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14 Commits

Author SHA1 Message Date
JacobCrabill 8e01fe661a fixup! Update submodule nuttx 2022-03-18 10:56:44 -07:00
JacobCrabill 64863fe54e uavcan_v1: Add Publishers dir to includes 2022-03-18 09:03:48 -07:00
JacobCrabill 73b1de85cb uavcan_v1: SocketCAN set 'can_fd' based on CONFIG 2022-03-18 09:03:06 -07:00
JacobCrabill fd3662097f fixup! Update submodule nuttx 2022-03-18 09:02:00 -07:00
JacobCrabill 76da12fce3 uavcan_v1: Immediate transmit() from Publishers
Add 'do_transmit()' to UavcanNode
Add 'transmit()' to Publisher base class to call do_transmit()
Call transmit() after canardTxPush from Publishers
2022-03-17 17:01:54 -07:00
JacobCrabill 9531900afa mro/ctrl-zero-h7-oem: Start adding socketcan support 2022-03-16 10:21:10 -07:00
JacobCrabill 25271a3f04 fixup! Update submodule nuttx 2022-03-16 10:20:29 -07:00
JacobCrabill 4048ac57bf fixup! Update submodule nuttx 2022-03-15 18:53:13 -07:00
JacobCrabill 399ab35a4f fixup! HACK: Disable SO_TIMESTAMP in uavcan_v1 temporarily while bringing up H7 SocketCAN driver 2022-03-15 18:52:00 -07:00
JacobCrabill f4f8eee02d cubeorange: Add TX_DEADLINE support 2022-03-15 18:24:03 -07:00
JacobCrabill dec15b4fa9 Update submodule nuttx 2022-03-15 18:23:22 -07:00
JacobCrabill 7db8d3ad78 HACK: Disable SO_TIMESTAMP in uavcan_v1 temporarily while bringing up H7 SocketCAN driver 2022-03-15 17:45:34 -07:00
JacobCrabill 7e34806046 mavlink: Replace CONFIG_NET with CONFIG_NET_UDP
Allows use of SocketCAN w/o also enabling UDP support in NuttX
2022-03-15 17:22:27 -07:00
JacobCrabill 9f18ef6688 Orange Cube: Add socketcan target 2022-03-15 17:11:42 -07:00
722 changed files with 12385 additions and 75228 deletions
+1 -4
View File
@@ -28,7 +28,7 @@ pipeline {
]
def base_builds = [
target: ["px4_sitl_default"],
target: ["px4_sitl_rtps"],
image: docker_images.base,
archive: false
]
@@ -52,14 +52,12 @@ pipeline {
"cuav_x7pro_default",
"cubepilot_cubeorange_default",
"cubepilot_cubeyellow_default",
"diatone_mamba-f405-mk2_default",
"freefly_can-rtk-gps_canbootloader",
"freefly_can-rtk-gps_default",
"holybro_can-gps-v1_canbootloader",
"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",
@@ -105,7 +103,6 @@ pipeline {
"px4_fmu-v6u_default",
"px4_fmu-v6x_default",
"px4_io-v2_default",
"sky-drones_smartap-airlink_default",
"spracing_h7extreme_default",
"uvify_core_default"
],
+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"'
}
-3
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,
@@ -30,7 +29,6 @@ jobs:
cuav_x7pro,
cubepilot_cubeorange,
cubepilot_cubeyellow,
diatone_mamba-f405-mk2,
freefly_can-rtk-gps,
holybro_can-gps-v1,
holybro_durandal-v1,
@@ -62,7 +60,6 @@ jobs:
px4_fmu-v5x,
px4_fmu-v6u,
px4_fmu-v6x,
sky-drones_smartap-airlink,
spracing_h7extreme,
uvify_core
]
+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_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
- name: Prepare ccache timestamp
id: ccache_cache_timestamp
+2 -5
View File
@@ -24,8 +24,8 @@
branch = master
[submodule "platforms/nuttx/NuttX/nuttx"]
path = platforms/nuttx/NuttX/nuttx
url = https://github.com/PX4/NuttX.git
branch = px4_firmware_nuttx-10.1.0+
url = https://github.com/JacobCrabill/incubator-nuttx.git
branch = dev-h7-socketcan
[submodule "platforms/nuttx/NuttX/apps"]
path = platforms/nuttx/NuttX/apps
url = https://github.com/PX4/NuttX-apps.git
@@ -64,6 +64,3 @@
path = src/lib/crypto/libtommath
url = https://github.com/PX4/libtommath.git
branch = px4
[submodule "src/modules/microdds_client/Micro-XRCE-DDS-Client"]
path = src/modules/microdds_client/Micro-XRCE-DDS-Client
url = https://github.com/eProsima/Micro-XRCE-DDS-Client.git
-10
View File
@@ -121,16 +121,6 @@ CONFIG:
buildType: MinSizeRel
settings:
CONFIG: ark_can-rtk-gps_canbootloader
ark_cannode_default:
short: ark_cannode_default
buildType: MinSizeRel
settings:
CONFIG: ark_cannode_default
