32,6 @@
settings_modules="modules/ahrs_int_cmpl_quat.xml modules/imu_common.xml"
gui_color="blue"
/>
<aircraft
name="discovery"
ac_id="9"
airframe="airframes/FLIXR/flixr_discovery.xml"
radio="radios/mc20.xml"
telemetry="telemetry/default_fixedwing_imu.xml"
flight_plan="flight_plans/basic.xml"
settings="settings/fixedwing_basic.xml"
settings_modules="modules/switch_servo.xml modules/gps.xml modules/imu_common.xml modules/ahrs_int_cmpl_quat.xml modules/nav_basic_fw.xml modules/guidance_full_pid_fw.xml modules/stabilization_adaptive_fw.xml"
gui_color="blue"
/>
<aircraft
name="flixr_lisamx"
ac_id="42"
-369
View File
@@ -1,369 +0,0 @@
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<!-- ST Model Discovery (http://www.sheng-teng.com/)
TWOG1 (http://wiki.paparazziuav.org/wiki/TWOG/v1.0)
* uBlox LEA5H and Sarantel helix GPS antenna
-->
<airframe name="Discovery">
<firmware name="fixedwing">
<target name="ap" board="twog_1.0">
<configure name="PERIODIC_FREQUENCY" value="960"/> <!-- IMU FREQ -->
<configure name="AHRS_PROPAGATE_FREQUENCY" value="120"/>
<configure name="AHRS_CORRECT_FREQUENCY" value="60"/>
<configure name="AHRS_ALIGNER_LED" value="2"/>
<configure name="SYS_TIME_LED" value="1"/>
<configure name="GPS_LED" value="none"/>
<!-- for airspeed sensor
<define name="USE_I2C0"/>
-->
</target>
<target name="sim" board="pc"/>
<define name="LOITER_TRIM"/>
<define name="USE_PITCH_TRIM"/> <!-- basically same as loiter trim, but for adaptive-->
<define name="USE_GYRO_PITCH_RATE"/>
<define name="WIND_INFO"/>
<!-- Communication -->
<module name="telemetry" type="transparent"/>
<module name="radio_control" type="ppm"/>
<!--module name="settings" type="rc"/-->
<!-- Control -->
<module name="control" type="new"/>
<module name="navigation"/>
<module name="ahrs" type="int_cmpl_quat">
<configure name="USE_MAGNETOMETER" value="0"/>
<define name="AHRS_USE_GPS_HEADING" value="1"/>
</module>
<module name="ins" type="alt_float"/>
<!-- Sensors -->
<module name="imu" type="b2_v1.0">
<configure name="NO_MAG" value="1"/>
</module>
<module name="gps" type="ublox"/>
<module name="current_sensor">
<configure name="ADC_CURRENT_SENSOR" value="ADC_3"/>
</module>
<module name="switch" type="servo"/>
<module name="sys_mon"/>
<module name="adc_generic">
<configure name="ADC_CHANNEL_GENERIC1" value="ADC_4"/> <!-- voltage sensor -->
</module>
</firmware>
<firmware name="setup">
<target name="tunnel" board="twog_1.0" />
<target name="usb_tunnel" board="twog_1.0">
<configure name="TUNNEL_PORT" value="UART1"/>
</target>
</firmware>
<firmware name="test_progs">
<configure name="SYS_TIME_LED" value="1"/>
<target name="test_gpio" board="twog_1.0"/>
<target name="test_sys_time_timer" board="twog_1.0"/>
<target name="test_telemetry" board="twog_1.0"/>
</firmware>
<!-- Define here to which CONNECTOR NUMBER the servo is connected to, on the autopilot cicuit board -->
<servos>
<servo name="MOTOR" no="0" min="1100" neutral="1100" max="1900"/>
<servo name="ELEVATOR" no="2" min="1100" neutral="1500" max="1900"/>
<servo name="AILERON_RIGHT" no="3" min="1000" neutral="1500" max="1000"/>
<servo name="AILERON_LEFT" no="4" min="1000" neutral="1500" max="2000"/>
<servo name="RUDDER" no="6" min="1000" neutral="1500" max="2000"/>
<servo name="HATCH" no="7" min="1100" neutral="1100" max="1900"/>
</servos>
<section name="SWITCH_SERVO" PREFIX="SWITCH_SERVO_">
<define name="SERVO" value="HATCH"/>
<define name="ON_VALUE" value="SERVO_HATCH_MIN"/>
<define name="OFF_VALUE" value="SERVO_HATCH_MAX"/>
</section>
<!-- commands section -->
<commands>
<axis name="THROTTLE" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="YAW" failsafe_value="2000"/>
<axis name="HATCH" failsafe_value="-9599"/>
<!-- maybe set to open position so we can insert the payload -->
</commands>
<rc_commands>
<set command="THROTTLE" value="@THROTTLE"/>
<set command="ROLL" value="@ROLL"/>
<set command="PITCH" value="@PITCH"/>
<set command="YAW" value="@YAW"/>
</rc_commands>
<auto_rc_commands>
<!-- To still be able to use rudder, which is needed with sidewind landing in auto1 stabilization mode only YAW -->
<set command="YAW" value="@YAW"/>
</auto_rc_commands>
<!--For mixed controlflaps -->
<section name="MIXER">
<define name="AILERON_DIFF" value="0.7"/>
<define name="COMBI_SWITCH" value="0.3"/>
</section>
<command_laws>
<set servo="MOTOR" value="@THROTTLE"/>
<set servo="ELEVATOR" value="@PITCH"/>
<set servo="RUDDER" value="@YAW + @ROLL*COMBI_SWITCH"/>
<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="HATCH" value="@HATCH"/-->
</command_laws>
<section name="IMU" prefix="IMU_">
<define name="GYRO_P_CHAN" value="1"/>
<define name="GYRO_Q_CHAN" value="2"/>
<define name="GYRO_R_CHAN" value="0"/>
<define name="GYRO_P_SIGN" value="1"/>
<define name="GYRO_Q_SIGN" value="1"/>
<define name="GYRO_R_SIGN" value="-1"/>
<define name="GYRO_P_NEUTRAL" value="32362"/>
<define name="GYRO_R_NEUTRAL" value="32080"/>
<define name="GYRO_Q_NEUTRAL" value="32096"/>
<define name="GYRO_P_SENS" value="1.1032765" integer="16"/>
<define name="GYRO_R_SENS" value="1.1360802599" integer="16"/>
<define name="GYRO_Q_SENS" value="1.1249874614" integer="16"/>
<define name="ACCEL_X_CHAN" value="3"/>
<define name="ACCEL_Y_CHAN" value="6"/>
<define name="ACCEL_Z_CHAN" value="5"/>
<define name="ACCEL_X_SIGN" value="-1"/>
<define name="ACCEL_Y_SIGN" value="1"/>
<define name="ACCEL_Z_SIGN" value="-1"/>
<define name="ACCEL_X_SENS" value="2.45932966" integer="16"/>
<define name="ACCEL_Z_SENS" value="2.45106376" integer="16"/>
