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Author SHA1 Message Date
Daniel Agar 9ee8fa21cd PX4 ROS2 msg conformity and explicit topics
- .msg files are PascalCase
 - topics are still either per msg or explicitly listed in TOPICS
 - compatible structs are still generated (eg struct msg_s), but ROS2 style px4::msg::Msg is also available
2022-03-07 10:36:27 -05:00
1016 changed files with 16595 additions and 74802 deletions
-8
View File
@@ -58,29 +58,22 @@ pipeline {
"holybro_can-gps-v1_default",
"holybro_durandal-v1_default",
"holybro_kakutef7_default",
"holybro_kakuteh7_default",
"holybro_pix32v5_default",
"matek_h743-slim",
"matek_gnss-m9n-f4_canbootloader",
"matek_gnss-m9n-f4_default",
"modalai_fc-v1_default",
"modalai_fc-v1_rtps",
"modalai_fc-v2_default",
"mro_ctrl-zero-f7_default",
"mro_ctrl-zero-f7-oem_default",
"mro_ctrl-zero-h7_default",
"mro_ctrl-zero-h7_rtps",
"mro_ctrl-zero-h7-oem_default",
"mro_ctrl-zero-h7-oem_rtps",
"mro_pixracerpro_default",
"mro_pixracerpro_rtps",
"mro_x21-777_default",
"mro_x21_default",
"nxp_fmuk66-e_default",
"nxp_fmuk66-e_rtps",
"nxp_fmuk66-e_socketcan",
"nxp_fmuk66-v3_default",
"nxp_fmuk66-v3_rtps",
"nxp_fmuk66-v3_socketcan",
"nxp_fmurt1062-v1_default",
"nxp_ucans32k146_canbootloader",
@@ -96,7 +89,6 @@ pipeline {
"px4_fmu-v4pro_default",
"px4_fmu-v5_debug",
"px4_fmu-v5_default",
"px4_fmu-v5_rtps",
"px4_fmu-v5_stackcheck",
"px4_fmu-v5_uavcanv0periph",
"px4_fmu-v5_uavcanv1",
+4 -7
View File
@@ -705,21 +705,18 @@ void quickCalibrate() {
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "gyro_calibration status || true"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate accel quick; sleep 1"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate accel quick"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_ACC*"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate gyro; sleep 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate gyro"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_GYRO*"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate level; sleep 2"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate level"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show SENS*"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate mag quick; sleep 1"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate mag quick"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_MAG*"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate baro; sleep 5"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_BARO*"'
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_*"' // parameters after
sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "sensors status"'
}
-1
View File
@@ -23,7 +23,6 @@ jobs:
"shellcheck_all",
"NO_NINJA_BUILD=1 px4_fmu-v5_default",
"NO_NINJA_BUILD=1 px4_sitl_default",
"BUILD_MICRORTPS_AGENT=1 px4_sitl_rtps",
"airframe_metadata",
"module_documentation",
"parameters_metadata",
-1
View File
@@ -20,7 +20,6 @@ jobs:
ark_can-flow,
ark_can-gps,
ark_can-rtk-gps,
ark_cannode,
atl_mantis-edu,
av_x-v1,
bitcraze_crazyflie,
-40
View File
@@ -115,43 +115,3 @@ jobs:
cd Tools/uorb_graph
ls -ls *
# TODO: deploy graph_px4_sitl.json to S3 px4-travis:Firmware/master/
micrortps_agent:
runs-on: ubuntu-latest
container: px4io/px4-dev-base-focal:2021-09-08
steps:
- uses: actions/checkout@v1
with:
token: ${{ secrets.ACCESS_TOKEN }}
- name: microRTPS agent
run: |
make px4_sitl_rtps
git clone https://github.com/PX4/micrortps_agent.git
cp -R build/px4_sitl_rtps/src/modules/micrortps_bridge/micrortps_agent/* micrortps_agent
ROS_msgs:
runs-on: ubuntu-latest
container: px4io/px4-dev-base-focal:2021-09-08
steps:
- uses: actions/checkout@v1
with:
token: ${{ secrets.ACCESS_TOKEN }}
- name: PX4 ROS msgs
run: |
git clone https://github.com/PX4/px4_msgs.git
python3 msg/tools/uorb_to_ros_msgs.py msg/ px4_msgs/msg/
ROS2_bridge:
runs-on: ubuntu-latest
container: px4io/px4-dev-base-focal:2021-09-08
steps:
- uses: actions/checkout@v1
with:
token: ${{ secrets.ACCESS_TOKEN }}
- name: PX4 ROS2 bridge
run: |
git clone https://github.com/PX4/px4_ros_com.git
./msg/tools/uorb_to_ros_urtps_topics.py -i msg/tools/urtps_bridge_topics.yaml -o px4_ros_com/templates/urtps_bridge_topics.yaml
+2 -2
View File
@@ -29,9 +29,9 @@ jobs:
token: ${{ secrets.ACCESS_TOKEN }}
- name: Download MAVSDK
run: wget "https://github.com/mavlink/MAVSDK/releases/download/v$(cat test/mavsdk_tests/MAVSDK_VERSION)/libmavsdk-dev_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
run: wget "https://github.com/mavlink/MAVSDK/releases/download/v$(cat test/mavsdk_tests/MAVSDK_VERSION)/mavsdk_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
- name: Install MAVSDK
run: dpkg -i "libmavsdk-dev_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
run: dpkg -i "mavsdk_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
- name: Prepare ccache timestamp
id: ccache_cache_timestamp
-7
View File
@@ -18,10 +18,6 @@
path = src/drivers/gps/devices
url = https://github.com/PX4/PX4-GPSDrivers.git
branch = master
[submodule "src/modules/micrortps_bridge/micro-CDR"]
path = src/modules/micrortps_bridge/micro-CDR
url = https://github.com/PX4/Micro-CDR.git
branch = master
[submodule "platforms/nuttx/NuttX/nuttx"]
path = platforms/nuttx/NuttX/nuttx
url = https://github.com/PX4/NuttX.git
@@ -64,6 +60,3 @@
path = src/lib/crypto/libtommath
url = https://github.com/PX4/libtommath.git
branch = px4
[submodule "src/modules/microdds_client/Micro-XRCE-DDS-Client"]
path = src/modules/microdds_client/Micro-XRCE-DDS-Client
url = https://github.com/eProsima/Micro-XRCE-DDS-Client.git
+5 -15
View File
@@ -6,11 +6,6 @@ CONFIG:
buildType: RelWithDebInfo
settings:
CONFIG: px4_sitl_default
px4_sitl_rtps:
short: px4_sitl_rtps
buildType: RelWithDebInfo
settings:
CONFIG: px4_sitl_rtps
px4_sitl_asan:
short: px4_sitl (AddressSanitizer)
buildType: AddressSanitizer
@@ -31,6 +26,11 @@ CONFIG:
buildType: RelWithDebInfo
settings:
CONFIG: px4_sitl_test
px4_ros2_default:
short: px4_ros2
buildType: RelWithDebInfo
settings:
CONFIG: px4_ros2_default
px4_io-v2_default:
short: px4_io-v2
buildType: MinSizeRel
@@ -121,16 +121,6 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: ark_can-rtk-gps_canbootloader
ark_cannode_default:
short: ark_cannode_default
buildType: MinSizeRel
settings:
CONFIG: ark_cannode_default
ark_cannode_canbootloader:
short: ark_cannode_canbootloader
buildType: MinSizeRel
settings:
CONFIG: ark_cannode_canbootloader
atl_mantis-edu_default:
short: atl_mantis-edu
buildType: MinSizeRel
+5 -2
View File
@@ -6,7 +6,7 @@
"C_Cpp.autoAddFileAssociations": false,
"C_Cpp.clang_format_fallbackStyle": "none",
"C_Cpp.default.browse.limitSymbolsToIncludedHeaders": true,
"C_Cpp.default.cppStandard": "c++14",
"C_Cpp.default.cppStandard": "c++17",
"C_Cpp.default.cStandard": "c11",
"C_Cpp.formatting": "Disabled",
"C_Cpp.intelliSenseEngine": "Default",
@@ -121,6 +121,7 @@
"variant": "cpp",
"vector": "cpp"
},
"ros.distro": "foxy",
"search.exclude": {
"${workspaceFolder}/build": true
},
@@ -136,5 +137,7 @@
"yaml.schemas": {
"${workspaceFolder}/validation/module_schema.yaml": "${workspaceFolder}/src/modules/*/module.yaml"
},
"cortex-debug.openocdPath": "${env:PICO_SDK_PATH}/../openocd/src/openocd" // Added for rp2040
"python.autoComplete.extraPaths": [
"/opt/ros/foxy/lib/python3.8/site-packages"
]
}
-172
View File
@@ -1,172 +0,0 @@
# This file is NOT licensed under the GPLv3, which is the license for the rest
# of YouCompleteMe.
#
# Here's the license text for this file:
#
# This is free and unencumbered software released into the public domain.
#
# Anyone is free to copy, modify, publish, use, compile, sell, or
# distribute this software, either in source code form or as a compiled
# binary, for any purpose, commercial or non-commercial, and by any
# means.
#
# In jurisdictions that recognize copyright laws, the author or authors
# of this software dedicate any and all copyright interest in the
# software to the public domain. We make this dedication for the benefit
# of the public at large and to the detriment of our heirs and
# successors. We intend this dedication to be an overt act of
# relinquishment in perpetuity of all present and future rights to this
# software under copyright law.
#
# THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND,
# EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF
# MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT.
# IN NO EVENT SHALL THE AUTHORS BE LIABLE FOR ANY CLAIM, DAMAGES OR
# OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE,
# ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR
# OTHER DEALINGS IN THE SOFTWARE.
#
# For more information, please refer to <http://unlicense.org/>
import os
import ycm_core
# These are the compilation flags that will be used in case there's no
# compilation database set (by default, one is not set).
# CHANGE THIS LIST OF FLAGS. YES, THIS IS THE DROID YOU HAVE BEEN LOOKING FOR.
flags = [
'-Wall',
'-Wextra',
'-Werror',
#'-Wc++98-compat',
'-Wno-long-long',
'-Wno-variadic-macros',
'-fexceptions',
'-DNDEBUG',
# You 100% do NOT need -DUSE_CLANG_COMPLETER in your flags; only the YCM
# source code needs it.
#'-DUSE_CLANG_COMPLETER',
# THIS IS IMPORTANT! Without a "-std=<something>" flag, clang won't know which
# language to use when compiling headers. So it will guess. Badly. So C++
# headers will be compiled as C headers. You don't want that so ALWAYS specify
# a "-std=<something>".
# For a C project, you would set this to something like 'c99' instead of
# 'c++14'.
'-std=c++14',
# ...and the same thing goes for the magic -x option which specifies the
# language that the files to be compiled are written in. This is mostly
# relevant for c++ headers.
# For a C project, you would set this to 'c' instead of 'c++'.
'-x',
'c++',
'-undef', # get rid of standard definitions to allow us to include arm math header
'-I', os.path.join(os.path.expanduser("~"),'gcc-arm-none-eabi-4_7-2013q3/arm-none-eabi/include'),
'-I', 'Build/px4_io-v2_default.build/nuttx-export/include/',
'-I', './NuttX/nuttx/arch/arm/include',
'-include', './src/include/visibility.h',
'-I', './src',
'-I', './src/modules',
'-I', './src/include',
'-I', './src/lib',
'-I', './NuttX',
]
# Set this to the absolute path to the folder (NOT the file!) containing the
# compile_commands.json file to use that instead of 'flags'. See here for
# more details: http://clang.llvm.org/docs/JSONCompilationDatabase.html
#
# Most projects will NOT need to set this to anything; you can just change the
# 'flags' list of compilation flags. Notice that YCM itself uses that approach.
compilation_database_folder = ''
if os.path.exists( compilation_database_folder ):
database = ycm_core.CompilationDatabase( compilation_database_folder )
else:
database = None
SOURCE_EXTENSIONS = [ '.cpp', '.cxx', '.cc', '.c', '.m', '.mm' ]
def DirectoryOfThisScript():
return os.path.dirname( os.path.abspath( __file__ ) )
def MakeRelativePathsInFlagsAbsolute( flags, working_directory ):
if not working_directory:
return list( flags )
new_flags = []
make_next_absolute = False
path_flags = [ '-isystem', '-I', '-iquote', '--sysroot=' ]
for flag in flags:
new_flag = flag
if make_next_absolute:
make_next_absolute = False
if not flag.startswith( '/' ):
new_flag = os.path.join( working_directory, flag )
for path_flag in path_flags:
if flag == path_flag:
make_next_absolute = True
break
if flag.startswith( path_flag ):
path = flag[ len( path_flag ): ]
new_flag = path_flag + os.path.join( working_directory, path )
break
if new_flag:
new_flags.append( new_flag )
return new_flags
def IsHeaderFile( filename ):
extension = os.path.splitext( filename )[ 1 ]
return extension in [ '.h', '.hxx', '.hpp', '.hh' ]
def GetCompilationInfoForFile( filename ):
# The compilation_commands.json file generated by CMake does not have entries
# for header files. So we do our best by asking the db for flags for a
# corresponding source file, if any. If one exists, the flags for that file
# should be good enough.
if IsHeaderFile( filename ):
basename = os.path.splitext( filename )[ 0 ]
for extension in SOURCE_EXTENSIONS:
replacement_file = basename + extension
if os.path.exists( replacement_file ):
compilation_info = database.GetCompilationInfoForFile(
replacement_file )
if compilation_info.compiler_flags_:
return compilation_info
return None
return database.GetCompilationInfoForFile( filename )
def FlagsForFile( filename, **kwargs ):
if database:
# Bear in mind that compilation_info.compiler_flags_ does NOT return a
# python list, but a "list-like" StringVec object
compilation_info = GetCompilationInfoForFile( filename )
if not compilation_info:
return None
final_flags = MakeRelativePathsInFlagsAbsolute(
compilation_info.compiler_flags_,
compilation_info.compiler_working_dir_ )
# NOTE: This is just for YouCompleteMe; it's highly likely that your project
# does NOT need to remove the stdlib flag. DO NOT USE THIS IN YOUR
# ycm_extra_conf IF YOU'RE NOT 100% SURE YOU NEED IT.
#try:
# final_flags.remove( '-stdlib=libc++' )
#except ValueError:
# pass
else:
relative_to = DirectoryOfThisScript()
final_flags = MakeRelativePathsInFlagsAbsolute( flags, relative_to )
return {
'flags': final_flags,
'do_cache': True
}
+173 -67
View File
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2017 - 2019 PX4 Development Team. All rights reserved.