ark_cannode_canbootloader:
short: ark_cannode_canbootloader
buildType: MinSizeRel
settings:
CONFIG: ark_cannode_canbootloader
atl_mantis-edu_default:
short: atl_mantis-edu
buildType: MinSizeRel
-7
View File
@@ -412,7 +412,6 @@ endif()
# subdirectories
#
add_library(parameters_interface INTERFACE)
add_library(kernel_parameters_interface INTERFACE)
include(px4_add_library)
add_subdirectory(src/lib EXCLUDE_FROM_ALL)
@@ -435,13 +434,7 @@ add_subdirectory(src/lib/metadata EXCLUDE_FROM_ALL)
# must be the last module before firmware
add_subdirectory(src/lib/parameters EXCLUDE_FROM_ALL)
if(${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})
+1 -1
View File
@@ -88,7 +88,7 @@ unset BOARD_RC_SENSORS
# Check for flow sensor
if param compare SENS_EN_PX4FLOW 1
then
px4flow start -X &
px4flow start -X
fi
uavcannode start
@@ -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
+7 -7
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
@@ -223,13 +224,6 @@ 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
@@ -259,6 +253,12 @@ 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
@@ -7,8 +7,8 @@
#
# @output MAIN1 motor 1
# @output MAIN2 motor 2
# @output MAIN3 motor 3
# @output MAIN4 motor 4
# @output MAIN3 motor 4
# @output MAIN4 motor 5
# @output MAIN5 elevon left
# @output MAIN6 elevon right
# @output MAIN7 canard surface
@@ -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-default 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-default 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.
#
+27 -40
View File
@@ -83,24 +83,18 @@ 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
# Possible external paw3902 optical flow sensor
if param greater -s SENS_EN_PAW3902 0
then
paw3902 -S start
fi
# vl53l1x i2c distance sensor
if param compare -s SENS_EN_VL53L1X 1
then
@@ -129,31 +123,13 @@ fi
# Sensirion SDP3X differential pressure sensor external I2C
if param compare -s SENS_EN_SDP3X 1
then
if ! sdp3x start -X
if ! sdp3x_airspeed start -X
then
# try another common address
sdp3x start -X -a 0x22
sdp3x_airspeed start -X -a 0x22
fi
fi
# TE MS4515 differential pressure sensor external I2C
if param compare -s SENS_EN_MS4515 1
then
ms4515 start -X
fi
# TE MS4525DO differential pressure sensor external I2C
if param compare -s SENS_EN_MS4525DO 1
then
ms4525do start -X
fi
# TE MS5525DSO differential pressure sensor external I2C
if param compare -s SENS_EN_MS5525DS 1
then
ms5525dso start -X
fi
# SHT3x temperature and hygrometer sensor, external I2C
if param compare -s SENS_EN_SHT3X 1
then
@@ -161,19 +137,24 @@ then
sht3x start -X -a 0x45
fi
# TE MS4525 differential pressure sensor external I2C
if param compare -s SENS_EN_MS4525 1
then
ms4525_airspeed start -X
fi
# TE MS5525 differential pressure sensor external I2C
if param compare -s SENS_EN_MS5525 1
then
ms5525_airspeed start -X
fi
# IR-LOCK sensor external I2C
if param compare -s SENS_EN_IRLOCK 1
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
@@ -198,3 +179,9 @@ then
# start last (wait for possible icm20948 passthrough mode)
ak09916 -X -q start
fi
###############################################################################
# End Optional drivers #
###############################################################################
sensors start
@@ -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 -14
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
@@ -405,17 +406,9 @@ else
battery_status start
fi
sensors start
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
@@ -466,6 +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)
#
@@ -493,6 +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
@@ -509,12 +515,6 @@ else
gyro_calibration start
fi
# Check for px4flow sensor
if param compare -s SENS_EN_PX4FLOW 1
then
px4flow start -X &
fi
#
# Optional board supplied extras: rc.board_extras
#
@@ -573,6 +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%.