<define name="ACCEL_Y_SENS" value="2.47825717" integer="16"/>
<define name="ACCEL_X_NEUTRAL" value="31886"/>
<define name="ACCEL_Z_NEUTRAL" value="32162"/>
<define name="ACCEL_Y_NEUTRAL" value="32941"/>
<define name="GYRO_P_Q" value="0."/>
<define name="GYRO_P_R" value="0."/>
<define name="GYRO_Q_P" value="0."/>
<define name="GYRO_Q_R" value="0."/>
<define name="GYRO_R_P" value="0."/>
<define name="GYRO_R_Q" value="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>
<!-- Munich -->
<section name="AHRS" prefix="AHRS_">
<define name="H_X" value="0.4357869"/>
<define name="H_Y" value="0.0177010"/>
<define name="H_Z" value="0.8998758"/>
</section>
<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="55" unit="deg"/>
<define name="MAX_PITCH" value="35" unit="deg"/>
</section>
<section name="BAT">
<define name="MilliAmpereOfAdc(adc)" value="(adc*88)"/>
<!-- <define name="ADC_CHANNEL_VOLTAGE" value="ADC_4" /> -->
<!-- The real multiplier is unknown we take 2 as test example -->
<!-- <define name="VoltageOfAdc(adc)" value ="(adc*2)"/> -->
<!-- If NO current-volts sensor installed uncomment below -->
<!--define name="MILLIAMP_AT_FULL_THROTTLE" value="17000" unit="mA"/-->
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/> <!-- 3S lipo 3.1*3=9.3 -->
<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/>
<define name="LOW_BAT_LEVEL" value="9.7" unit="V"/>
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/> <!-- 3S lipo 4.2*3=12.6 -->
</section>
<section name="MISC">
<define name="MINIMUM_AIRSPEED" value="9.0" unit="m/s"/>
<define name="NOMINAL_AIRSPEED" value="14.0" unit="m/s"/>
<define name="MAXIMUM_AIRSPEED" value="22.0" unit="m/s"/>
<define name="CARROT" value="5.0" unit="s"/>
<define name="KILL_MODE_DISTANCE" value="(1.5*MAX_DIST_FROM_HOME)"/>
<define name="CONTROL_FREQUENCY" value="60" unit="Hz"/>
<!--UNLOCKED_HOME_MODE if set to TRUE means that HOME mode does not get stuck.
If not set before when you would enter home mode you had to flip a bit via the GCS to get out. -->
<!--define name="UNLOCKED_HOME_MODE" value="TRUE"/-->
<!-- RC_LOST_MODE means that if your RC Transmitter signal is not received anymore in the autopilot, e.g. you switch it off
or fly a long range mission you define the wanted mode behaviour here.
If you do not define it, it defaults to flying to the flightplan HOME -->
<!--define name="RC_LOST_MODE" value="PPRZ_MODE_AUTO2"/-->
<define name="DEFAULT_CIRCLE_RADIUS" value="50.0"/>
<!-- The Glide definitions are used for calculating the touch down point during auto landing -->
<!--
-->
</section>
<!-- ******************* VERTICAL CONTROL ********************************** -->
<section name="VERTICAL CONTROL" prefix="V_CTL_">
<define name="POWER_CTL_BAT_NOMINAL" value="11.2" unit="volt"/>
<!-- outer loop proportional gain -->
<define name="ALTITUDE_PGAIN" value="0.04" unit="(m/s)/m"/>
<!-- outer loop saturation -->
<define name="ALTITUDE_MAX_CLIMB" value="2." unit="m/s"/>
<!-- Cruise throttle + limits -->
<define name="AUTO_THROTTLE_NOMINAL_CRUISE_THROTTLE" value="0.65" unit="%"/>
<define name="AUTO_THROTTLE_MIN_CRUISE_THROTTLE" value="0.40" unit="%"/>
<define name="AUTO_THROTTLE_MAX_CRUISE_THROTTLE" value="0.90" unit="%"/>
<define name="THROTTLE_SLEW_LIMITER" value="0.5" unit="s"/>
<define name="AUTO_PITCH_MAX_PITCH" value="RadOfDeg(25)"/>
<define name="AUTO_PITCH_MIN_PITCH" value="RadOfDeg(-20)"/>
<!-- Climb loop (throttle) -->
<define name="AUTO_THROTTLE_CLIMB_THROTTLE_INCREMENT" value="0.05" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_PGAIN" value="0.007" unit="%/(m/s)"/>
<define name="AUTO_THROTTLE_IGAIN" value="0.001"/>
<define name="AUTO_THROTTLE_DGAIN" value="0.0"/>
<!-- Climb loop (pitch) -->
<define name="AUTO_THROTTLE_PITCH_OF_VZ_PGAIN" value="0.20" unit="rad/(m/s)"/>
<!--define name="AUTO_PITCH_PGAIN" value="0.0"/>
<define name="AUTO_PITCH_DGAIN" value="0.0"/>
<define name="AUTO_PITCH_IGAIN" value="0.0"/-->
<define name="AUTO_PITCH_PGAIN" value="0.052"/>
<define name="AUTO_PITCH_DGAIN" value="0.0"/>
<define name="AUTO_PITCH_IGAIN" value="0.065"/>
<!-- airspeed control -->
<!--define name="AUTO_AIRSPEED_SETPOINT" value="12."/>
<define name="AUTO_AIRSPEED_THROTTLE_PGAIN" value="0.1"/>
<define name="AUTO_AIRSPEED_THROTTLE_DGAIN" value="0.12"/>
<define name="AUTO_AIRSPEED_THROTTLE_IGAIN" value="0.0"/>
<define name="AUTO_AIRSPEED_PITCH_PGAIN" value="0.06"/>
<define name="AUTO_AIRSPEED_PITCH_DGAIN" value="0.0"/>
<define name="AUTO_AIRSPEED_PITCH_IGAIN" value="0.042"/>
<define name="AIRSPEED_MAX" value="25"/>
<define name="AIRSPEED_MIN" value="8"/-->
<!-- groundspeed control -->
<!--define name="AUTO_GROUNDSPEED_SETPOINT" value="15"/>
<define name="AUTO_GROUNDSPEED_PGAIN" value="1."/>
<define name="AUTO_GROUNDSPEED_IGAIN" value="0."/-->
<!-- Loiter and Dash trimming -->
<define name="AUTO_THROTTLE_LOITER_TRIM" value="0" unit="pprz_t"/>
<define name="AUTO_THROTTLE_DASH_TRIM" value="0" unit="pprz_t"/>
<define name="PITCH_LOITER_TRIM" value="0" unit="pprz_t"/>
<define name="PITCH_DASH_TRIM" value="0" unit="pprz_t"/>
</section>
<!-- ******************* HORIZONTAL CONTROL ******************************** -->
<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
<define name="COURSE_PGAIN" value="1.1"/>
<!-- <define name="COURSE_IGAIN" value="0.01"/> -->
<!-- <define name="COURSE_DGAIN" value="0.02"/> -->
<!-- <define name="COURSE_PRE_BANK_CORRECTION" value="0.5"/> -->
<!-- maybe handy to avoid over corner with lots of wind and small airframe -->