# Copyright (c) 2017 - 2022 PX4 Development Team. All rights reserved.
#
# Redistribution and use in source and binary forms, with or without
# modification, are permitted provided that the following conditions
@@ -101,6 +101,8 @@
cmake_minimum_required(VERSION 3.2 FATAL_ERROR)
cmake_policy(SET CMP0058 NEW)
set(PX4_SOURCE_DIR "${CMAKE_CURRENT_SOURCE_DIR}" CACHE FILEPATH "PX4 source directory" FORCE)
set(PX4_BINARY_DIR "${CMAKE_CURRENT_BINARY_DIR}" CACHE FILEPATH "PX4 binary directory" FORCE)
@@ -138,30 +140,41 @@ define_property(GLOBAL PROPERTY PX4_SRC_FILES
BRIEF_DOCS "src files from all PX4 modules & libs"
FULL_DOCS "SRC files from px4_add_{module,library}"
)
define_property(GLOBAL PROPERTY PX4_PUBLICATIONS
BRIEF_DOCS "PX4 publication topics"
FULL_DOCS "List of topics published by PX4 modules"
)
define_property(GLOBAL PROPERTY PX4_SUBSCRIPTIONS
BRIEF_DOCS "PX4 subscription topics"
FULL_DOCS "List of topics subscribed by PX4 modules"
)
#=============================================================================
# configuration
#
set(CONFIG "px4_sitl_default" CACHE STRING "desired configuration")
# default to px4_ros2_default if building within a ROS2 colcon environment
if((DEFINED ENV{COLCON_PREFIX_PATH}) AND (DEFINED ENV{ROS_VERSION}))
if("$ENV{ROS_VERSION}" MATCHES "2")
message(STATUS "ROS_VERSION: $ENV{ROS_VERSION}")
set(CONFIG "px4_ros2_default" CACHE STRING "desired configuration") # TODO
endif()
endif()
if(NOT CONFIG)
set(CONFIG "px4_sitl_default" CACHE STRING "desired configuration")
endif()
include(px4_add_module)
set(config_module_list)
set(config_kernel_list)
# Find Python
# If using catkin, Python 2 is found since it points
# to the Python libs installed with the ROS distro
if (NOT CATKIN_DEVEL_PREFIX)
find_package(PythonInterp 3)
# We have a custom error message to tell users how to install python3.
if (NOT PYTHONINTERP_FOUND)
message(FATAL_ERROR "Python 3 not found. Please install Python 3:\n"
" Ubuntu: sudo apt install python3 python3-dev python3-pip\n"
" macOS: brew install python")
endif()
else()
find_package(PythonInterp REQUIRED)
find_package(PythonInterp 3)
# We have a custom error message to tell users how to install python3.
if(NOT PYTHONINTERP_FOUND)
message(FATAL_ERROR "Python 3 not found. Please install Python 3:\n"
" Ubuntu: sudo apt install python3 python3-dev python3-pip\n"
" macOS: brew install python")
endif()
option(PYTHON_COVERAGE "Python code coverage" OFF)
@@ -197,10 +210,6 @@ set_property(GLOBAL PROPERTY PX4_MODULE_CONFIG_FILES)
include(platforms/${PX4_PLATFORM}/cmake/px4_impl_os.cmake)
list(APPEND CMAKE_MODULE_PATH ${PX4_SOURCE_DIR}/platforms/${PX4_PLATFORM}/cmake)
if(EXISTS "${PX4_SOURCE_DIR}/platforms/${PX4_PLATFORM}/cmake/init.cmake")
include(init)
endif()
# CMake build type (Debug Release RelWithDebInfo MinSizeRel Coverage)
if(NOT CMAKE_BUILD_TYPE)
if(${PX4_PLATFORM} STREQUAL "nuttx")
@@ -236,20 +245,18 @@ project(px4 CXX C ASM)
set(package-contact "px4users@googlegroups.com")
set(CMAKE_CXX_STANDARD 14)
set(CMAKE_CXX_STANDARD 17)
set(CMAKE_CXX_STANDARD_REQUIRED ON)
set(CMAKE_C_STANDARD 11)
set(CMAKE_C_STANDARD_REQUIRED ON)
set(CMAKE_EXPORT_COMPILE_COMMANDS ON)
# For the catkin build process, unset build of dynamically-linked binaries
# and do not change CMAKE_RUNTIME_OUTPUT_DIRECTORY
if (NOT CATKIN_DEVEL_PREFIX)
set(CMAKE_RUNTIME_OUTPUT_DIRECTORY ${PX4_BINARY_DIR})
set(CMAKE_RUNTIME_OUTPUT_DIRECTORY_DEBUG ${PX4_BINARY_DIR})
set(CMAKE_RUNTIME_OUTPUT_DIRECTORY_RELEASE ${PX4_BINARY_DIR})
else()
SET(BUILD_SHARED_LIBS OFF)
set(CMAKE_RUNTIME_OUTPUT_DIRECTORY ${PX4_BINARY_DIR})
set(CMAKE_RUNTIME_OUTPUT_DIRECTORY_DEBUG ${PX4_BINARY_DIR})
set(CMAKE_RUNTIME_OUTPUT_DIRECTORY_RELEASE ${PX4_BINARY_DIR})
if(EXISTS "${PX4_SOURCE_DIR}/platforms/${PX4_PLATFORM}/cmake/init.cmake")
include(init)
endif()
#=============================================================================
@@ -295,21 +302,6 @@ endif()
include(ccache)
#=============================================================================
# find programs and packages
#
# see if catkin was invoked to build this
if (CATKIN_DEVEL_PREFIX)
message(STATUS "catkin ENABLED")
find_package(catkin REQUIRED)
if (catkin_FOUND)
catkin_package()
else()
message(FATAL_ERROR "catkin not found")
endif()
endif()
#=============================================================================
# get chip and chip manufacturer
#
@@ -321,13 +313,6 @@ if(NOT PX4_CHIP)
message(FATAL_ERROR "px4_os_determine_build_chip() needs to set PX4_CHIP")
endif()
#=============================================================================
# build flags
#
include(px4_add_common_flags)
px4_add_common_flags()
px4_os_add_flags()
#=============================================================================
# board cmake init (optional)
#
@@ -335,6 +320,13 @@ if(EXISTS ${PX4_BOARD_DIR}/cmake/init.cmake)
include(${PX4_BOARD_DIR}/cmake/init.cmake)
endif()
#=============================================================================
# build flags
#
include(px4_add_common_flags)
px4_add_common_flags()
px4_os_add_flags()
#=============================================================================
# message, and airframe generation
#
@@ -412,13 +404,17 @@ endif()
# subdirectories
#
add_library(parameters_interface INTERFACE)
add_library(kernel_parameters_interface INTERFACE)
include(px4_add_library)
add_subdirectory(src/lib EXCLUDE_FROM_ALL)
add_subdirectory(platforms/${PX4_PLATFORM}/src/px4)
add_subdirectory(platforms EXCLUDE_FROM_ALL)
add_subdirectory(platforms/${PX4_PLATFORM}/src/px4 EXCLUDE_FROM_ALL)
if(${PX4_PLATFORM} MATCHES "ros2") # TODO: fix
add_subdirectory(platforms/common/work_queue EXCLUDE_FROM_ALL)
else()
add_subdirectory(platforms EXCLUDE_FROM_ALL)
endif()
if(EXISTS "${PX4_BOARD_DIR}/CMakeLists.txt")
add_subdirectory(${PX4_BOARD_DIR})
@@ -435,17 +431,131 @@ add_subdirectory(src/lib/metadata EXCLUDE_FROM_ALL)
# must be the last module before firmware
add_subdirectory(src/lib/parameters EXCLUDE_FROM_ALL)
if(${PX4_PLATFORM} STREQUAL "nuttx" AND NOT CONFIG_BUILD_FLAT)
target_link_libraries(parameters_interface INTERFACE usr_parameters)
target_link_libraries(kernel_parameters_interface INTERFACE parameters)
else()
target_link_libraries(parameters_interface INTERFACE parameters)
endif()
# firmware added last to generate the builtin for included modules
add_subdirectory(platforms/${PX4_PLATFORM})
set(PX4_ORB_TOPIC_COUNT 0)
if(${PX4_PLATFORM} MATCHES "ros2") # TODO: fix
configure_file(${CMAKE_SOURCE_DIR}/build/px4_fmu-v5x_default/uORBTopics.cpp ${CMAKE_BINARY_DIR}/uORBTopics.cpp COPYONLY)
configure_file(${CMAKE_SOURCE_DIR}/build/px4_fmu-v5x_default/uORBTopics.hpp ${CMAKE_BINARY_DIR}/uORBTopics.hpp COPYONLY)
set(PX4_ORB_TOPIC_COUNT 1)
else()
get_property(publications GLOBAL PROPERTY PX4_PUBLICATIONS)
get_property(subscriptions GLOBAL PROPERTY PX4_SUBSCRIPTIONS)
# TODO: for now combine subsriptions and publications for complete topic list
list(APPEND publications ${subscriptions})
list(SORT publications)
list(REMOVE_DUPLICATES publications)
set(pub_all_topics)
set(PX4_MSG_TYPE_ID)
set(PX4_MSG_TOPIC_ID)
set(PX4_MSG_TOPIC_ID_STRING)
set(PX4_MSG_TOPIC_ORB_ID)
set(PX4_ORB_DECLARE_STR)
set(PX4_ORB_DEFINE_STR)
set(PX4_ORB_HEADER_INCLUDE_STR)
foreach(pub ${publications})
#message(STATUS "pub: ${pub}")
string(REPLACE " /" ";" pub ${pub})
list(GET pub 0 pub_type)
list(GET pub 1 pub_topic)
string(REPLACE "::" ";" pub_type_split ${pub_type})
list(GET pub_type_split 2 pub_type_simple_lower)
# Pascal case to snake case (PubType -> pub_type)
string(REGEX REPLACE "(.)([A-Z][a-z]+)" "\\1_\\2" pub_type_simple_lower "${pub_type_simple_lower}")
string(REGEX REPLACE "([a-z0-9])([A-Z])" "\\1_\\2" pub_type_simple_lower "${pub_type_simple_lower}")
string(TOLOWER "${pub_type_simple_lower}" pub_type_simple_lower)
#message(STATUS "pub: Type: ${pub_type}, Topic: ${pub_topic} (${pub_type_simple_lower})")
# pub_type to include path (eg px4::msg::VehicleStatus => px4/msg/vehicle_status.hpp)
# temporary create px4/msg/vehicle_status.hpp which simply includes <uORB/topics/vehicle_status.h>
list(APPEND pub_all_topics ${pub_topic})
list(APPEND PX4_MSG_TYPE_ID ${pub_type})
#list(APPEND PX4_MSG_TOPIC_ID ${pub_topic})
set(PX4_MSG_TOPIC_ID "${PX4_MSG_TOPIC_ID}\t${pub_topic},\n")
#set(PX4_MSG_TOPIC_ID_STRING "${PX4_MSG_TOPIC_ID_STRING}\t"case ORB_ID::${pub_topic}: return \"${pub_topic}\";"\n")
set(PX4_MSG_TOPIC_ORB_ID "${PX4_MSG_TOPIC_ORB_ID}\tORB_ID(${pub_topic}),\n")
list(APPEND PX4_MSG_TOPIC_ID_STRING
"case ORB_ID::${pub_topic}: return \"${pub_topic}\";\n"
)
# PX4_MSG_TYPE_ID
# PX4_MSG_TOPIC_ID
# .h ORB_DECLARE(actuator_controls_0);
# .c ORB_DEFINE(actuator_controls_0, struct actuator_controls_s, 48, __orb_actuator_controls_fields, static_cast<uint8_t>(ORB_ID::actuator_controls_0));
set(PX4_ORB_DECLARE_STR
"${PX4_ORB_DECLARE_STR}ORB_DECLARE(${pub_topic});\n")
# ORB_DEFINE(actuator_armed, struct actuator_armed_s, 16, __orb_actuator_armed_fields, static_cast<uint8_t>(ORB_ID::actuator_armed));
set(PX4_ORB_DEFINE_STR
"${PX4_ORB_DEFINE_STR}ORB_DEFINE(${pub_topic}, ${pub_type}, px4_embedded::${pub_type_simple_lower}_s::SIZE_NO_PADDING, px4_embedded::${pub_type_simple_lower}_s::FIELDS, static_cast<uint8_t>(ORB_ID::${pub_topic}));\n")
set(PX4_ORB_HEADER_INCLUDE_STR
"${PX4_ORB_HEADER_INCLUDE_STR}#include <uORB/topics/${pub_type_simple_lower}.h>\n")
math(EXPR PX4_ORB_TOPIC_COUNT "${PX4_ORB_TOPIC_COUNT}+1")
endforeach()
list(REMOVE_DUPLICATES PX4_MSG_TYPE_ID)
#list(REMOVE_DUPLICATES PX4_MSG_TOPIC_ID)
#message(STATUS "PX4_MSG_TYPE_ID: ${PX4_MSG_TYPE_ID}")
#message(STATUS "PX4_MSG_TOPIC_ID: ${PX4_MSG_TOPIC_ID}")
if(PX4_ORB_TOPIC_COUNT GREATER 0)
configure_file(uORBTopics.cpp.in ${CMAKE_BINARY_DIR}/uORBTopics.cpp)
configure_file(uORBTopics.hpp.in ${CMAKE_BINARY_DIR}/uORBTopics.hpp)
endif()
# .hpp enum ORB_ID
# .cpp struct orb_metadat ORB_ID() array
foreach(f ${msg_files})
#message(STATUS "MSG: ${f}")
endforeach()
endif()
if(PX4_ORB_TOPIC_COUNT GREATER 0)
add_library(uorb_msgs ${uorb_headers} ${CMAKE_BINARY_DIR}/uORBTopics.cpp ${CMAKE_BINARY_DIR}/uORBTopics.hpp)
add_dependencies(uorb_msgs prebuild_targets uorb_headers)
endif()
if(${PX4_PLATFORM} MATCHES "ros2") # TODO: fix
ament_target_dependencies(uorb_msgs rclcpp std_msgs)
rosidl_target_interfaces(uorb_msgs ${PROJECT_NAME} "rosidl_typesupport_cpp")
endif()
#=============================================================================
# uORB graph generation: add a custom target 'uorb_graph'
#
@@ -473,17 +583,13 @@ include(doxygen)
include(metadata)
include(package)
# print size
add_custom_target(size
COMMAND size $<TARGET_FILE:px4>
DEPENDS px4
WORKING_DIRECTORY ${PX4_BINARY_DIR}
USES_TERMINAL
)
# install python requirements using configured python
add_custom_target(install_python_requirements
COMMAND ${PYTHON_EXECUTABLE} -m pip install --requirement ${PX4_SOURCE_DIR}/Tools/setup/requirements.txt
DEPENDS ${PX4_SOURCE_DIR}/Tools/setup/requirements.txt
USES_TERMINAL
)
if(EXISTS "${PX4_SOURCE_DIR}/platforms/${PX4_PLATFORM}/cmake/finalize.cmake")
include(finalize)
endif()