+3 -3
View File
@@ -16,15 +16,15 @@ if board_adc start
then
fi
if sdp3x start -X
if sdp3x_airspeed start -X
then
fi
if ms5525dso start -X
if ms5525_airspeed start -X
then
fi
if ms4525do start -X
if ms4525_airspeed start -X
then
fi
@@ -27,5 +27,4 @@ exec find boards msg src platforms test \
-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
+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)
+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 = {
-1
View File
@@ -139,7 +139,6 @@ 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
@@ -1,6 +0,0 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT=""
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_NSH_BUILTIN_APPS=y
-37
View File
@@ -1,37 +0,0 @@
CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
CONFIG_BOARD_ARCHITECTURE="cortex-m4"
CONFIG_BOARD_ROMFSROOT="cannode"
CONFIG_BOARD_CONSTRAINED_FLASH=y
#CONFIG_BOARD_NO_HELP=y
CONFIG_BOARD_CONSTRAINED_MEMORY=y
CONFIG_BOARD_EXTERNAL_METADATA=y
CONFIG_COMMON_BAROMETERS=y
CONFIG_COMMON_DIFFERENTIAL_PRESSURE=y
CONFIG_COMMON_DISTANCE_SENSOR=y
CONFIG_COMMON_HYGROMETERS=y
CONFIG_COMMON_MAGNETOMETER=y
CONFIG_COMMON_LIGHT=y
CONFIG_DRIVERS_BATT_SMBUS=y
CONFIG_DRIVERS_BOOTLOADERS=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_IMU_ANALOG_DEVICES_ADIS16448=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM20948=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM42688P=y
CONFIG_DRIVERS_IRLOCK=y
CONFIG_DRIVERS_PWM_OUT=y
CONFIG_BOARD_UAVCAN_INTERFACES=1
CONFIG_DRIVERS_UAVCANNODE=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
#CONFIG_MODULES_SENSORS=y
CONFIG_NSH_BUILTIN_APPS=y
CONFIG_SYSTEMCMDS_ACTUATOR_TEST=y
CONFIG_SYSTEMCMDS_I2CDETECT=y
CONFIG_SYSTEMCMDS_LED_CONTROL=y
CONFIG_SYSTEMCMDS_MIXER=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_SYSTEMCMDS_TOP=y
CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
CONFIG_SYSTEMCMDS_PWM=y
CONFIG_SYSTEMCMDS_REBOOT=y
CONFIG_SYSTEMCMDS_WORK_QUEUE=y
-13
View File
@@ -1,13 +0,0 @@
{
"board_id": 83,
"magic": "PX4FWv1",
"description": "Firmware for the ARK CANnode board",
"image": "",
"build_time": 0,
"summary": "ARKCANNODE",
"version": "0.1",
"image_size": 0,
"image_maxsize": 2080768,
"git_identity": "",
"board_revision": 0
}
@@ -1,7 +0,0 @@
#!/bin/sh
#
# board specific defaults
#------------------------------------------------------------------------------
pwm_out start
control_allocator start
-118
View File
@@ -1,118 +0,0 @@
#!/bin/sh
#
# board sensors init
#------------------------------------------------------------------------------
icm42688p -R 0 -s start
if param compare -s SENS_EN_BATT 1
then
batt_smbus start -X
fi
# Lidar-Lite on I2C
if param compare -s SENS_EN_LL40LS 2
then
ll40ls start -X
fi
# mappydot lidar sensor
if param compare -s SENS_EN_MPDT 1
then
mappydot start -X
fi
# mb12xx sonar sensor
if param greater -s SENS_EN_MB12XX 0
then
mb12xx start -X
fi
# Lightware i2c lidar sensor
if param greater -s SENS_EN_SF1XX 0
then
lightware_laser_i2c start -X
fi