<!-- <define name="COURSE_SLEW_INCREMENT" value="RadOfDeg(4)"/> -->
<define name="ROLL_MAX_SETPOINT" value="50" unit="deg"/>
<define name="PITCH_MAX_SETPOINT" value="35" unit="deg"/>
<define name="PITCH_MIN_SETPOINT" value="-30" unit="deg"/>
<define name="ROLL_ATTITUDE_GAIN" value="7500."/>
<define name="ROLL_RATE_GAIN" value="1500"/>
<!-- only for stabilization adaptive -->
<define name="ROLL_IGAIN" value="500"/>
<define name="ROLL_KFFA" value="0."/>
<define name="ROLL_KFFD" value="0."/>
<!-- ** Maximal roll angle change per 1/60 of second ** -->
<!--define name="ROLL_SLEW" value="0.6"/--> <!-- was 0.05 -->
<define name="PITCH_PGAIN" value="7000."/>
<!-- only for stabilization adaptive -->
<define name="PITCH_DGAIN" value="1000."/>
<define name="PITCH_IGAIN" value="500."/>
<define name="PITCH_KFFA" value="0."/>
<define name="PITCH_KFFD" value="0."/>
<define name="AILERON_OF_THROTTLE" value="0.0"/>
<define name="PITCH_OF_ROLL" value="0.03"/>
</section>
<!-- ******************************** NAV ********************************** -->
<section name="NAV">
<define name="NAV_GLIDE_PITCH_TRIM" value="0"/>
</section>
<!-- ***************************** AGGRESIVE ******************************* -->
<section name="AGGRESSIVE" prefix="AGR_">
<define name="BLEND_START" value="18"/> <!-- Altitude Error to Initiate Aggressive Climb CANNOT BE ZERO!!-->
<define name="BLEND_END" value="8"/> <!-- Altitude Error to Blend Aggressive to Regular Climb Modes CANNOT BE ZERO!!-->
<define name="CLIMB_THROTTLE" value="0.99"/> <!-- Gaz for Aggressive Climb -->
<define name="CLIMB_PITCH" value="RadOfDeg(45)"/> <!-- Pitch for Aggressive Climb -->
<define name="DESCENT_THROTTLE" value="0.5"/> <!-- Gaz for Aggressive Decent -->
<define name="DESCENT_PITCH" value="RadOfDeg(-30)"/> <!-- 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="0.99"/>
</section>
<!-- ****************************** FAILSAFE ******************************* -->
<section name="FAILSAFE" prefix="FAILSAFE_">
<define name="DELAY_WITHOUT_GPS" value="3" unit="s"/>
<define name="DEFAULT_THROTTLE" value="0" unit="%"/>
<define name="DEFAULT_ROLL" value="0.15" unit="rad"/>
<define name="DEFAULT_PITCH" value="-0.1" unit="rad"/>
<define name="HOME_RADIUS" value="60" unit="m"/>
</section>
<!-- ******************************** SIMU ********************************* -->
<section name="SIMU">
<define name="YAW_RESPONSE_FACTOR" value="0.5"/> <!-- a to low of a value gives bad simulation results -->
</section>
</airframe>
@@ -1,177 +0,0 @@
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<airframe name="STM32F4 Discovery Board test">
<firmware name="rotorcraft">
<target name="ap" board="stm32f4_discovery">
<module name="radio_control" type="spektrum">
<define name="RADIO_MODE" value="RADIO_AUX1"/>
</module>
</target>
<module name="motor_mixing"/>
<module name="actuators" type="pwm">
<!--define name="SERVO_HZ" value="400"/-->
</module>
<module name="telemetry" type="transparent"/>
<module name="imu" type="aspirin_v2.1">
<configure name="ASPIRIN_2_SPI_DEV" value="spi1"/>
<configure name="ASPIRIN_2_SPI_SLAVE_IDX" value="SPI_SLAVE0"/>
</module>
<module name="gps" type="ublox"/>
<module name="stabilization" type="int_quat"/>
<module name="ahrs" type="int_cmpl_quat">
<define name="AHRS_GRAVITY_HEURISTIC_FACTOR" value="30"/>
</module>
<module name="ins"/>
</firmware>
<firmware name="test_progs">
<target name="test_adc" board="stm32f4_discovery"/>
<target name="test_lis302dl" board="stm32f4_discovery">
<define name="STM32F4_DISCOVERY_SPI1_FOR_LIS302"/>
</target>
</firmware>
<modules main_freq="512">
</modules>
<servos driver="Pwm">
<servo name="FRONT" no="0" min="1000" neutral="1100" max="1900"/>
<servo name="BACK" no="1" min="1000" neutral="1100" max="1900"/>
<servo name="RIGHT" no="2" min="1000" neutral="1100" max="1900"/>
<servo name="LEFT" no="3" min="1000" neutral="1100" max="1900"/>
</servos>
<commands>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="0"/>
</commands>
<section name="MIXING" prefix="MOTOR_MIXING_">
<define name="TRIM_ROLL" value="0"/>
<define name="TRIM_PITCH" value="0"/>
<define name="TRIM_YAW" value="0"/>
<define name="NB_MOTOR" value="4"/>
<define name="SCALE" value="256"/>
<!-- front/back turning CW, right/left CCW -->
<define name="ROLL_COEF" value="{ 0, 0, -256, 256 }"/>
<define name="PITCH_COEF" value="{ 256, -256, 0, 0 }"/>
<define name="YAW_COEF" value="{ -256, -256, 256, 256 }"/>
<define name="THRUST_COEF" value="{ 256, 256, 256, 256 }"/>
</section>
<command_laws>
<call fun="motor_mixing_run(autopilot_get_motors_on(),FALSE,values)"/>
<set servo="FRONT" value="motor_mixing.commands[0]"/>
<set servo="BACK" value="motor_mixing.commands[1]"/>
<set servo="RIGHT" value="motor_mixing.commands[2]"/>
<set servo="LEFT" value="motor_mixing.commands[3]"/>
</command_laws>
<section name="IMU" prefix="IMU_">
<define name="ACCEL_X_NEUTRAL" value="11"/>
<define name="ACCEL_Y_NEUTRAL" value="11"/>
<define name="ACCEL_Z_NEUTRAL" value="-25"/>
<!-- replace this with your own calibration -->
<define name="MAG_X_NEUTRAL" value="-179"/>
<define name="MAG_Y_NEUTRAL" value="-21"/>
<define name="MAG_Z_NEUTRAL" value="79"/>
<define name="MAG_X_SENS" value="4.17334785618" integer="16"/>
<define name="MAG_Y_SENS" value="3.98885954135" integer="16"/>
<define name="MAG_Z_SENS" value="4.40442339014" integer="16"/>
<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>
<section name="AHRS" prefix="AHRS_">
<define name="H_X" value="0.3770441"/>
<define name="H_Y" value="0.0193986"/>
<define name="H_Z" value="0.9259921"/>