-1
View File
@@ -829,7 +829,6 @@ RECURSIVE = YES
# run.
EXCLUDE = @CMAKE_SOURCE_DIR@/src/modules/uavcan/libuavcan \
@CMAKE_SOURCE_DIR@/src/modules/micrortps_bridge/micro-CDR \
@CMAKE_SOURCE_DIR@/src/examples \
@CMAKE_SOURCE_DIR@/src/templates
Vendored
-172
View File
@@ -12,76 +12,6 @@ pipeline {
}
}
parallel {
// stage('Catkin build on ROS workspace') {
// agent {
// docker {
// image 'px4io/px4-dev-ros-melodic:2021-08-18'
// args '-e CCACHE_BASEDIR=$WORKSPACE -v ${CCACHE_DIR}:${CCACHE_DIR}:rw -e HOME=$WORKSPACE'
// }
// }
// steps {
// sh 'ls -l'
// sh '''#!/bin/bash -l
// echo $0;
// mkdir -p catkin_ws/src;
// cd catkin_ws;
// git -C ${WORKSPACE}/catkin_ws/src/Firmware submodule update --init --recursive --force Tools/sitl_gazebo
// git clone --recursive ${WORKSPACE}/catkin_ws/src/Firmware/Tools/sitl_gazebo src/mavlink_sitl_gazebo;
// git -C ${WORKSPACE}/catkin_ws/src/Firmware fetch --tags;
// source /opt/ros/melodic/setup.bash;
// export PYTHONPATH=/opt/ros/$ROS_DISTRO/lib/python2.7/dist-packages:/usr/lib/python2.7/dist-packages:/usr/local/lib/python2.7/dist-packages;
// catkin init;
// catkin build -j$(nproc) -l$(nproc);
// '''
// // test if the binary was correctly installed and runs using 'mavros_posix_silt.launch'
// sh '''#!/bin/bash -l
// echo $0;
// source catkin_ws/devel/setup.bash;
// rostest px4 pub_test.launch;
// '''
// }
// post {
// always {
// sh 'rm -rf catkin_ws'
// }
// failure {
// archiveArtifacts(allowEmptyArchive: false, artifacts: '.ros/**/*.xml, .ros/**/*.log')
// }
// }
// options {
// checkoutToSubdirectory('catkin_ws/src/Firmware')
// }
// }
stage('Colcon build on ROS2 workspace') {
agent {
docker {
image 'px4io/px4-dev-ros2-foxy:2021-08-18'
args '-e CCACHE_BASEDIR=$WORKSPACE -v ${CCACHE_DIR}:${CCACHE_DIR}:rw -e HOME=$WORKSPACE'
}
}
steps {
sh 'ls -l'
sh '''#!/bin/bash -l
echo $0;
unset ROS_DISTRO;
mkdir -p colcon_ws/src;
cd colcon_ws;
git -C ${WORKSPACE}/colcon_ws/src/Firmware submodule update --init --recursive --force Tools/sitl_gazebo;
git -C ${WORKSPACE}/colcon_ws/src/Firmware fetch --tags;
source /opt/ros/foxy/setup.sh;
colcon build --event-handlers console_direct+ --symlink-install;
'''
}
post {
always {
sh 'rm -rf colcon_ws'
}
}
options {
checkoutToSubdirectory('colcon_ws/src/Firmware')
}
}
stage('Airframe') {
agent {
@@ -254,108 +184,6 @@ pipeline {
}
}
stage('microRTPS agent') {
agent {
docker { image 'px4io/px4-dev-base-focal:2021-08-18' }
}
steps {
sh('export')
sh('git fetch --all --tags')
sh('make distclean; git clean -ff -x -d .')
sh('make px4_sitl_rtps')
withCredentials([usernamePassword(credentialsId: 'px4buildbot_github_personal_token', passwordVariable: 'GIT_PASS', usernameVariable: 'GIT_USER')]) {
sh("git clone https://${GIT_USER}:${GIT_PASS}@github.com/PX4/micrortps_agent.git -b ${BRANCH_NAME}")
sh("rm -rf micrortps_agent/src micrortps_agent/idl")
sh('cp -R build/px4_sitl_rtps/src/modules/micrortps_bridge/micrortps_agent/* micrortps_agent')
sh('cd micrortps_agent; git status; git add src; git commit -a -m "Update microRTPS agent source code `date`" || true')
sh('cd micrortps_agent; git push origin ${BRANCH_NAME} || true')
sh('cd micrortps_agent; git status; git add idl; git commit -a -m "Update IDL definitions `date`" || true')
sh('cd micrortps_agent; git push origin ${BRANCH_NAME} || true')
sh('cd micrortps_agent; git status; git add CMakeLists.txt; git commit -a -m "Update CMakeLists.txt `date`" || true')
sh('cd micrortps_agent; git push origin ${BRANCH_NAME} || true')
sh('rm -rf micrortps_agent')
}
}
when {
anyOf {
branch 'master'
branch 'pr-jenkins' // for testing
}
}
}
stage('PX4 ROS msgs') {
agent {
docker { image 'px4io/px4-dev-base-focal:2021-08-18' }
}
steps {
sh('export')
sh('make distclean; git clean -ff -x -d .')
withCredentials([usernamePassword(credentialsId: 'px4buildbot_github_personal_token', passwordVariable: 'GIT_PASS', usernameVariable: 'GIT_USER')]) {
sh("git clone https://${GIT_USER}:${GIT_PASS}@github.com/PX4/px4_msgs.git")
// 'master' branch
sh('./msg/tools/uorb_to_ros_msgs.py msg/ px4_msgs/msg/')
sh('cd px4_msgs; git status; git add .; git commit -a -m "Update message definitions `date`" || true')
sh('cd px4_msgs; git push origin master || true')
// 'ros1' branch
sh('cd px4_msgs; git checkout ros1')
sh('./msg/tools/uorb_to_ros_msgs.py msg/ px4_msgs/msg/')
sh('cd px4_msgs; git status; git add .; git commit -a -m "Update message definitions `date`" || true')
sh('cd px4_msgs; git push origin ros1 || true')
sh('rm -rf px4_msgs')
}
}
when {
anyOf {
branch 'master'
branch 'pr-jenkins' // for testing
}
}
}
stage('PX4 ROS2 bridge') {
agent {
docker { image 'px4io/px4-dev-base-focal:2021-08-18' }
}
steps {
sh('export')
sh('make distclean; git clean -ff -x -d .')