# vl53l1x i2c distance sensor
if param compare -s SENS_EN_VL53L1X 1
then
vl53l1x start -X
fi
# ADIS16448 spi external IMU
if param compare -s SENS_EN_ADIS164X 1
then
if param compare -s SENS_OR_ADIS164X 0
then
adis16448 -S start
fi
if param compare -s SENS_OR_ADIS164X 4
then
adis16448 -S start -R 4
fi
fi
# Eagle Tree airspeed sensor external I2C
if param compare -s SENS_EN_ETSASPD 1
then
ets_airspeed start -X
fi
# Sensirion SDP3X differential pressure sensor external I2C
if param compare -s SENS_EN_SDP3X 1
then
if ! sdp3x start -X
then
# try another common address
sdp3x start -X -a 0x22
fi
fi
# SHT3x temperature and hygrometer sensor, external I2C
if param compare -s SENS_EN_SHT3X 1
then
sht3x start -X
sht3x start -X -a 0x45
fi
# TE MS4525DO differential pressure sensor external I2C
if param compare -s SENS_EN_MS4525DO 1
then
ms4525do start -X
fi
# TE MS5525DSO differential pressure sensor external I2C
if param compare -s SENS_EN_MS5525DS 1
then
ms5525dso start -X
fi
# IR-LOCK sensor external I2C
if param compare -s SENS_EN_IRLOCK 1
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
gps start -d /dev/ttyS0 -p ubx
# probe for optional external I2C devices
icm20948_i2c_passthrough -X -q start
# compasses
hmc5883 -T -X -q start
ist8308 -X -q start
ist8310 -X -q start
lis2mdl -X -q start
lis3mdl -X -q start
qmc5883l -X -q start
rm3100 -X -q start
# start last (wait for possible icm20948 passthrough mode)
ak09916 -X -q start
@@ -1,61 +0,0 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/ark/cannode/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32"
CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=4096
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BINFMT_DISABLE=y
CONFIG_BOARD_LOOPSPERMSEC=16717
CONFIG_C99_BOOL8=y
CONFIG_CLOCK_MONOTONIC=y
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEFAULT_SMALL=y
CONFIG_DISABLE_MOUNTPOINT=y
CONFIG_DISABLE_MQUEUE=y
CONFIG_DISABLE_PTHREAD=y
CONFIG_EXPERIMENTAL=y
CONFIG_FDCLONE_DISABLE=y
CONFIG_FDCLONE_STDIO=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_IDLETHREAD_STACKSIZE=4096
CONFIG_LIBC_FLOATINGPOINT=y
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_STRERROR=y
CONFIG_LIB_BOARDCTL=y
CONFIG_FS_PROCFS_MAX_TASKS=0
CONFIG_MM_REGIONS=2
CONFIG_NAME_MAX=0
CONFIG_NUNGET_CHARS=0
CONFIG_PREALLOC_TIMERS=0
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAM_SIZE=262144
CONFIG_RAM_START=0x20010000
CONFIG_RAW_BINARY=y
CONFIG_SDCLONE_DISABLE=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_DISABLE_BUFFERING=y
CONFIG_STM32_FLASH_CONFIG_G=y
CONFIG_STM32_NOEXT_VECTORS=y
CONFIG_TASK_NAME_SIZE=0
CONFIG_USEC_PER_TICK=1000
CONFIG_USERMAIN_STACKSIZE=4096
@@ -1,149 +0,0 @@
/************************************************************************************
* configs/px4fmu/include/board.h
* include/arch/board/board.h
*
* Copyright (C) 2009 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* 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 NuttX 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.