</section>
<section name="INS" prefix="INS_">
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<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_A" value="0"/>
<define name="DEADBAND_E" value="0"/>
<define name="DEADBAND_R" value="250"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="400" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="400." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_Q" value="400" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="400." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_R" value="250" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="1000"/>
<define name="PHI_DGAIN" value="400"/>
<define name="PHI_IGAIN" value="200"/>
<define name="THETA_PGAIN" value="1000"/>
<define name="THETA_DGAIN" value="400"/>
<define name="THETA_IGAIN" value="200"/>
<define name="PSI_PGAIN" value="500"/>
<define name="PSI_DGAIN" value="300"/>
<define name="PSI_IGAIN" value="10"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value="300"/>
<define name="THETA_DDGAIN" value="300"/>
<define name="PSI_DDGAIN" value="300"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<define name="HOVER_KP" value="150"/>
<define name="HOVER_KD" value="80"/>
<define name="HOVER_KI" value="20"/>
<!--define name="NOMINAL_HOVER_THROTTLE" value="0.5"/-->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="MAX_BANK" value="20" unit="deg"/>
<define name="PGAIN" value="50"/>
<define name="DGAIN" value="100"/>
<define name="AGAIN" value="70"/>
<define name="IGAIN" value="20"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_HOVER_Z_HOLD"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
</section>
<section name="BAT">
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/>
<define name="LOW_BAT_LEVEL" value="9.7" unit="V"/>
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/>
</section>
</airframe>
@@ -1,76 +0,0 @@
# Hey Emacs, this is a -*- makefile -*-
#
# stm32f3_discovery_chibios.makefile
#
#
BOARD=stm32f3_discovery
BOARD_VERSION=1.0
BOARD_DIR=$(BOARD)/chibios/v$(BOARD_VERSION)
BOARD_CFG=\"boards/$(BOARD_DIR)/board.h\"
ARCH=chibios
$(TARGET).ARCHDIR = $(ARCH)
RTOS=chibios
## FPU on F3
USE_FPU=hard
$(TARGET).CFLAGS += -DSTM32F3 -DPPRZLINK_ENABLE_FD
##############################################################################
# Architecture or project specific options
#
# Define project name here (target)
PROJECT = $(TARGET)
# Project specific files and paths (see Makefile.chibios for details)
CHIBIOS_BOARD_PLATFORM = STM32F3xx/platform.mk
CHIBIOS_BOARD_LINKER = STM32F303xC.ld
CHIBIOS_BOARD_STARTUP = startup_stm32f3xx.mk
##############################################################################
# Compiler settings
#
MCU = cortex-m4
# default flash mode is via DFU-UTIL
# possibilities: DFU-UTIL, SWD, STLINK
FLASH_MODE ?= DFU-UTIL
HAS_LUFTBOOT = FALSE
#
# default LED configuration
#
RADIO_CONTROL_LED ?= 4
BARO_LED ?= none
AHRS_ALIGNER_LED ?= 5
GPS_LED ?= 6
SYS_TIME_LED ?= 3
#
# default UART configuration (modem, gps, spektrum)
#
MODEM_PORT ?= UART1
MODEM_BAUD ?= B57600
GPS_PORT ?= UART2
GPS_BAUD ?= B38400
RADIO_CONTROL_SPEKTRUM_PRIMARY_PORT ?= UART3
SBUS_PORT ?= UART3
#
# default actuator configuration
#
# you can use different actuators by adding a configure option to your firmware section
# e.g. <configure name="ACTUATORS" value="actuators_ppm/>
# and by setting the correct "driver" attribute in servo section
# e.g. <servo driver="Ppm">
#
ACTUATORS ?= actuators_pwm
-55
View File
@@ -1,55 +0,0 @@
# Hey Emacs, this is a -*- makefile -*-
#
# stm32f4_discovery.makefile
#
#
BOARD=stm32f4_discovery
BOARD_VERSION=
BOARD_CFG=\"boards/$(BOARD).h\"
ARCH=stm32
ARCH_L=f4
ARCH_DIR=stm32
SRC_ARCH=arch/$(ARCH_DIR)
$(TARGET).ARCHDIR = $(ARCH)
$(TARGET).LDSCRIPT=$(SRC_ARCH)/stm32f4_discovery.ld
HARD_FLOAT=yes
# default flash mode is via usb dfu bootloader
# possibilities: STLINK, DFU-UTIL, SWD, JTAG_BMP
FLASH_MODE ?= STLINK
#
# default LED configuration
#
RADIO_CONTROL_LED ?= 4
BARO_LED ?= none
AHRS_ALIGNER_LED ?= 5
GPS_LED ?= 6
SYS_TIME_LED ?= 3
#
# default UART configuration (modem, gps, spektrum)
#
MODEM_PORT ?= UART6
MODEM_BAUD ?= B57600
GPS_PORT ?= UART3
GPS_BAUD ?= B38400
RADIO_CONTROL_SPEKTRUM_PRIMARY_PORT ?= UART1
#
# default actuator configuration
#
# you can use different actuators by adding a configure option to your firmware section
# e.g. <configure name="ACTUATORS" value="actuators_ppm/>
# and by setting the correct "driver" attribute in servo section
# e.g. <servo driver="Ppm">
#
ACTUATORS ?= actuators_pwm
-4
View File
@@ -54,7 +54,6 @@
<variable name="FLASH_MODE" value="DFU-UTIL"/>
<boards>
<board name="apogee_.*"/>
<board name="stm32f4_discovery"/>
<board name="li[s]?a_mx_.*"/>
<board name="navstik_.*"/>
<board name="elle*"/>
@@ -71,7 +70,6 @@
<variable name="FLASH_MODE" value="STLINK"/>
<boards>
<board name="apogee_.*"/>
<board name="stm32f4_discovery"/>
<board name="li[s]?a_mx_.*"/>
<board name="cc3d"/>
<board name="elle*"/>
@@ -89,7 +87,6 @@
<variable name="FLASH_MODE" value="SWD"/>
<boards>
<board name="apogee_.*"/>
<board name="stm32f4_discovery"/>
<board name="li[s]?a_m_.*"/>
<board name="li[s]?a_mx_.*"/>
<board name="px4fmu_.*"/>
@@ -120,7 +117,6 @@
<variable name="FLASH_MODE" value="JTAG_BMP"/>
<boards>
<board name="apogee_*"/>
<board name="stm32f4_discovery"/>
<board name="li[s]?a_[ms]?_.*"/>
<board name="li[s]?a_mx_.*"/>
<board name="px4fmu_.*"/>
@@ -1,34 +0,0 @@
/*
* Copyright (C) 2013 Gautier Hattenberger
*
* This file is part of Paparazzi.