withCredentials([usernamePassword(credentialsId: 'px4buildbot_github_personal_token', passwordVariable: 'GIT_PASS', usernameVariable: 'GIT_USER')]) {
sh("git clone https://${GIT_USER}:${GIT_PASS}@github.com/PX4/px4_ros_com.git -b ${BRANCH_NAME}")
// deploy uORB RTPS ID map
sh('./msg/tools/uorb_to_ros_urtps_topics.py -i msg/tools/urtps_bridge_topics.yaml -o px4_ros_com/templates/urtps_bridge_topics.yaml')
sh('cd px4_ros_com; git status; git add .; git commit -a -m "Update uORB RTPS ID map `date`" || true')
sh('cd px4_ros_com; git push origin ${BRANCH_NAME} || true')
// deploy uORB RTPS required tools
sh('cp msg/tools/uorb_rtps_classifier.py px4_ros_com/scripts/uorb_rtps_classifier.py')
sh('cp msg/tools/generate_microRTPS_bridge.py px4_ros_com/scripts/generate_microRTPS_bridge.py')
sh('cp msg/tools/px_generate_uorb_topic_files.py px4_ros_com/scripts/px_generate_uorb_topic_files.py')
sh('cp msg/tools/px_generate_uorb_topic_helper.py px4_ros_com/scripts/px_generate_uorb_topic_helper.py')
// deploy templates
sh('cp msg/templates/urtps/microRTPS_agent.cpp.em px4_ros_com/templates/microRTPS_agent.cpp.em')
sh('cp msg/templates/urtps/microRTPS_timesync.cpp.em px4_ros_com/templates/microRTPS_timesync.cpp.em')
sh('cp msg/templates/urtps/microRTPS_timesync.h.em px4_ros_com/templates/microRTPS_timesync.h.em')
sh('cp msg/templates/urtps/microRTPS_transport.cpp px4_ros_com/templates/microRTPS_transport.cpp')
sh('cp msg/templates/urtps/microRTPS_transport.h px4_ros_com/templates/microRTPS_transport.h')
sh('cp msg/templates/urtps/Publisher.cpp.em px4_ros_com/templates/Publisher.cpp.em')
sh('cp msg/templates/urtps/Publisher.h.em px4_ros_com/templates/Publisher.h.em')
sh('cp msg/templates/urtps/Subscriber.cpp.em px4_ros_com/templates/Subscriber.cpp.em')
sh('cp msg/templates/urtps/Subscriber.h.em px4_ros_com/templates/Subscriber.h.em')
sh('cp msg/templates/urtps/RtpsTopics.cpp.em px4_ros_com/templates/RtpsTopics.cpp.em')
sh('cp msg/templates/urtps/RtpsTopics.h.em px4_ros_com/templates/RtpsTopics.h.em')
sh('cd px4_ros_com; git status; git add .; git commit -a -m "Update uORB RTPS script tools `date`" || true')
sh('cd px4_ros_com; git push origin ${BRANCH_NAME} || true')
sh('rm -rf px4_msgs')
}
}
when {
anyOf {
branch 'master'
branch 'pr-jenkins' // for testing
}
}
}
stage('S3') {
agent {
docker { image 'px4io/px4-dev-base-focal:2021-08-18' }
+3
View File
@@ -17,6 +17,8 @@ menu "Toolchain"
bool "posix"
config PLATFORM_QURT
bool "qurt"
config PLATFORM_ROS2
bool "ros2"
endchoice
config BOARD_PLATFORM
@@ -24,6 +26,7 @@ menu "Toolchain"
default "nuttx" if PLATFORM_NUTTX
default "posix" if PLATFORM_POSIX
default "qurt" if PLATFORM_QURT
default "ros2" if PLATFORM_ROS2
config BOARD_LOCKSTEP
bool "Force enable lockstep"
+3 -25
View File
@@ -170,11 +170,6 @@ ifdef PYTHON_EXECUTABLE
CMAKE_ARGS += -DPYTHON_EXECUTABLE=${PYTHON_EXECUTABLE}
endif
# Check if the microRTPS agent is to be built
ifdef BUILD_MICRORTPS_AGENT
CMAKE_ARGS += -DBUILD_MICRORTPS_AGENT=ON
endif
# Functions
# --------------------------------------------------------------------
# describe how to build a cmake config
@@ -251,7 +246,7 @@ endef
# Other targets
# --------------------------------------------------------------------
.PHONY: qgc_firmware px4fmu_firmware misc_qgc_extra_firmware check_rtps
.PHONY: qgc_firmware px4fmu_firmware misc_qgc_extra_firmware
# QGroundControl flashable NuttX firmware
qgc_firmware: px4fmu_firmware misc_qgc_extra_firmware
@@ -276,15 +271,7 @@ misc_qgc_extra_firmware: \
check_airmind_mindpx-v2_default \
sizes
# builds with RTPS
check_rtps: \
check_px4_fmu-v3_rtps \
check_px4_fmu-v4_rtps \
check_px4_fmu-v4pro_rtps \
check_px4_sitl_rtps \
sizes
.PHONY: sizes check quick_check check_rtps uorb_graphs
.PHONY: sizes check quick_check uorb_graphs
sizes:
@-find build -name *.elf -type f | xargs size 2> /dev/null || :
@@ -479,7 +466,7 @@ clang-tidy-quiet: px4_sitl_default-clang
# TODO: Fix cppcheck errors then try --enable=warning,performance,portability,style,unusedFunction or --enable=all
cppcheck: px4_sitl_default
@mkdir -p "$(SRC_DIR)"/build/cppcheck
@cppcheck -i"$(SRC_DIR)"/src/examples --enable=performance --std=c++14 --std=c99 --std=posix --project="$(SRC_DIR)"/build/px4_sitl_default/compile_commands.json --xml-version=2 2> "$(SRC_DIR)"/build/cppcheck/cppcheck-result.xml > /dev/null
@cppcheck -i"$(SRC_DIR)"/src/examples --enable=performance --std=c++17 --std=c99 --std=posix --project="$(SRC_DIR)"/build/px4_sitl_default/compile_commands.json --xml-version=2 2> "$(SRC_DIR)"/build/cppcheck/cppcheck-result.xml > /dev/null
@cppcheck-htmlreport --source-encoding=ascii --file="$(SRC_DIR)"/build/cppcheck/cppcheck-result.xml --report-dir="$(SRC_DIR)"/build/cppcheck --source-dir="$(SRC_DIR)"/src/
shellcheck_all:
@@ -559,12 +546,3 @@ ifneq ($(ROS2_WS_DIR),)
else
ROS2_WS_DIR := ~/colcon_ws
endif
update_ros2_bridge:
@Tools/update_px4_ros2_bridge.sh --ws_dir ${ROS2_WS_DIR} --all
update_px4_ros_com:
@Tools/update_px4_ros2_bridge.sh --ws_dir ${ROS2_WS_DIR} --px4_ros_com
update_px4_msgs:
@Tools/update_px4_ros2_bridge.sh --ws_dir ${ROS2_WS_DIR} --px4_msgs
@@ -36,7 +36,6 @@ add_subdirectory(airframes)
px4_add_romfs_files(
px4-rc.mavlink
px4-rc.params
px4-rc.rtps
px4-rc.simulator
rc.replay
rcS
@@ -10,7 +10,6 @@
# enable fusion of landing target velocity
param set-default LTEST_MODE 1
param set-default PLD_HACC_RAD 0.1
param set-default RTL_PLD_MD 2
# Start up Landing Target Estimator module
landing_target_estimator start
@@ -8,5 +8,8 @@
# disable circuit breaker for airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
set MAV_TYPE 12
param set MAV_TYPE ${MAV_TYPE}
set MIXER_FILE etc/mixers-sitl/uuv_x_sitl.main.mix
set MIXER custom
@@ -8,5 +8,8 @@
# disable circuit breaker for airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
set MAV_TYPE 12
param set MAV_TYPE ${MAV_TYPE}
set MIXER_FILE etc/mixers-sitl/uuv_x_sitl.main.mix
set MIXER custom
@@ -67,3 +67,4 @@ param set-default PWM_MAIN_FUNC7 107
param set-default PWM_MAIN_FUNC8 108
set MIXER skip
@@ -71,6 +71,7 @@ param set-default MPC_XY_VEL_I_ACC 4
param set-default MPC_XY_VEL_D_ACC 0.1
param set-default NAV_ACC_RAD 5
param set-default NAV_LOITER_RAD 80
param set-default VT_FWD_THRUST_EN 4
param set-default VT_F_TRANS_THR 0.75
@@ -79,5 +80,7 @@ param set-default VT_FW_MOT_OFFID 1234
param set-default VT_B_TRANS_DUR 8
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER_FILE etc/mixers-sitl/standard_vtol_sitl.main.mix
set MIXER custom
@@ -7,8 +7,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 20
# param set-default SYS_CTRL_ALLOC 1
param set-default CA_AIRFRAME 4
@@ -70,6 +68,7 @@ param set-default MPC_XY_VEL_I_ACC 4
param set-default MPC_XY_VEL_D_ACC 0.1
param set-default NAV_ACC_RAD 5
param set-default NAV_LOITER_RAD 80
param set-default VT_FW_DIFTHR_EN 1
param set-default VT_FW_DIFTHR_SC 0.5
@@ -79,5 +78,7 @@ param set-default VT_TYPE 0
param set-default WV_EN 0
set MAV_TYPE 20
set MIXER_FILE etc/mixers-sitl/quad_x_vtol.main.mix
set MIXER custom
@@ -7,8 +7,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 21
# param set-default SYS_CTRL_ALLOC 1
param set-default CA_AIRFRAME 3
@@ -82,6 +80,7 @@ param set-default MPC_XY_VEL_I_ACC 4
param set-default MPC_XY_VEL_D_ACC 0.1
param set-default NAV_ACC_RAD 5
param set-default NAV_LOITER_RAD 80
param set-default VT_B_TRANS_DUR 8
param set-default VT_FWD_THRUST_EN 4
@@ -89,5 +88,7 @@ param set-default VT_MOT_ID 1234
param set-default VT_TILT_TRANS 0.6
param set-default VT_TYPE 1
set MAV_TYPE 21
set MIXER_FILE etc/mixers-sitl/tiltrotor_sitl.main.mix
set MIXER custom
@@ -38,6 +38,7 @@ param set-default MPC_XY_VEL_I_ACC 4
param set-default MPC_XY_VEL_D_ACC 0.1
param set-default NAV_ACC_RAD 5
param set-default NAV_LOITER_RAD 80
param set-default VT_FWD_THRUST_EN 4
param set-default VT_F_TRANS_THR 0.75
@@ -50,5 +51,7 @@ param set-default RC_MAP_AUX1 8
param set-default RC_MAP_AUX2 9
param set-default RC_MAP_AUX3 10
set MAV_TYPE 22
set MIXER_FILE etc/mixers-sitl/standard_vtol_sitl.main.mix
set MIXER custom
@@ -37,4 +37,6 @@ param set-default PWM_MAIN_FUNC2 201
param set-default PWM_MAIN_FUNC6 101
param set-default PWM_MAIN_FUNC7 101
set MAV_TYPE 10
set MIXER_FILE skip
@@ -37,4 +37,6 @@ param set-default PWM_MAIN_FUNC2 101
param set-default PWM_MAIN_FUNC6 102
param set-default PWM_MAIN_FUNC7 102
set MAV_TYPE 10
set MIXER_FILE skip
@@ -10,8 +10,6 @@
. ${R}etc/init.d/rc.rover_defaults
param set-default MAV_TYPE 10
param set-default GND_L1_DIST 5
param set-default GND_SP_CTRL_MODE 1
param set-default GND_SPEED_D 3
@@ -35,4 +33,6 @@ param set-default CBRK_AIRSPD_CHK 162128
param set-default GND_MAX_ANG 0.6
param set-default GND_WHEEL_BASE 3.0
set MAV_TYPE 10
set MIXER_FILE etc/mixers-sitl/rover_ackermann_sitl.main.mix
@@ -47,4 +47,6 @@ param set-default CA_R_REV 3
param set-default PWM_MAIN_FUNC1 101
param set-default PWM_MAIN_FUNC2 102
set MAV_TYPE 11
set MIXER skip
@@ -9,8 +9,6 @@
. ${R}etc/init.d/rc.mc_defaults
param set-default MAV_TYPE 13
param set-default MC_PITCHRATE_P 0.1
param set-default MC_PITCHRATE_I 0.05
param set-default MC_PITCH_P 6.0
@@ -26,4 +24,6 @@ param set-default TRIG_MODE 4
param set-default MNT_MODE_IN 4
param set-default MNT_DO_STAB 2
set MAV_TYPE 13
set MIXER hexa_x
@@ -7,8 +7,6 @@
. ${R}etc/init.d/rc.mc_defaults
param set-default MAV_TYPE 13
param set-default MC_PITCHRATE_P 0.0800
param set-default MC_PITCHRATE_I 0.0400
param set-default MC_PITCHRATE_D 0.0010
@@ -28,4 +26,6 @@ param set-default MNT_MODE_IN 4
param set-default MNT_MODE_OUT 2
param set-default MAV_PROTO_VER 2
set MAV_TYPE 13
set MIXER hexa_x
@@ -7,8 +7,6 @@
. ${R}etc/init.d/rc.mc_defaults
param set-default MAV_TYPE 13
param set-default SYS_CTRL_ALLOC 1
param set-default MC_PITCHRATE_P 0.0800
@@ -60,5 +58,7 @@ param set-default PWM_MAIN_FUNC4 104
param set-default PWM_MAIN_FUNC5 105
param set-default PWM_MAIN_FUNC6 106
set MAV_TYPE 13
set MIXER skip
set MIXER_AUX none
@@ -1,4 +0,0 @@
#!/bin/sh
# shellcheck disable=SC2154
micrortps_client start -t UDP -r $((2019+2*px4_instance)) -s $((2020+2*px4_instance))
+7 -13
View File
@@ -24,6 +24,7 @@ fi
# initialize script variables
set IO_PRESENT no
set MAV_TYPE none
set MIXER none
set MIXER_AUX none
set MIXER_FILE none
@@ -223,21 +224,8 @@ rc_update start
manual_control start
sensors start
commander start
# Configure vehicle type specific parameters.
# Note: rc.vehicle_setup is the entry point for rc.interface,
# rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
#
. ${R}etc/init.d/rc.vehicle_setup
navigator start
# Try to start the micrortps_client with UDP transport if module exists
if px4-micrortps_client status > /dev/null 2>&1
then
. px4-rc.rtps
fi
if param greater -s MNT_MODE_IN -1
then
gimbal start
@@ -259,6 +247,12 @@ then
gyro_calibration start
fi
# Configure vehicle type specific parameters.
# Note: rc.vehicle_setup is the entry point for rc.interface,
# rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
#
. ${R}etc/init.d/rc.vehicle_setup
#user defined mavlink streams for instances can be in PATH
. px4-rc.mavlink
@@ -36,5 +36,4 @@ param set-default MC_PITCHRATE_P 0.19
param set-default MC_PITCHRATE_I 0.05
param set-default MC_PITCHRATE_D 0.004
param set-default MC_YAW_P 4
set MIXER quad_w
@@ -49,6 +49,7 @@ param set-default MPC_Z_VEL_MAX_DN 1.5
param set-default NAV_ACC_RAD 5
param set-default NAV_DLL_ACT 2
param set-default NAV_LOITER_RAD 80
param set-default RTL_DESCEND_ALT 10
param set-default RTL_RETURN_ALT 30
@@ -103,7 +104,7 @@ param set-default CBRK_SUPPLY_CHK 894281
param set-default COM_PREARM_MODE 0
param set-default CBRK_IO_SAFETY 22027
param set-default MAV_TYPE 22
set MAV_TYPE 22
set MIXER standard_vtol_hitl
@@ -47,7 +47,7 @@ param set-default HIL_ACT_FUNC6 201
param set-default HIL_ACT_REV 32
param set-default MAV_TYPE 19
set MAV_TYPE 19
set MIXER vtol_tailsitter_duo_sat
set PWM_OUT 1234
@@ -54,8 +54,7 @@ param set-default PWM_AUX_DIS5 950
param set-default VT_TYPE 2
param set-default VT_MOT_ID 1234
param set-default VT_FW_MOT_OFFID 1234
param set-default MAV_TYPE 22
set MAV_TYPE 22
set MIXER quad_x
set MIXER_AUX vtol_AAERT
@@ -19,6 +19,7 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 19
param set-default MC_ROLL_P 6
@@ -37,6 +38,7 @@ param set-default VT_IDLE_PWM_MC 1080
param set-default VT_ELEV_MC_LOCK 0
param set-default VT_MOT_ID 12
param set-default VT_TYPE 0
set MAV_TYPE 19
set MIXER vtol_tailsitter_duo
@@ -23,7 +23,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 21
param set-default MC_ROLL_P 7
param set-default MC_ROLLRATE_P 0.19
@@ -46,6 +45,7 @@ param set-default VT_TILT_TRANS 0.5
param set-default VT_TILT_FW 0.9
param set-default VT_ELEV_MC_LOCK 0
param set-default VT_TYPE 1
set MAV_TYPE 21
set MIXER firefly6
set MIXER_AUX firefly6
@@ -13,8 +13,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 20
param set-default CA_AIRFRAME 4
param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 0.15
@@ -40,6 +38,7 @@ param set-default PWM_MAIN_MAX 2000
param set-default VT_MOT_ID 1234
param set-default VT_IDLE_PWM_MC 1080
param set-default VT_TYPE 0
set MAV_TYPE 20
set MIXER quad_x_vtol
@@ -22,13 +22,13 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 20
param set-default PWM_MAIN_MAX 2000
param set-default VT_IDLE_PWM_MC 1080
param set-default VT_TYPE 0
set MAV_TYPE 20
set MIXER quad_+_vtol
set PWM_OUT 1234
@@ -52,6 +52,7 @@ param set-default VT_MOT_ID 1234
param set-default VT_FW_MOT_OFFID 1234
param set-default VT_IDLE_PWM_MC 1080
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER quad_x
set MIXER_AUX vtol_AAERT
@@ -41,6 +41,7 @@ param set-default VT_FW_MOT_OFFID 1234
param set-default VT_F_TRANS_THR 0.75
param set-default VT_IDLE_PWM_MC 1080
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER quad_x
set MIXER_AUX vtol_delta
@@ -33,6 +33,7 @@ param set-default VT_MOT_ID 1234
param set-default VT_FW_MOT_OFFID 1234
param set-default VT_IDLE_PWM_MC 1080
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER quad_x
set MIXER_AUX vtol_AAVVT
@@ -46,6 +46,7 @@ param set-default VT_IDLE_PWM_MC 1080
param set-default VT_MOT_ID 1234
param set-default VT_FW_MOT_OFFID 1234
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER quad_x
set MIXER_AUX vtol_AAERT
@@ -77,6 +77,8 @@ param set-default VT_TRANS_MIN_TM 5
param set-default VT_TRANS_TIMEOUT 30
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER quad_x
set MIXER_AUX vtol_AAERT
@@ -13,8 +13,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-defualt MAV_TYPE 21
param set-default PWM_AUX_DISARM 1000
param set-default PWM_AUX_MAX 2000
param set-default PWM_AUX_MIN 1000
@@ -30,6 +28,7 @@ param set-default VT_TILT_MC 0.08
param set-default VT_TILT_TRANS 0.5
param set-default VT_ELEV_MC_LOCK 0
param set-default VT_TYPE 1
set MAV_TYPE 21
set MIXER claire
set MIXER_AUX claire
@@ -22,8 +22,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-defualt MAV_TYPE 21
param set-default CBRK_AIRSPD_CHK 162128
param set-default FW_ARSP_MODE 1
@@ -66,6 +64,7 @@ param set-default VT_TRANS_MIN_TM 1.2
param set-default VT_TRANS_P2_DUR 1.3
param set-default VT_ELEV_MC_LOCK 0
param set-default VT_TYPE 1
set MAV_TYPE 21
set MIXER vtol_convergence
@@ -22,8 +22,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 22
param set-default BAT1_CAPACITY 23000
param set-default BAT1_N_CELLS 4
param set-default BAT1_R_INTERNAL 0.0025
@@ -136,6 +134,7 @@ param set-default VT_TRANS_TIMEOUT 22
param set-default VT_F_TRANS_RAMP 4
param set-default COM_RC_OVERRIDE 0
set MAV_TYPE 22
set MIXER deltaquad
set MIXER_AUX pass
@@ -23,8 +23,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 22
param set-default BAT1_N_CELLS 6
param set-default FW_AIRSPD_MAX 30
@@ -96,6 +94,8 @@ param set-default VT_PSHER_RMP_DT 2
param set-default VT_TRANS_MIN_TM 4
param set-default VT_TYPE 2
set MAV_TYPE 22
set MIXER babyshark
set MIXER_AUX pass
@@ -27,8 +27,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 21
param set-default VT_IDLE_PWM_MC 1100
param set-default VT_TYPE 1
param set-default VT_MOT_ID 1234
@@ -59,6 +57,8 @@ param set-default CA_SV_CS3_TRQ_Y 1.0
param set-default CA_SV_CS3_TYPE 4
param set-default CA_SV_TL_COUNT 4
set MAV_TYPE 21
set MIXER quad_x
set MIXER_AUX vtol_TTTTAAER
@@ -31,6 +31,7 @@ param set-default PWM_AUX_DIS5 950
param set-default VT_TYPE 2
param set-default VT_MOT_ID 12345678
param set-default VT_FW_MOT_OFFID 12345678
set MAV_TYPE 22
set MIXER octo_cox
set MIXER_AUX vtol_AAERT
@@ -19,8 +19,6 @@
. ${R}etc/init.d/rc.vtol_defaults
param set-default MAV_TYPE 19
param set-default VT_ELEV_MC_LOCK 0
param set-default VT_MOT_COUNT 2
param set-default VT_TYPE 0
@@ -39,6 +37,8 @@ param set-default CA_SV_CS1_TRQ_P 0.5
param set-default CA_SV_CS1_TRQ_Y -0.5
param set-default CA_SV_CS1_TYPE 6
param set-default MAV_TYPE 19
set MAV_TYPE 19
set MIXER vtol_tailsitter_duo
set PWM_OUT 1234
@@ -18,7 +18,4 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_TRICOPTER 15
param set-default MAV_TYPE 15
set MIXER tri_y_yaw+
@@ -18,7 +18,4 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_TRICOPTER 15
param set-default MAV_TYPE 15
set MIXER tri_y_yaw-
@@ -17,9 +17,7 @@
#
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_COAXIAL 3
param set-default MAV_TYPE 3
set MIXER coax
param set-default MC_ROLLRATE_P 0.17
param set-default MC_ROLLRATE_I 0.05
@@ -38,9 +36,6 @@ param set-default PWM_MAIN_RATE 400
param set-default RTL_RETURN_ALT 30
param set-default RTL_DESCEND_ALT 10
set MIXER coax
# This is the gimbal pass mixer
set MIXER_AUX pass
@@ -20,7 +20,7 @@
. ${R}etc/init.d/rc.mc_defaults
# Configure as helicopter (number 4 defined in commander_helper.cpp)
param set-default MAV_TYPE 4
set MAV_TYPE 4
set MIXER blade130
@@ -41,6 +41,5 @@ param set-default FW_R_LIM 40
param set-default FW_P_LIM_MAX 25
param set-default FW_P_LIM_MIN -5
param set-default FW_P_RMAX_NEG 20
set MIXER TF-G2
set MIXER_AUX pass
@@ -24,5 +24,8 @@ param set-default MAV_0_CONFIG 102
param set-default GPS_UBX_DYNMODEL 8
param set-default SER_TEL2_BAUD 9600
set MAV_TYPE 8
param set MAV_TYPE ${MAV_TYPE}
set MIXER IO_pass
set MIXER_AUX pass
@@ -26,7 +26,7 @@
# @board px4_fmu-v2 exclude
#
. ${R}etc/init.d/rc.mc_defaults
set VEHICLE_TYPE mc
param set-default NAV_ACC_RAD 2
@@ -39,7 +39,6 @@ param set-default PWM_MAIN_RATE 400
param set-default RTL_DESCEND_ALT 10
param set-default RTL_RETURN_ALT 30
set MIXER dodeca_top_cox
set MIXER_AUX dodeca_bottom_cox
@@ -41,6 +41,9 @@ param set-default FW_RR_P 0.04
param set-default PWM_MAIN_DISARM 1000
# Configure this as plane.
set MAV_TYPE 1
# Set mixer.
set MIXER fw_generic_wing
@@ -24,6 +24,8 @@
set MIXER quad_s250aq
set MAV_TYPE 2
param set-default ATT_BIAS_MAX 0
param set-default CBRK_IO_SAFETY 22027
@@ -21,7 +21,10 @@
# @board cuav_x7pro exclude
#
. ${R}etc/init.d/rc.mc_defaults
set VEHICLE_TYPE mc
set MIXER quad_x
set PWM_OUT 1234
# Attitude & rate gains
param set-default MC_ROLLRATE_D 0.0013
@@ -21,7 +21,10 @@
# @maintainer Hyon Lim <lim@uvify.com>
#
. ${R}etc/init.d/rc.mc_defaults
set VEHICLE_TYPE mc
set MIXER quad_x
set PWM_OUT 1234
# Attitude & rate gains
param set-default MC_ROLLRATE_D 0.0013
@@ -24,6 +24,10 @@
. ${R}etc/init.d/rc.mc_defaults
# Configure this as Quadrotor
# set MAV_TYPE 14
# Set mixer
set MIXER tilt_quad
set MIXER_AUX tilt_quad
@@ -48,6 +48,8 @@ param set-default NAV_ACC_RAD 0.5
param set-default PWM_MAIN_DISARM 1500
param set-default PWM_MAIN_MAX 2000
param set-default PWM_MAIN_MIN 1000
# Configure this as rover
set MAV_TYPE 10
# Set mixer
set MIXER rover_generic
@@ -76,6 +76,9 @@ param set-default RBCLW_SER_CFG 104
# Start this driver after setting parameters, because the driver uses some of those parameters.
# roboclaw start /dev/ttyS3
# Configure this as rover
set MAV_TYPE 10
# Set mixer
set MIXER generic_diff_rover
@@ -65,6 +65,9 @@ param set-default PWM_MAIN_MIN4 970
# Enable Airspeed check circuit breaker because Rovers will have no airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
# Configure this as rover
set MAV_TYPE 10
# Set mixer
set MIXER rover_diff_and_servo
@@ -16,4 +16,7 @@
# disable circuit breaker for airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
set MAV_TYPE 12
param set MAV_TYPE ${MAV_TYPE}
set MIXER uuv_x
@@ -16,4 +16,7 @@
# disable circuit breaker for airspeed sensor
param set-default CBRK_AIRSPD_CHK 162128
set MAV_TYPE 12
param set MAV_TYPE ${MAV_TYPE}
set MIXER uuv_x
@@ -23,9 +23,6 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_HEXAROTOR 13
param set-default MAV_TYPE 13
param set-default CA_ROTOR_COUNT 6
param set-default CA_ROTOR0_PX 0.0
param set-default CA_ROTOR0_PY 0.5
@@ -27,8 +27,9 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_HEXAROTOR 13
param set-default MAV_TYPE 13
set MIXER hexa_x
set PWM_OUT 12345678
###############################################
# Attitude & rate gains
@@ -119,7 +120,3 @@ param set-default MAV_1_MODE 2
param set-default MAV_1_FORWARD 1
param set-default MAV_1_RATE 800000
param set-default SER_TEL2_BAUD 921600
set MIXER hexa_x
set PWM_OUT 12345678
@@ -23,9 +23,6 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_HEXAROTOR 13
param set-default MAV_TYPE 13
param set-default CA_ROTOR_COUNT 6
param set-default CA_ROTOR0_PX 0.5
param set-default CA_ROTOR0_PY 0.0
@@ -25,9 +25,6 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_OCTOROTOR 14