*
* Paparazzi is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 2, or (at your option)
* any later version.
*
* Paparazzi is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with Paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
* Boston, MA 02111-1307, USA.
*/
/* Linker script for ST STM32F4DISCOVERY (STM32F407VG, 1024K flash, 128K RAM). */
/* Define memory regions. */
MEMORY
{
ram (rwx) : ORIGIN = 0x20000000, LENGTH = 128K
/* Reserving 128kb at the end of the flash for persistent settings. */
rom (rx) : ORIGIN = 0x08000000, LENGTH = 896K
}
/* Include the common ld script. */
INCLUDE libopencm3_stm32f4.ld
@@ -1,265 +0,0 @@
/*
ChibiOS - Copyright (C) 2006..2018 Giovanni Di Sirio
Licensed under the Apache License, Version 2.0 (the "License");
you may not use this file except in compliance with the License.
You may obtain a copy of the License at
http://www.apache.org/licenses/LICENSE-2.0
Unless required by applicable law or agreed to in writing, software
distributed under the License is distributed on an "AS IS" BASIS,
WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
See the License for the specific language governing permissions and
limitations under the License.
*/
/*
* This file has been automatically generated using ChibiStudio board
* generator plugin. Do not edit manually.
*/
#include "hal.h"
#include "stm32_gpio.h"
/*===========================================================================*/
/* Driver local definitions. */
/*===========================================================================*/
/*===========================================================================*/
/* Driver exported variables. */
/*===========================================================================*/
/*===========================================================================*/
/* Driver local variables and types. */
/*===========================================================================*/
/**
* @brief Type of STM32 GPIO port setup.
*/
typedef struct {
uint32_t moder;
uint32_t otyper;
uint32_t ospeedr;
uint32_t pupdr;
uint32_t odr;
uint32_t afrl;
uint32_t afrh;
} gpio_setup_t;
/**
* @brief Type of STM32 GPIO initialization data.
*/
typedef struct {
#if STM32_HAS_GPIOA || defined(__DOXYGEN__)
gpio_setup_t PAData;
#endif
#if STM32_HAS_GPIOB || defined(__DOXYGEN__)
gpio_setup_t PBData;
#endif
#if STM32_HAS_GPIOC || defined(__DOXYGEN__)
gpio_setup_t PCData;
#endif
#if STM32_HAS_GPIOD || defined(__DOXYGEN__)
gpio_setup_t PDData;
#endif
#if STM32_HAS_GPIOE || defined(__DOXYGEN__)
gpio_setup_t PEData;
#endif
#if STM32_HAS_GPIOF || defined(__DOXYGEN__)
gpio_setup_t PFData;
#endif
#if STM32_HAS_GPIOG || defined(__DOXYGEN__)
gpio_setup_t PGData;
#endif
#if STM32_HAS_GPIOH || defined(__DOXYGEN__)
gpio_setup_t PHData;
#endif
#if STM32_HAS_GPIOI || defined(__DOXYGEN__)
gpio_setup_t PIData;
#endif
#if STM32_HAS_GPIOJ || defined(__DOXYGEN__)
gpio_setup_t PJData;
#endif
#if STM32_HAS_GPIOK || defined(__DOXYGEN__)
gpio_setup_t PKData;
#endif
} gpio_config_t;
/**
* @brief STM32 GPIO static initialization data.
*/
static const gpio_config_t gpio_default_config = {
#if STM32_HAS_GPIOA
{VAL_GPIOA_MODER, VAL_GPIOA_OTYPER, VAL_GPIOA_OSPEEDR, VAL_GPIOA_PUPDR,
VAL_GPIOA_ODR, VAL_GPIOA_AFRL, VAL_GPIOA_AFRH},
#endif
#if STM32_HAS_GPIOB
{VAL_GPIOB_MODER, VAL_GPIOB_OTYPER, VAL_GPIOB_OSPEEDR, VAL_GPIOB_PUPDR,
VAL_GPIOB_ODR, VAL_GPIOB_AFRL, VAL_GPIOB_AFRH},
#endif
#if STM32_HAS_GPIOC
{VAL_GPIOC_MODER, VAL_GPIOC_OTYPER, VAL_GPIOC_OSPEEDR, VAL_GPIOC_PUPDR,
VAL_GPIOC_ODR, VAL_GPIOC_AFRL, VAL_GPIOC_AFRH},
#endif
#if STM32_HAS_GPIOD
{VAL_GPIOD_MODER, VAL_GPIOD_OTYPER, VAL_GPIOD_OSPEEDR, VAL_GPIOD_PUPDR,
VAL_GPIOD_ODR, VAL_GPIOD_AFRL, VAL_GPIOD_AFRH},
#endif
#if STM32_HAS_GPIOE
{VAL_GPIOE_MODER, VAL_GPIOE_OTYPER, VAL_GPIOE_OSPEEDR, VAL_GPIOE_PUPDR,
VAL_GPIOE_ODR, VAL_GPIOE_AFRL, VAL_GPIOE_AFRH},
#endif
#if STM32_HAS_GPIOF
{VAL_GPIOF_MODER, VAL_GPIOF_OTYPER, VAL_GPIOF_OSPEEDR, VAL_GPIOF_PUPDR,
VAL_GPIOF_ODR, VAL_GPIOF_AFRL, VAL_GPIOF_AFRH},
#endif
#if STM32_HAS_GPIOG
{VAL_GPIOG_MODER, VAL_GPIOG_OTYPER, VAL_GPIOG_OSPEEDR, VAL_GPIOG_PUPDR,
VAL_GPIOG_ODR, VAL_GPIOG_AFRL, VAL_GPIOG_AFRH},
#endif
#if STM32_HAS_GPIOH
{VAL_GPIOH_MODER, VAL_GPIOH_OTYPER, VAL_GPIOH_OSPEEDR, VAL_GPIOH_PUPDR,
VAL_GPIOH_ODR, VAL_GPIOH_AFRL, VAL_GPIOH_AFRH},
#endif
#if STM32_HAS_GPIOI
{VAL_GPIOI_MODER, VAL_GPIOI_OTYPER, VAL_GPIOI_OSPEEDR, VAL_GPIOI_PUPDR,
VAL_GPIOI_ODR, VAL_GPIOI_AFRL, VAL_GPIOI_AFRH},
#endif
#if STM32_HAS_GPIOJ
{VAL_GPIOJ_MODER, VAL_GPIOJ_OTYPER, VAL_GPIOJ_OSPEEDR, VAL_GPIOJ_PUPDR,
VAL_GPIOJ_ODR, VAL_GPIOJ_AFRL, VAL_GPIOJ_AFRH},
#endif
#if STM32_HAS_GPIOK
{VAL_GPIOK_MODER, VAL_GPIOK_OTYPER, VAL_GPIOK_OSPEEDR, VAL_GPIOK_PUPDR,
VAL_GPIOK_ODR, VAL_GPIOK_AFRL, VAL_GPIOK_AFRH}
#endif
};
/*===========================================================================*/
/* Driver local functions. */
/*===========================================================================*/
static void gpio_init(stm32_gpio_t *gpiop, const gpio_setup_t *config) {
gpiop->OTYPER = config->otyper;
gpiop->OSPEEDR = config->ospeedr;
gpiop->PUPDR = config->pupdr;
gpiop->ODR = config->odr;
gpiop->AFRL = config->afrl;
gpiop->AFRH = config->afrh;
gpiop->MODER = config->moder;
}
static void stm32_gpio_init(void) {
/* Enabling GPIO-related clocks, the mask comes from the
registry header file.*/
rccResetAHB1(STM32_GPIO_EN_MASK);
rccEnableAHB1(STM32_GPIO_EN_MASK, true);
/* Initializing all the defined GPIO ports.*/
#if STM32_HAS_GPIOA
gpio_init(GPIOA, &gpio_default_config.PAData);
#endif
#if STM32_HAS_GPIOB
gpio_init(GPIOB, &gpio_default_config.PBData);
#endif
#if STM32_HAS_GPIOC
gpio_init(GPIOC, &gpio_default_config.PCData);
#endif
#if STM32_HAS_GPIOD
gpio_init(GPIOD, &gpio_default_config.PDData);
#endif
#if STM32_HAS_GPIOE
gpio_init(GPIOE, &gpio_default_config.PEData);
#endif
#if STM32_HAS_GPIOF
gpio_init(GPIOF, &gpio_default_config.PFData);
#endif
#if STM32_HAS_GPIOG
gpio_init(GPIOG, &gpio_default_config.PGData);
#endif
#if STM32_HAS_GPIOH
gpio_init(GPIOH, &gpio_default_config.PHData);
#endif
#if STM32_HAS_GPIOI
gpio_init(GPIOI, &gpio_default_config.PIData);
#endif
#if STM32_HAS_GPIOJ
gpio_init(GPIOJ, &gpio_default_config.PJData);
#endif
#if STM32_HAS_GPIOK
gpio_init(GPIOK, &gpio_default_config.PKData);
#endif
}
/*===========================================================================*/
/* Driver interrupt handlers. */
/*===========================================================================*/
/*===========================================================================*/
/* Driver exported functions. */
/*===========================================================================*/
/**
* @brief Early initialization code.
* @details GPIO ports and system clocks are initialized before everything
* else.
*/
void __early_init(void) {
stm32_gpio_init();
stm32_clock_init();
}
#if HAL_USE_SDC || defined(__DOXYGEN__)
/**
* @brief SDC card detection.
*/
bool sdc_lld_is_card_inserted(SDCDriver *sdcp) {
static bool last_status = false;
(void)sdcp;
/* TODO: Fill the implementation.*/
return true;
}
/**
* @brief SDC card write protection detection.
*/
bool sdc_lld_is_write_protected(SDCDriver *sdcp) {
(void)sdcp;
return false;
}
#endif /* HAL_USE_SDC */
#if HAL_USE_MMC_SPI || defined(__DOXYGEN__)
/**
* @brief MMC_SPI card detection.
*/
bool mmc_lld_is_card_inserted(MMCDriver *mmcp) {
(void)mmcp;
/* TODO: Fill the implementation.*/
return true;
}
/**
* @brief MMC_SPI card write protection detection.
*/
bool mmc_lld_is_write_protected(MMCDriver *mmcp) {
(void)mmcp;
/* TODO: Fill the implementation.*/
return false;
}
#endif
/**
* @brief Board-specific initialization code.
* @todo Add your board-specific code, if any.
*/
void boardInit(void) {
}
File diff suppressed because it is too large Load Diff
@@ -1,24 +0,0 @@
#
# ChibiOS/RT - Copyright (C) 2006-2013 Giovanni Di Sirio
#
# Licensed under the Apache License, Version 2.0 (the "License");
# you may not use this file except in compliance with the License.
# You may obtain a copy of the License at
#
# http://www.apache.org/licenses/LICENSE-2.0
#
# Unless required by applicable law or agreed to in writing, software
# distributed under the License is distributed on an "AS IS" BASIS,
# WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
# See the License for the specific language governing permissions and
# limitations under the License.
#
# Required include directories
BOARDINC = $(CHIBIOS_BOARD_DIR)
# List of all the board related files.
BOARDSRC = ${BOARDINC}/board.c
# Shared variables
ALLCSRC += $(BOARDSRC)
ALLINC += $(BOARDINC)
@@ -1,301 +0,0 @@
/*
ChibiOS - Copyright (C) 2006..2016 Giovanni Di Sirio
Licensed under the Apache License, Version 2.0 (the "License");
you may not use this file except in compliance with the License.
You may obtain a copy of the License at
http://www.apache.org/licenses/LICENSE-2.0
Unless required by applicable law or agreed to in writing, software
distributed under the License is distributed on an "AS IS" BASIS,
WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
See the License for the specific language governing permissions and
limitations under the License.