param set-default MAV_TYPE 14
param set-default CA_ROTOR_COUNT 8
param set-default CA_ROTOR0_KM -0.05
param set-default CA_ROTOR0_PX 0.46
@@ -25,9 +25,6 @@
. ${R}etc/init.d/rc.mc_defaults
# MAV_TYPE_OCTOROTOR 14
param set-default MAV_TYPE 14
set MIXER octo_+
set PWM_OUT 12345678
@@ -7,9 +7,6 @@
set VEHICLE_TYPE airship
# MAV_TYPE_AIRSHIP 7
param set-default MAV_TYPE 7
#
# This is the gimbal pass mixer.
#
@@ -7,9 +7,6 @@
set VEHICLE_TYPE fw
# MAV_TYPE_FREE_BALLOON 8
param set-default MAV_TYPE 8
#
# Default parameters for balloon UAVs.
#
@@ -7,9 +7,6 @@
set VEHICLE_TYPE rover
# MAV_TYPE_SURFACE_BOAT 11
param set-default MAV_TYPE 11
#
# Default parameters for UGVs.
#
+2 -3
View File
@@ -7,15 +7,14 @@
set VEHICLE_TYPE fw
# MAV_TYPE_FIXED_WING 1
param set-default MAV_TYPE 1
#
# Default parameters for fixed wing UAVs.
#
param set-default COM_POS_FS_DELAY 5
param set-default COM_POS_FS_EPH 15
param set-default COM_POS_FS_EPV 30
param set-default COM_POS_FS_GAIN 0
param set-default COM_POS_FS_PROB 1
param set-default COM_VEL_FS_EVH 5
# Disable preflight disarm to not interfere with external launching
param set-default COM_DISARM_PRFLT -1
@@ -7,9 +7,6 @@
set VEHICLE_TYPE mc
# MAV_TYPE_QUADROTOR 2
param set-default MAV_TYPE 2
if param compare IMU_GYRO_RATEMAX 400
then
param set-default IMU_GYRO_RATEMAX 800
@@ -7,9 +7,6 @@
set VEHICLE_TYPE rover
# MAV_TYPE_GROUND_ROVER 10
param set-default MAV_TYPE 10
#
# Default parameters for UGVs.
#
+4 -23
View File
@@ -83,28 +83,16 @@ then
teraranger start -X
fi
# paa3905 optical flow sensor (external SPI)
if param greater -s SENS_EN_PAA3905 0
then
paa3905 -S start
fi
# paw3902 optical flow sensor (external SPI)
if param greater -s SENS_EN_PAW3902 0
then
paw3902 -S start
fi
# pmw3901 optical flow sensor (external SPI)
# Possible external pmw3901 optical flow sensor
if param greater -s SENS_EN_PMW3901 0
then
pmw3901 -S start
fi
# Check for px4flow sensor
if param compare -s SENS_EN_PX4FLOW 1
# Possible external paw3902 optical flow sensor
if param greater -s SENS_EN_PAW3902 0
then
px4flow start -X
paw3902 -S start
fi
# vl53l1x i2c distance sensor
@@ -167,13 +155,6 @@ then
irlock start -X
fi
# SPL06 sensor external I2C
if param compare -s SENS_EN_SPL06 1
then
spl06 -X start
spl06 -X -a 0x77 start
fi
# PCF8583 counter (RPM sensor)
if param compare -s SENS_EN_PCF8583 1
then
@@ -7,9 +7,6 @@
set VEHICLE_TYPE uuv
# MAV_TYPE_SUBMARINE 12
param set-default MAV_TYPE 12
param set-default PWM_MAIN_MAX 1950
param set-default PWM_MAIN_MIN 1050
param set-default PWM_MAIN_DISARM 1500
+93 -2
View File
@@ -12,9 +12,19 @@ if [ $VEHICLE_TYPE = fw ]
then
if [ $MIXER = none ]
then
echo "FW mixer undefined"
# Set default mixer for fixed wing if not defined.
set MIXER AERT
fi
if [ $MAV_TYPE = none ]
then
# Set a default MAV_TYPE = 1 if not defined.
set MAV_TYPE 1
fi
# Set the mav type parameter.
param set MAV_TYPE ${MAV_TYPE}
# Load mixer and configure outputs.
. ${R}etc/init.d/rc.interface
@@ -32,6 +42,41 @@ then
echo "MC mixer undefined"
fi
if [ $MAV_TYPE = none ]
then
# Set a default MAV_TYPE = 2 if not defined.
set MAV_TYPE 2
# Use mixer to detect vehicle type
if [ $MIXER = coax ]
then
set MAV_TYPE 3
fi
if [ $MIXER = hexa_x -o $MIXER = hexa_+ ]
then
set MAV_TYPE 13
fi
if [ $MIXER = hexa_cox ]
then
set MAV_TYPE 13
fi
if [ $MIXER = octo_x -o $MIXER = octo_+ ]
then
set MAV_TYPE 14
fi
if [ $MIXER = octo_cox -o $MIXER = octo_cox_w ]
then
set MAV_TYPE 14
fi
if [ $MIXER = tri_y_yaw- -o $MIXER = tri_y_yaw+ ]
then
set MAV_TYPE 15
fi
fi
# Set the mav type parameter.
param set MAV_TYPE ${MAV_TYPE}
# Load mixer and configure outputs.
. ${R}etc/init.d/rc.interface
@@ -46,9 +91,19 @@ if [ $VEHICLE_TYPE = rover ]
then
if [ $MIXER = none ]
then
echo "rover mixer undefined"
# Set default mixer for UGV if not defined.
set MIXER rover_generic
fi
if [ $MAV_TYPE = none ]
then
# Set a default MAV_TYPE = 10 if not defined.
set MAV_TYPE 10
fi
# Set the mav type parameter.
param set MAV_TYPE ${MAV_TYPE}
# Load mixer and configure outputs.
. ${R}etc/init.d/rc.interface
@@ -66,6 +121,25 @@ then
echo "VTOL mixer undefined"
fi
if [ $MAV_TYPE = none ]
then
# Set a default MAV_TYPE = 19 if not defined.
set MAV_TYPE 19
# Use mixer to detect vehicle type.
if [ $MIXER = firefly6 ]
then
set MAV_TYPE 21
fi
if [ $MIXER = quad_x_pusher_vtol ]
then
set MAV_TYPE 22
fi
fi
# Set the mav type parameter.
param set MAV_TYPE ${MAV_TYPE}
# Load mixer and configure outputs.
. ${R}etc/init.d/rc.interface
@@ -83,6 +157,15 @@ then
echo "Airship mixer undefined"
fi
if [ $MAV_TYPE = none ]
then
# Set a default MAV_TYPE = 7 if not defined.
set MAV_TYPE 7
fi
# Set the mav type parameter.
param set MAV_TYPE ${MAV_TYPE}
# Load mixer and configure outputs.
. ${R}etc/init.d/rc.interface
@@ -100,11 +183,19 @@ then
echo "UUV mixer undefined"
fi
if [ $MAV_TYPE = none ]
then
# Set default MAV_TYPE to submarine if not defined
set MAV_TYPE 12
fi
param set MAV_TYPE ${MAV_TYPE}
# Load mixer and configure outputs.
. ${R}etc/init.d/rc.interface
# Start standard vtol apps.
. ${R}etc/init.d/rc.uuv_apps
fi
@@ -7,9 +7,6 @@
set VEHICLE_TYPE vtol
# MAV_TYPE_VTOL_FIXEDROTOR 22
param set-default MAV_TYPE 22
param set-default MIS_TAKEOFF_ALT 20
param set-default MIS_YAW_TMT 10
+15 -7
View File
@@ -29,6 +29,7 @@ set IOFW "/etc/extras/px4_io-v2_default.bin"
set IO_PRESENT no
set LOGGER_ARGS ""
set LOGGER_BUF 8
set MAV_TYPE none
set MIXER none
set MIXER_AUX none
set MIXER_FILE none
@@ -408,13 +409,6 @@ else
commander start
fi
#
# Configure vehicle type specific parameters.
# Note: rc.vehicle_setup is the entry point for rc.interface,
# rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
#
. ${R}etc/init.d/rc.vehicle_setup
# Pre-takeoff continuous magnetometer calibration
if param compare -s MBE_ENABLE 1
then
@@ -465,6 +459,13 @@ else
fi
fi
#
# Configure vehicle type specific parameters.
# Note: rc.vehicle_setup is the entry point for rc.interface,
# rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
#
. ${R}etc/init.d/rc.vehicle_setup
#
# Play the startup tune (if not disabled or there is an error)
#
@@ -492,6 +493,12 @@ else
gimbal start
fi
# Check for flow sensor
if param compare -s SENS_EN_PX4FLOW 1
then
px4flow start -X
fi
# Blacksheep telemetry
if param compare -s TEL_BST_EN 1
then
@@ -566,6 +573,7 @@ unset IO_PRESENT
unset IOFW
unset LOGGER_ARGS
unset LOGGER_BUF
unset MAV_TYPE
unset MIXER
unset MIXER_AUX
unset MIXER_FILE
@@ -1,7 +1,5 @@
Mixer for Tailsitter with x motor configuration and elevons
===========================================================
# @board px4_fmu-v2 exclude
# @board omnibus_f4sd exclude
This file defines a single mixer for tailsitter with motors in X configuration. All controls
are mixed 100%.
@@ -8,7 +8,6 @@ if [ $# -gt 0 ]; then
fi
exec find boards msg src platforms test \
-path msg/templates/urtps -prune -o \
-path platforms/nuttx/NuttX -prune -o \
-path platforms/qurt/dspal -prune -o \
-path src/drivers/uavcan/libuavcan -prune -o \
@@ -21,11 +20,8 @@ exec find boards msg src platforms test \
-path src/modules/ekf2/EKF -prune -o \
-path src/modules/gyro_fft/CMSIS_5 -prune -o \
-path src/modules/mavlink/mavlink -prune -o \
-path src/modules/micrortps_bridge/micro-CDR -prune -o \
-path src/modules/micrortps_bridge/microRTPS_client -prune -o \
-path test/mavsdk_tests/catch2 -prune -o \
-path src/lib/crypto/monocypher -prune -o \
-path src/lib/crypto/libtomcrypt -prune -o \
-path src/lib/crypto/libtommath -prune -o \
-path src/modules/microdds_client/Micro-XRCE-DDS-Client -prune -o \
-type f \( -name "*.c" -o -name "*.h" -o -name "*.cpp" -o -name "*.hpp" \) | grep $PATTERN
-15
View File
@@ -1,15 +0,0 @@
#!/usr/bin/env bash
set -e
SCRIPT_DIR=$0
if [[ ${SCRIPT_DIR:0:1} != '/' ]]; then
SCRIPT_DIR=$(dirname $(realpath -s "$PWD/$0"))
fi
PX4_DIR=$(cd "$(dirname $(dirname $SCRIPT_DIR))" && pwd)
if [ -d $PX4_DIR/build/*_rtps ]; then
cd $PX4_DIR/build/*_rtps/src/modules/micrortps_bridge/micrortps_agent/
cmake -Bbuild
cmake --build build -j$(nproc --all)
fi
+1 -1
View File
@@ -55,7 +55,7 @@ def perform_imu_checks(
# perform the vibration check
imu_status['imu_vibration_check'] = 'Pass'
for imu_vibr_metric in ['imu_coning', 'imu_hfgyro', 'imu_hfaccel']:
for imu_vibr_metric in ['imu_coning', 'imu_hfdang', 'imu_hfdvel']:
mean_metric = '{:s}_mean'.format(imu_vibr_metric)
peak_metric = '{:s}_peak'.format(imu_vibr_metric)
if imu_metrics[mean_metric] > check_levels['{:s}_warn'.format(mean_metric)] \
+10 -20
View File
@@ -144,27 +144,17 @@ def calculate_imu_metrics(ulog: ULog, multi_instance, in_air_no_ground_effects:
imu_metrics[result] = calculate_stat_from_signal(
estimator_status_data, 'estimator_status', signal, in_air_no_ground_effects, np.median)
# calculates peak and mean for IMU vibration checks
for imu_status_instance in range(4):
try:
vehicle_imu_status_data = ulog.get_dataset('vehicle_imu_status', imu_status_instance).data
if vehicle_imu_status_data['accel_device_id'][0] == estimator_status_data['accel_device_id'][0]:
for signal, result in [('delta_angle_coning_metric', 'imu_coning'),
('gyro_vibration_metric', 'imu_hfgyro'),
('accel_vibration_metric', 'imu_hfaccel')]:
peak = calculate_stat_from_signal(vehicle_imu_status_data, 'vehicle_imu_status', signal, in_air_no_ground_effects, np.amax)
if peak > 0.0:
imu_metrics['{:s}_peak'.format(result)] = peak
imu_metrics['{:s}_mean'.format(result)] = calculate_stat_from_signal(vehicle_imu_status_data, 'vehicle_imu_status', signal, in_air_no_ground_effects, np.mean)
except:
pass
for signal, result in [('vibe[0]', 'imu_coning'),
('vibe[1]', 'imu_hfdang'),
('vibe[2]', 'imu_hfdvel')]:
peak = calculate_stat_from_signal(
estimator_status_data, 'estimator_status', signal, in_air_no_ground_effects, np.amax)
if peak > 0.0:
imu_metrics['{:s}_peak'.format(result)] = peak
imu_metrics['{:s}_mean'.format(result)] = calculate_stat_from_signal(
estimator_status_data, 'estimator_status', signal,
in_air_no_ground_effects, np.mean)
# IMU bias checks
estimator_states_data = ulog.get_dataset('estimator_states', multi_instance).data
+28 -28
View File
@@ -48,7 +48,7 @@ for filename in os.listdir(metadata_directory):
# # print out the check levels
# print('\n'+'The following metadata loaded from '+filename+' were used'+'\n')
# val = population_data.get(filename, {}).get('imu_hfgyro_mean')
# val = population_data.get(filename, {}).get('imu_hfdang_mean')
# print(val)
# Open pdf file for plotting
@@ -90,10 +90,10 @@ population_results = {
'ofy_fail_pct_avg':[float('NaN'),'The mean percentage of innovation test fails for the Y axis optical flow sensor'],
'imu_coning_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU delta angle coning vibration level (mrad)'],
'imu_coning_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta angle coning vibration level (mrad)'],
'imu_hfgyro_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency gyro vibration level (rad/s)'],
'imu_hfgyro_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency gyro vibration level (rad/s)'],
'imu_hfaccel_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency accel vibration level (m/s/s)'],
'imu_hfaccel_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency accel vibration level (m/s/s)'],
'imu_hfdang_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency delta angle vibration level (mrad)'],
'imu_hfdang_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency delta angle vibration level (mrad)'],