*/
#ifndef MCUCONF_H
#define MCUCONF_H
/*
* STM32F3xx drivers configuration.
* The following settings override the default settings present in
* the various device driver implementation headers.
* Note that the settings for each driver only have effect if the whole
* driver is enabled in halconf.h.
*
* IRQ priorities:
* 15...0 Lowest...Highest.
*
* DMA priorities:
* 0...3 Lowest...Highest.
*/
#define STM32F3xx_MCUCONF
/*
* HAL driver system settings.
*/
#define STM32_NO_INIT FALSE
#define STM32_PVD_ENABLE FALSE
#define STM32_PLS STM32_PLS_LEV0
#define STM32_HSI_ENABLED TRUE
#define STM32_LSI_ENABLED TRUE
#define STM32_HSE_ENABLED TRUE
#define STM32_LSE_ENABLED FALSE
#define STM32_SW STM32_SW_PLL
#define STM32_PLLSRC STM32_PLLSRC_HSE
#define STM32_PREDIV_VALUE 1
#define STM32_PLLMUL_VALUE 9
#define STM32_HPRE STM32_HPRE_DIV1
#define STM32_PPRE1 STM32_PPRE1_DIV2
#define STM32_PPRE2 STM32_PPRE2_DIV2
#define STM32_MCOSEL STM32_MCOSEL_NOCLOCK
#define STM32_ADC12PRES STM32_ADC12PRES_DIV1
#define STM32_ADC34PRES STM32_ADC34PRES_DIV1
#define STM32_USART1SW STM32_USART1SW_PCLK
#define STM32_USART2SW STM32_USART2SW_PCLK
#define STM32_USART3SW STM32_USART3SW_PCLK
#define STM32_UART4SW STM32_UART4SW_PCLK
#define STM32_UART5SW STM32_UART5SW_PCLK
#define STM32_I2C1SW STM32_I2C1SW_SYSCLK
#define STM32_I2C2SW STM32_I2C2SW_SYSCLK
#define STM32_TIM1SW STM32_TIM1SW_PCLK2
#define STM32_TIM8SW STM32_TIM8SW_PCLK2
#define STM32_RTCSEL STM32_RTCSEL_LSI
#define STM32_USB_CLOCK_REQUIRED TRUE
#define STM32_USBPRE STM32_USBPRE_DIV1P5
/*
* ADC driver system settings.
*/
#define STM32_ADC_DUAL_MODE FALSE
#define STM32_ADC_COMPACT_SAMPLES FALSE
#define STM32_ADC_USE_ADC1 TRUE
#define STM32_ADC_USE_ADC2 FALSE
#define STM32_ADC_USE_ADC3 FALSE
#define STM32_ADC_USE_ADC4 FALSE
#define STM32_ADC_ADC1_DMA_STREAM STM32_DMA_STREAM_ID(1, 1)
#define STM32_ADC_ADC2_DMA_STREAM STM32_DMA_STREAM_ID(2, 1)
#define STM32_ADC_ADC3_DMA_STREAM STM32_DMA_STREAM_ID(2, 5)
#define STM32_ADC_ADC4_DMA_STREAM STM32_DMA_STREAM_ID(2, 2)
#define STM32_ADC_ADC1_DMA_PRIORITY 2
#define STM32_ADC_ADC2_DMA_PRIORITY 2
#define STM32_ADC_ADC3_DMA_PRIORITY 2
#define STM32_ADC_ADC4_DMA_PRIORITY 2
#define STM32_ADC_ADC12_IRQ_PRIORITY 5
#define STM32_ADC_ADC3_IRQ_PRIORITY 5
#define STM32_ADC_ADC4_IRQ_PRIORITY 5
#define STM32_ADC_ADC1_DMA_IRQ_PRIORITY 5
#define STM32_ADC_ADC2_DMA_IRQ_PRIORITY 5
#define STM32_ADC_ADC3_DMA_IRQ_PRIORITY 5
#define STM32_ADC_ADC4_DMA_IRQ_PRIORITY 5
#define STM32_ADC_ADC12_CLOCK_MODE ADC_CCR_CKMODE_AHB_DIV1
#define STM32_ADC_ADC34_CLOCK_MODE ADC_CCR_CKMODE_AHB_DIV1
/*
* CAN driver system settings.
*/
#if USE_CAN1
#define STM32_CAN_USE_CAN1 TRUE
#else
#define STM32_CAN_USE_CAN1 FALSE
#endif
#define STM32_CAN_CAN1_IRQ_PRIORITY 11
/*
* DAC driver system settings.
*/
#define STM32_DAC_DUAL_MODE FALSE
#define STM32_DAC_USE_DAC1_CH1 TRUE
#define STM32_DAC_USE_DAC1_CH2 TRUE
#define STM32_DAC_DAC1_CH1_IRQ_PRIORITY 10
#define STM32_DAC_DAC1_CH2_IRQ_PRIORITY 10
#define STM32_DAC_DAC1_CH1_DMA_PRIORITY 2
#define STM32_DAC_DAC1_CH2_DMA_PRIORITY 2
/*
* EXT driver system settings.
*/
#define STM32_EXT_EXTI0_IRQ_PRIORITY 6
#define STM32_EXT_EXTI1_IRQ_PRIORITY 6
#define STM32_EXT_EXTI2_IRQ_PRIORITY 6
#define STM32_EXT_EXTI3_IRQ_PRIORITY 6
#define STM32_EXT_EXTI4_IRQ_PRIORITY 6
#define STM32_EXT_EXTI5_9_IRQ_PRIORITY 6
#define STM32_EXT_EXTI10_15_IRQ_PRIORITY 6
#define STM32_EXT_EXTI16_IRQ_PRIORITY 6
#define STM32_EXT_EXTI17_IRQ_PRIORITY 6
#define STM32_EXT_EXTI18_IRQ_PRIORITY 6
#define STM32_EXT_EXTI19_IRQ_PRIORITY 6
#define STM32_EXT_EXTI20_IRQ_PRIORITY 6
#define STM32_EXT_EXTI21_22_29_IRQ_PRIORITY 6
#define STM32_EXT_EXTI30_32_IRQ_PRIORITY 6
#define STM32_EXT_EXTI33_IRQ_PRIORITY 6
/*
* GPT driver system settings.