'imu_hfdvel_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency delta velocity vibration level (m/s)'],
'imu_hfdvel_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency delta velocity vibration level (m/s)'],
'obs_ang_median_avg':[float('NaN'),'The mean of the median in-flight value of the output observer angular tracking error magnitude (mrad)'],
'obs_vel_median_avg':[float('NaN'),'The mean of the median in-flight value of the output observer velocity tracking error magnitude (m/s)'],
'obs_pos_median_avg':[float('NaN'),'The mean of the median in-flight value of the output observer position tracking error magnitude (m)'],
@@ -360,54 +360,54 @@ if (len(result1) > 0 and len(result2) > 0):
plt.close(8)
# IMU high frequency delta angle vibration levels
temp = np.asarray([population_data[k].get('imu_hfgyro_peak') for k in found_keys])
temp = np.asarray([population_data[k].get('imu_hfdang_peak') for k in found_keys])
result1 = 1000.0 * temp[np.isfinite(temp)]
temp = np.asarray([population_data[k].get('imu_hfgyro_mean') for k in found_keys])
temp = np.asarray([population_data[k].get('imu_hfdang_mean') for k in found_keys])
result2 = 1000.0 * temp[np.isfinite(temp)]
if (len(result1) > 0 and len(result2) > 0):
population_results['imu_hfgyro_max_avg'][0] = np.mean(result1)
population_results['imu_hfgyro_mean_avg'][0] = np.mean(result2)
population_results['imu_hfdang_max_avg'][0] = np.mean(result1)
population_results['imu_hfdang_mean_avg'][0] = np.mean(result2)
plt.figure(9,figsize=(20,13))
plt.subplot(2,1,1)
plt.hist(result1)
plt.title("Gaussian Histogram - IMU HF Gyroscope Vibration Peak")
plt.xlabel("imu_hfgyro_max (rad/s)")
plt.title("Gaussian Histogram - IMU HF Delta Angle Vibration Peak")
plt.xlabel("imu_hfdang_max (mrad)")
plt.ylabel("Frequency")
plt.subplot(2,1,2)
plt.hist(result2)
plt.title("Gaussian Histogram - IMU HF Gyroscope Vibration Mean")
plt.xlabel("imu_hfgyro_mean (rad/s)")
plt.title("Gaussian Histogram - IMU HF Delta Angle Vibration Mean")
plt.xlabel("imu_hfdang_mean (mrad)")
plt.ylabel("Frequency")
pp.savefig()
plt.close(9)
# IMU high frequency accel vibration levels
temp = np.asarray([population_data[k].get('imu_hfaccel_peak') for k in found_keys])
# IMU high frequency delta velocity vibration levels
temp = np.asarray([population_data[k].get('imu_hfdvel_peak') for k in found_keys])
result1 = temp[np.isfinite(temp)]
temp = np.asarray([population_data[k].get('imu_hfaccel_mean') for k in found_keys])
temp = np.asarray([population_data[k].get('imu_hfdvel_mean') for k in found_keys])
result2 = temp[np.isfinite(temp)]
if (len(result1) > 0 and len(result2) > 0):
population_results['imu_hfaccel_max_avg'][0] = np.mean(result1)
population_results['imu_hfaccel_mean_avg'][0] = np.mean(result2)
population_results['imu_hfdvel_max_avg'][0] = np.mean(result1)
population_results['imu_hfdvel_mean_avg'][0] = np.mean(result2)
plt.figure(10,figsize=(20,13))
plt.subplot(2,1,1)
plt.hist(result1)
plt.title("Gaussian Histogram - IMU HF Accelerometer Vibration Peak")
plt.xlabel("imu_hfaccel_max (m/s/s)")
plt.title("Gaussian Histogram - IMU HF Delta Velocity Vibration Peak")
plt.xlabel("imu_hfdvel_max (m/s)")
plt.ylabel("Frequency")
plt.subplot(2,1,2)
plt.hist(result2)
plt.title("Gaussian Histogram - IMU HF Accelerometer Vibration Mean")
plt.xlabel("imu_hfaccel_mean (m/s/s)")
plt.title("Gaussian Histogram - IMU HF Delta Velocity Vibration Mean")
plt.xlabel("imu_hfdvel_mean (m/s)")
plt.ylabel("Frequency")
pp.savefig()
@@ -535,12 +535,12 @@ single_log_results = {
'hgt_sensor_status':['Pass','Height sensor check summary. This sensor data can be sourced from either Baro, GPS, range fidner or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required'],
'hgt_test_max':[float('NaN'),'The maximum in-flight value of the height sensor innovation consistency test ratio.'],
'hgt_test_mean':[float('NaN'),'The mean in-flight value of the height sensor innovation consistency test ratio.'],
'imu_coning_mean':[float('NaN'),'Mean in-flight value of the IMU delta angle coning vibration metric (rad^2)'],
'imu_coning_peak':[float('NaN'),'Peak in-flight value of the IMU delta angle coning vibration metric (rad^2)'],
'imu_hfgyro_mean':[float('NaN'),'Mean in-flight value of the IMU gyro high frequency vibration metric (rad/s)'],
'imu_hfgyro_peak':[float('NaN'),'Peak in-flight value of the IMU gyro high frequency vibration metric (rad/s)'],
'imu_hfaccel_mean':[float('NaN'),'Mean in-flight value of the IMU accel high frequency vibration metric (m/s/s)'],
'imu_hfaccel_peak':[float('NaN'),'Peak in-flight value of the IMU accel high frequency vibration metric (m/s/s)'],
'imu_coning_mean':[float('NaN'),'Mean in-flight value of the IMU delta angle coning vibration metric (rad)'],
'imu_coning_peak':[float('NaN'),'Peak in-flight value of the IMU delta angle coning vibration metric (rad)'],
'imu_hfdang_mean':[float('NaN'),'Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)'],
'imu_hfdang_peak':[float('NaN'),'Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)'],
'imu_hfdvel_mean':[float('NaN'),'Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)'],
'imu_hfdvel_peak':[float('NaN'),'Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)'],
'imu_sensor_status':['Pass','IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required'],
'in_air_transition_time':[float('NaN'),'The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.'],
'mag_percentage_amber':[float('NaN'),'The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.'],
+4 -4
View File
@@ -21,10 +21,10 @@ hagl_amber_warn_pct,5.0
tas_amber_warn_pct,5.0
imu_coning_peak_warn,1.8E-5
imu_coning_mean_warn,3.6E-6
imu_hfgyro_peak_warn,12
imu_hfgyro_mean_warn,2.4
imu_hfaccel_peak_warn,360
imu_hfaccel_mean_warn,72
imu_hfdang_peak_warn,3.0E-3
imu_hfdang_mean_warn,6.0E-4
imu_hfdvel_peak_warn,9.0E-2
imu_hfdvel_mean_warn,1.8E-2
obs_ang_err_median_warn,8.0E-3
obs_vel_err_median_warn,0.05
obs_pos_err_median_warn,0.15
1 check_id threshold
21 tas_amber_warn_pct 5.0
22 imu_coning_peak_warn 1.8E-5
23 imu_coning_mean_warn 3.6E-6
24 imu_hfgyro_peak_warn imu_hfdang_peak_warn 12 3.0E-3
25 imu_hfgyro_mean_warn imu_hfdang_mean_warn 2.4 6.0E-4
26 imu_hfaccel_peak_warn imu_hfdvel_peak_warn 360 9.0E-2
27 imu_hfaccel_mean_warn imu_hfdvel_mean_warn 72 1.8E-2
28 obs_ang_err_median_warn 8.0E-3
29 obs_vel_err_median_warn 0.05
30 obs_pos_err_median_warn 0.15
+6 -6
View File
@@ -49,12 +49,12 @@ hagl_test_mean, The mean in-flight value of the height above ground sensor innov
ofx_fail_percentage, The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
ofy_fail_percentage, The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
filter_faults_max, Largest recorded value of the filter internal fault bitmask. Should always be zero.
imu_coning_peak, Peak in-flight value of the IMU delta angle coning vibration metric (rad^2)
imu_coning_mean, Mean in-flight value of the IMU delta angle coning vibration metric (rad^2)
imu_hfgyro_peak, Peak in-flight value of the IMU accel high frequency vibration metric (rad/s)
imu_hfgyro_mean, Mean in-flight value of the IMU accel high frequency vibration metric (rad/s)
imu_hfaccel_peak, Peak in-flight value of the IMU accel high frequency vibration metric (m/s/s)
imu_hfaccel_mean, Mean in-flight value of the IMU accel high frequency vibration metric (m/s/s)
imu_coning_peak, Peak in-flight value of the IMU delta angle coning vibration metric (rad)
imu_coning_mean, Mean in-flight value of the IMU delta angle coning vibration metric (rad)
imu_hfdang_peak, Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
imu_hfdang_mean, Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
imu_hfdvel_peak, Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
imu_hfdvel_mean, Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
output_obs_ang_err_median, Median in-flight value of the output observer angular error (rad)
output_obs_vel_err_median, Median in-flight value of the output observer velocity error (m/s)
output_obs_pos_err_median, Median in-flight value of the output observer position error (m)
1 check_id check_description
49 ofx_fail_percentage The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
50 ofy_fail_percentage The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
51 filter_faults_max Largest recorded value of the filter internal fault bitmask. Should always be zero.
52 imu_coning_peak Peak in-flight value of the IMU delta angle coning vibration metric (rad^2) Peak in-flight value of the IMU delta angle coning vibration metric (rad)
53 imu_coning_mean Mean in-flight value of the IMU delta angle coning vibration metric (rad^2) Mean in-flight value of the IMU delta angle coning vibration metric (rad)
54 imu_hfgyro_peak imu_hfdang_peak Peak in-flight value of the IMU accel high frequency vibration metric (rad/s) Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
55 imu_hfgyro_mean imu_hfdang_mean Mean in-flight value of the IMU accel high frequency vibration metric (rad/s) Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
56 imu_hfaccel_peak imu_hfdvel_peak Peak in-flight value of the IMU accel high frequency vibration metric (m/s/s) Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
57 imu_hfaccel_mean imu_hfdvel_mean Mean in-flight value of the IMU accel high frequency vibration metric (m/s/s) Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
58 output_obs_ang_err_median Median in-flight value of the output observer angular error (rad)
59 output_obs_vel_err_median Median in-flight value of the output observer velocity error (m/s)
60 output_obs_pos_err_median Median in-flight value of the output observer position error (m)
@@ -1,55 +0,0 @@
#!/usr/bin/env python
# -*- coding: utf-8 -*-
"""
Copyright (c) 2022 PX4 Development Team
Redistribution and use in source and binary forms, with or without
modification, are permitted provided that the following conditions
are met:
1. Redistributions of source code must retain the above copyright
notice, this list of conditions and the following disclaimer.
2. Redistributions in binary form must reproduce the above copyright
notice, this list of conditions and the following disclaimer in
the documentation and/or other materials provided with the
distribution.
3. Neither the name PX4 nor the names of its contributors may be
used to endorse or promote products derived from this software
without specific prior written permission.
THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
"AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
POSSIBILITY OF SUCH DAMAGE.
File: frag_fusion_symbolic.py
Author: Mathieu Bresciani <mathieu@auterion.com>
License: BSD 3-Clause
Description:
"""
from sympy import *
V = Symbol("V", real=True)
rho = Symbol("rho", real=True)
rho_n = Symbol("rho_n", real=True)
Mcoef = Symbol("Mcoef", real=True)
Bcoef = Symbol("Bcoef", real=True)
a = Symbol("a", real=True)
f1 = 0.5 * rho / Bcoef * V**2 + rho_n * Mcoef * V - a
print("If Bcoef > 0 and Mcoef > 0")
print("V =")
res_V = solve(f1, V)
res_V = res_V[0]
pprint(res_V)
print("a_pred =")
pprint(solve(f1, a))
@@ -1,202 +0,0 @@
#!/usr/bin/env python
# -*- coding: utf-8 -*-
"""
Copyright (c) 2022 PX4 Development Team
Redistribution and use in source and binary forms, with or without
modification, are permitted provided that the following conditions
are met:
1. Redistributions of source code must retain the above copyright
notice, this list of conditions and the following disclaimer.