*/
#define STM32_GPT_USE_TIM1 FALSE
#define STM32_GPT_USE_TIM2 FALSE
#define STM32_GPT_USE_TIM3 FALSE
#define STM32_GPT_USE_TIM4 FALSE
#define STM32_GPT_USE_TIM6 FALSE
#define STM32_GPT_USE_TIM7 FALSE
#define STM32_GPT_USE_TIM8 FALSE
#define STM32_GPT_TIM1_IRQ_PRIORITY 7
#define STM32_GPT_TIM2_IRQ_PRIORITY 7
#define STM32_GPT_TIM3_IRQ_PRIORITY 7
#define STM32_GPT_TIM4_IRQ_PRIORITY 7
#define STM32_GPT_TIM6_IRQ_PRIORITY 7
#define STM32_GPT_TIM7_IRQ_PRIORITY 7
#define STM32_GPT_TIM8_IRQ_PRIORITY 7
/*
* I2C driver system settings.
*/
#if USE_I2C1
#define STM32_I2C_USE_I2C1 TRUE
#else
#define STM32_I2C_USE_I2C1 FALSE
#endif
#if USE_I2C2
#define STM32_I2C_USE_I2C2 TRUE
#else
#define STM32_I2C_USE_I2C2 FALSE
#endif
#define STM32_I2C_BUSY_TIMEOUT 50
#define STM32_I2C_I2C1_IRQ_PRIORITY 10
#define STM32_I2C_I2C2_IRQ_PRIORITY 10
#define STM32_I2C_USE_DMA TRUE
#define STM32_I2C_I2C1_DMA_PRIORITY 1
#define STM32_I2C_I2C2_DMA_PRIORITY 1
#define STM32_I2C_DMA_ERROR_HOOK(i2cp) osalSysHalt("DMA failure")
/*
* ICU driver system settings.
*/
#define STM32_ICU_USE_TIM1 FALSE
#define STM32_ICU_USE_TIM2 FALSE
#define STM32_ICU_USE_TIM3 FALSE
#define STM32_ICU_USE_TIM4 FALSE
#define STM32_ICU_USE_TIM8 FALSE
#define STM32_ICU_TIM1_IRQ_PRIORITY 7
#define STM32_ICU_TIM2_IRQ_PRIORITY 7
#define STM32_ICU_TIM3_IRQ_PRIORITY 7
#define STM32_ICU_TIM4_IRQ_PRIORITY 7
#define STM32_ICU_TIM8_IRQ_PRIORITY 7
/*
* PWM driver system settings.
*/
#define STM32_PWM_USE_ADVANCED FALSE
#define STM32_PWM_USE_TIM1 FALSE
#ifndef STM32_PWM_USE_TIM2
#define STM32_PWM_USE_TIM2 TRUE
#endif
#ifndef STM32_PWM_USE_TIM3
#define STM32_PWM_USE_TIM3 TRUE
#endif
#define STM32_PWM_USE_TIM4 FALSE
#define STM32_PWM_USE_TIM8 FALSE
#define STM32_PWM_TIM1_IRQ_PRIORITY 7
#define STM32_PWM_TIM2_IRQ_PRIORITY 7
#define STM32_PWM_TIM3_IRQ_PRIORITY 7
#define STM32_PWM_TIM4_IRQ_PRIORITY 7
#define STM32_PWM_TIM8_IRQ_PRIORITY 7
/*
* SERIAL driver system settings.
*/
#if USE_UART1
#define STM32_SERIAL_USE_USART1 TRUE
#else
#define STM32_SERIAL_USE_USART1 FALSE
#endif
#if USE_UART2
#define STM32_SERIAL_USE_USART2 TRUE
#else
#define STM32_SERIAL_USE_USART2 FALSE
#endif
#if USE_UART3
#define STM32_SERIAL_USE_USART3 TRUE
#else
#define STM32_SERIAL_USE_USART3 FALSE
#endif
#if USE_UART4
#define STM32_SERIAL_USE_UART4 TRUE
#else
#define STM32_SERIAL_USE_UART4 FALSE
#endif
#if USE_UART5
#define STM32_SERIAL_USE_UART5 TRUE
#else
#define STM32_SERIAL_USE_UART5 FALSE
#endif
#define STM32_SERIAL_USART1_PRIORITY 12
#define STM32_SERIAL_USART2_PRIORITY 12
#define STM32_SERIAL_USART3_PRIORITY 12
#define STM32_SERIAL_UART4_PRIORITY 12
#define STM32_SERIAL_UART5_PRIORITY 12
/*
* SPI driver system settings.
*/
#if USE_SPI1
#define STM32_SPI_USE_SPI1 TRUE
#else
#define STM32_SPI_USE_SPI1 FALSE
#endif
#if USE_SPI2
#define STM32_SPI_USE_SPI2 TRUE
#else
#define STM32_SPI_USE_SPI2 FALSE
#endif
#if USE_SPI3
#define STM32_SPI_USE_SPI3 TRUE
#else
#define STM32_SPI_USE_SPI3 FALSE
#endif
#define STM32_SPI_SPI1_DMA_PRIORITY 1
#define STM32_SPI_SPI2_DMA_PRIORITY 1
#define STM32_SPI_SPI3_DMA_PRIORITY 1
#define STM32_SPI_SPI1_IRQ_PRIORITY 10
#define STM32_SPI_SPI2_IRQ_PRIORITY 10
#define STM32_SPI_SPI3_IRQ_PRIORITY 10
#define STM32_SPI_DMA_ERROR_HOOK(spip) osalSysHalt("DMA failure")
/*
* ST driver system settings.
*/
#define STM32_ST_IRQ_PRIORITY 8
#define STM32_ST_USE_TIMER 2
/*
* UART driver system settings.
*/
#define STM32_UART_USE_USART1 FALSE
#define STM32_UART_USE_USART2 FALSE
#define STM32_UART_USE_USART3 FALSE
#define STM32_UART_USART1_IRQ_PRIORITY 12
#define STM32_UART_USART2_IRQ_PRIORITY 12
#define STM32_UART_USART3_IRQ_PRIORITY 12
#define STM32_UART_USART1_DMA_PRIORITY 0
#define STM32_UART_USART2_DMA_PRIORITY 0
#define STM32_UART_USART3_DMA_PRIORITY 0
#define STM32_UART_DMA_ERROR_HOOK(uartp) osalSysHalt("DMA failure")
/*
* USB driver system settings.
*/
#define STM32_USB_USE_USB1 TRUE
#define STM32_USB_LOW_POWER_ON_SUSPEND FALSE
#define STM32_USB_USB1_HP_IRQ_PRIORITY 13
#define STM32_USB_USB1_LP_IRQ_PRIORITY 14
/*
* WDG driver system settings.
*/
#define STM32_WDG_USE_IWDG FALSE
#endif /* MCUCONF_H */
File diff suppressed because it is too large Load Diff