2. Redistributions in binary form must reproduce the above copyright
notice, this list of conditions and the following disclaimer in
the documentation and/or other materials provided with the
distribution.
3. Neither the name PX4 nor the names of its contributors may be
used to endorse or promote products derived from this software
without specific prior written permission.
THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
"AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
POSSIBILITY OF SUCH DAMAGE.
File: drag_replay.py
Author: Mathieu Bresciani <mathieu@auterion.com>
License: BSD 3-Clause
Description:
Find the best ballistic and momentum drag coefficients for wind estimation
using EKF2 replay data.
NOTE: this script currently assumes no wind.
"""
import matplotlib.pylab as plt
from pyulog import ULog
from pyulog.px4 import PX4ULog
import numpy as np
import quaternion
from scipy import optimize
def getAllData(logfile):
log = ULog(logfile)
v_local = np.matrix([getData(log, 'vehicle_local_position', 'vx'),
getData(log, 'vehicle_local_position', 'vy'),
getData(log, 'vehicle_local_position', 'vz')])
t_v_local = ms2s(getData(log, 'vehicle_local_position', 'timestamp'))
accel = np.matrix([getData(log, 'sensor_combined', 'accelerometer_m_s2[0]'),
getData(log, 'sensor_combined', 'accelerometer_m_s2[1]'),
getData(log, 'sensor_combined', 'accelerometer_m_s2[2]')])
t_accel = ms2s(getData(log, 'sensor_combined', 'timestamp'))
q = np.matrix([getData(log, 'vehicle_attitude', 'q[0]'),
getData(log, 'vehicle_attitude', 'q[1]'),
getData(log, 'vehicle_attitude', 'q[2]'),
getData(log, 'vehicle_attitude', 'q[3]')])
t_q = ms2s(getData(log, 'vehicle_attitude', 'timestamp'))
dist_bottom = getData(log, 'vehicle_local_position', 'dist_bottom')
t_dist_bottom = ms2s(getData(log, 'vehicle_local_position', 'timestamp'))
(t_aligned, v_body_aligned, accel_aligned) = alignData(t_v_local, v_local, t_accel, accel, t_q, q, t_dist_bottom, dist_bottom)
t_aligned -= t_aligned[0]
return (t_aligned, v_body_aligned, accel_aligned)
def alignData(t_v, v_local, t_accel, accel, t_q, q, t_dist_bottom, dist_bottom):
len_accel = len(t_accel)
len_q = len(t_q)
len_db = len(t_dist_bottom)
i_a = 0
i_q = 0
i_db = 0
v_body_aligned = np.empty((3,0))
accel_aligned = np.empty((3,0))
t_aligned = []
for i_v in range(len(t_v)):
t = t_v[i_v]
accel_sum = np.zeros((3,1))
accel_count = 0
while t_accel[i_a] < t and i_a < len_accel-1:
accel_sum += accel[:, i_a] # Integrate accel samples between 2 velocity samples
accel_count += 1
i_a += 1
while t_q[i_q] < t and i_q < len_q-1:
i_q += 1
while t_dist_bottom[i_db] < t and i_db < len_db-1:
i_db += 1
# Only use in air data
if dist_bottom[i_db] < 1.0 or accel_count == 0:
continue
qk = np.quaternion(q[0, i_q],q[1, i_q],q[2, i_q],q[3, i_q])
q_vl = np.quaternion(0, v_local[0, i_v], v_local[1, i_v], v_local[2, i_v])
q_vb = qk.conjugate() * q_vl * qk # Get velocity in body frame
vb = quaternion.as_float_array(q_vb)[1:4]
v_body_aligned = np.append(v_body_aligned, [[vb[0]], [vb[1]], [vb[2]]], axis=1)
accel_aligned = np.append(accel_aligned, accel_sum / accel_count, axis=1)
t_aligned.append(t)
return (t_aligned, v_body_aligned, np.asarray(accel_aligned))
def getData(log, topic_name, variable_name, instance=0):
variable_data = np.array([])
for elem in log.data_list:
if elem.name == topic_name:
if instance == elem.multi_id:
variable_data = elem.data[variable_name]
break
return variable_data
def ms2s(time_ms):
return time_ms * 1e-6
def run(logfile):
(t, v_body, a_body) = getAllData(logfile)
rho = 1.15 # air densitiy
rho15 = 1.225 # air density at 15 degC
# x[0]: momentum drag, scales with v
# x[1]: inverse of ballistic coefficient (X body axis), scales with v^2
# x[2]: inverse of ballistic coefficient (Y body axis), scales with v^2
predict_acc_x = lambda x: -v_body[0] * x[0] - 0.5 * rho * v_body[0]**2 * np.sign(v_body[0]) * x[1]
predict_acc_y = lambda x: -v_body[1] * x[0] - 0.5 * rho * v_body[1]**2 * np.sign(v_body[1]) * x[2]
J = lambda x: np.sum(np.power(abs(a_body[0]-predict_acc_x(x)), 2.0) + np.power(abs(a_body[1]-predict_acc_y(x)), 2.0)) # cost function
x0 = [0.15, 1/100, 1/100] # initial conditions
res = optimize.minimize(J, x0, method='nelder-mead', bounds=[(0,1),(0,10),(0,10)], options={'disp': True})
# Convert results to parameters
innov_var = J(res.x) / (len(v_body[0]) + len(v_body[1]))
mcoef = res.x[0] / np.sqrt(rho / rho15)
bcoef_x = 0.0
bcoef_y = 0.0
if res.x[1] > 1/200:
bcoef_x = 1/res.x[1]
if res.x[2] > 1/200:
bcoef_y = 1/res.x[2]
print(f"param set EKF2_BCOEF_X {bcoef_x:.1f}")
print(f"param set EKF2_BCOEF_Y {bcoef_y:.1f}")
print(f"param set EKF2_MCOEF {mcoef:.2f}")
print(f"/!\EXPERIMENTAL param set EKF2_DRAG_NOISE {innov_var:.2f}")
# Plot data
plt.figure(1)
plt.suptitle(logfile.split('/')[-1])
ax1 = plt.subplot(2, 1, 1)
ax1.plot(t, v_body[0])
ax1.plot(t, v_body[1])
ax1.set_xlabel("time (s)")
ax1.set_ylabel("velocity (m/s)")
ax1.legend(["forward", "right"])
ax2 = plt.subplot(2, 1, 2, sharex=ax1)
ax2.set_title(f"BCoef_x = {bcoef_x:.1f}, BCoef_y = {bcoef_y:.1f}, MCoef = {mcoef:.4f}", loc="right")
ax2.plot(t, a_body[0])
ax2.plot(t, a_body[1])
ax2.plot(t, predict_acc_x(res.x))
ax2.plot(t, predict_acc_y(res.x))
ax2.set_xlabel("time (s)")
ax2.set_ylabel("acceleration (m/s^2)")
ax2.legend(["meas_forward", "meas_right", "predicted_forward", "predicted_right"])
plt.show()
if __name__ == '__main__':
import os
import argparse
# Get the path of this script (without file name)
script_path = os.path.split(os.path.realpath(__file__))[0]
# Parse arguments
parser = argparse.ArgumentParser(
description='Estimate mag biases from ULog file')
# Provide parameter file path and name
parser.add_argument('logfile', help='Full ulog file path, name and extension', type=str)
args = parser.parse_args()
logfile = os.path.abspath(args.logfile) # Convert to absolute path
run(logfile)
@@ -1,32 +0,0 @@
# PX4 Drag fusion parameter tuning algorithm
In PX4, drag fusion can be enabled in order to estimate the wind when flying a multirotor, assuming that the body vertical acceleration is produced by the rotors and that the lateral forces are produced by drag.
The model assumes a combination of:
1. momentum drag: created by the rotors changing the direction of the incoming air, linear to the relative airspeed. Parameter `EKF2_MCOEF`
2. bluff body drag: created by the wetted area of the aircraft, quadratic to the relative airspeed. Parameters `EKF2_BCOEF_X` and `EKF2_BCOEF_Y`
The python script was created to automate the tuning of the aforementioned parameters using flight test data.
## How to use this script
First, a flight log with enough information is required in order to accurately estimate the parameters.
The best way to do this is to fly the drone in altitude mode, accelerate to a moderate-high speed and let the drone slow-down by its own drag.
Repeat the same maneuver in all directions and several times to obtain a good dataset.
/!\ NOTE: the current state of this script assumes no wind. Some modifications are required to estimate both the wind and the parameters at the same time.
Then, install the required python packages:
```
pip install -r requirements.txt
```
and run the script and give it the log file as an argument:
```
python drag_replay.py <logfilename.ulg>
```
The estimated parameters are displayed in the console and the fit quality is shown in a plot:
```
param set EKF2_BCOEF_X 0.0
param set EKF2_BCOEF_Y 62.1
param set EKF2_MCOEF 0.16
/!\EXPERIMENTAL param set EKF2_DRAG_NOISE 0.31
```
![DeepinScreenshot_matplotlib_20220329100027](https://user-images.githubusercontent.com/14822839/160563024-efddd100-d7db-46f7-8676-cf4296e9f737.png)
@@ -1,6 +0,0 @@
matplotlib==3.5.1
numpy==1.22.2
pyulog==0.9.0
quaternion==3.5.2.post4
scipy==1.8.0
sympy==1.10.1
+11 -25
View File
@@ -250,32 +250,18 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
data_plot.save()
data_plot.close()
# Plot the EKF IMU vibration metrics
for imu_status_instance in range(4):
try:
vehicle_imu_status_data = ulog.get_dataset('vehicle_imu_status', imu_status_instance).data
imu_status_time = 1e-6 * vehicle_imu_status_data['timestamp']
if vehicle_imu_status_data['accel_device_id'][0] == estimator_status['accel_device_id'][0]:
scaled_estimator_status = {'delta_angle_coning_metric': 1000. * vehicle_imu_status_data['delta_angle_coning_metric'],
'gyro_vibration_metric': vehicle_imu_status_data['gyro_vibration_metric'],
'accel_vibration_metric': vehicle_imu_status_data['accel_vibration_metric']
}
data_plot = CheckFlagsPlot(
imu_status_time, scaled_estimator_status, [['delta_angle_coning_metric'], ['gyro_vibration_metric'], ['accel_vibration_metric']],
x_label='time (sec)',
y_labels=['Del Ang Coning (mrad^2)', 'HF Gyro (rad/s)', 'HF accel (m/s/s)'],
plot_title='IMU Vibration Metrics',
pdf_handle=pdf_pages, annotate=True)
data_plot.save()
data_plot.close()
except:
pass
scaled_estimator_status = {'vibe[0]': 1000. * estimator_status['vibe[0]'],
'vibe[1]': 1000. * estimator_status['vibe[1]'],
'vibe[2]': estimator_status['vibe[2]']
}
data_plot = CheckFlagsPlot(
status_time, scaled_estimator_status, [['vibe[0]'], ['vibe[1]'], ['vibe[2]']],
x_label='time (sec)', y_labels=['Del Ang Coning (mrad)', 'HF Del Ang (mrad)',
'HF Del Vel (m/s)'], plot_title='IMU Vibration Metrics',
pdf_handle=pdf_pages, annotate=True)
data_plot.save()
data_plot.close()
# Plot the EKF output observer tracking errors
scaled_innovations = {
-3
View File
@@ -93,7 +93,6 @@ pca9685_pwm_out,CONFIG_DRIVERS_PCA9685_PWM_OUT=y
power_monitor/ina226,CONFIG_DRIVERS_POWER_MONITOR_INA226=y
power_monitor/voxlpm,CONFIG_DRIVERS_POWER_MONITOR_VOXLPM=y
pps_capture,CONFIG_DRIVERS_PPS_CAPTURE=y
protocol_splitter,CONFIG_DRIVERS_PROTOCOL_SPLITTER=y
pwm_input,CONFIG_DRIVERS_PWM_INPUT=y
pwm_out_sim,CONFIG_DRIVERS_PWM_OUT_SIM=y
pwm_out,CONFIG_DRIVERS_PWM_OUT=y
@@ -138,8 +137,6 @@ mc_att_control,CONFIG_MODULES_MC_ATT_CONTROL=y
mc_hover_thrust_estimator,CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
mc_pos_control,CONFIG_MODULES_MC_POS_CONTROL=y
mc_rate_control,CONFIG_MODULES_MC_RATE_CONTROL=y
micrortps_bridge,CONFIG_MODULES_MICRORTPS_BRIDGE=y
microdds_client,CONFIG_MODULES_MICRODDS_CLIENT=y
navigator,CONFIG_MODULES_NAVIGATOR=y
px4iofirmware,CONFIG_MODULES_PX4IOFIRMWARE=y
rc_update,CONFIG_MODULES_RC_UPDATE=y

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