*
************************************************************************************/
#include "board_dma_map.h"
#ifndef __ARCH_BOARD_BOARD_H
#define __ARCH_BOARD_BOARD_H
#include <nuttx/config.h>
#ifndef __ASSEMBLY__
# include <stdint.h>
#endif
#include <stm32.h>
/* HSI - 8 MHz RC factory-trimmed
* LSI - 32 KHz RC
* HSE - 8 MHz Crystal
* LSE - not installed
*/
#define STM32_BOARD_USEHSE 1
#define STM32_BOARD_XTAL 8000000
#define STM32_HSE_FREQUENCY STM32_BOARD_XTAL
#define STM32_HSI_FREQUENCY 16000000ul
#define STM32_LSI_FREQUENCY 32000
/* Main PLL Configuration */
#define STM32_PLLCFG_PLLM RCC_PLLCFG_PLLM(8)
#define STM32_PLLCFG_PLLN RCC_PLLCFG_PLLN(384)
#define STM32_PLLCFG_PLLP RCC_PLLCFG_PLLP_4
#define STM32_PLLCFG_PLLQ RCC_PLLCFG_PLLQ(8)
#define STM32_PLLCFG_PLLR RCC_PLLCFG_PLLR(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SM RCC_PLLI2SCFGR_PLLI2SM(16)
#define STM32_RCC_PLLI2SCFGR_PLLI2SN RCC_PLLI2SCFGR_PLLI2SN(192)
#define STM32_RCC_PLLI2SCFGR_PLLI2SQ RCC_PLLI2SCFGR_PLLI2SQ(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SR RCC_PLLI2SCFGR_PLLI2SR(2)
#define STM32_RCC_PLLI2SCFGR_PLLI2SSRC RCC_PLLI2SCFGR_PLLI2SSRC(0) /* HSE or HSI depending on PLLSRC of PLLCFGR*/
#define STM32_RCC_DCKCFGR2_CK48MSEL RCC_DCKCFGR2_CK48MSEL_PLL
#define STM32_RCC_DCKCFGR2_FMPI2C1SEL RCC_DCKCFGR2_FMPI2C1SEL_APB
#define STM32_RCC_DCKCFGR2_SDIOSEL RCC_DCKCFGR2_SDIOSEL_48MHZ
#define STM32_SYSCLK_FREQUENCY 96000000ul
/* AHB clock (HCLK) is SYSCLK (96MHz) */
#define STM32_RCC_CFGR_HPRE RCC_CFGR_HPRE_SYSCLK /* HCLK = SYSCLK / 1 */
#define STM32_HCLK_FREQUENCY STM32_SYSCLK_FREQUENCY
#define STM32_BOARD_HCLK STM32_HCLK_FREQUENCY /* Same as above, to satisfy compiler */
/* APB1 clock (PCLK1) is HCLK/2 (48MHz) */
#define STM32_RCC_CFGR_PPRE1 RCC_CFGR_PPRE1_HCLKd2 /* PCLK1 = HCLK / 2 */
#define STM32_PCLK1_FREQUENCY (STM32_HCLK_FREQUENCY/2)
/* Timers driven from APB1 will be twice PCLK1 (see page 112 of reference manual) */
#define STM32_APB1_TIM2_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM3_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM4_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM5_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM6_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM7_CLKIN (2*STM32_PCLK1_FREQUENCY)
#define STM32_APB1_TIM12_CLKIN (2*STM32_PCLK1_FREQUENCY)
/* APB2 clock (PCLK2) is HCLK (96MHz) */
#define STM32_RCC_CFGR_PPRE2 RCC_CFGR_PPRE2_HCLK /* PCLK2 = HCLK */
#define STM32_PCLK2_FREQUENCY (STM32_HCLK_FREQUENCY)
/* Timers driven from APB2 will be PCLK2 since no prescale division */
#define STM32_APB2_TIM1_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM8_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM9_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM10_CLKIN (STM32_PCLK2_FREQUENCY)
#define STM32_APB2_TIM11_CLKIN (STM32_PCLK2_FREQUENCY)
/* Timer Frequencies, if APBx is set to 1, frequency is same to APBx otherwise frequency is 2xAPBx. */
#define BOARD_TIM2_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM3_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM4_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM5_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM6_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM7_FREQUENCY (2 * STM32_PCLK1_FREQUENCY)
#define BOARD_TIM8_FREQUENCY (2 * STM32_PCLK2_FREQUENCY)
/* Alternate function pin selections ************************************************/
/* UARTs */
#define GPIO_USART1_RX GPIO_USART1_RX_2
#define GPIO_USART1_TX GPIO_USART1_TX_3
#define GPIO_USART2_RX GPIO_USART2_RX_1
#define GPIO_USART2_TX GPIO_USART2_TX_1
/* CAN */
#define GPIO_CAN1_RX GPIO_CAN1_RX_1
#define GPIO_CAN1_TX GPIO_CAN1_TX_1
/* SPI */
#define GPIO_SPI1_MISO GPIO_SPI1_MISO_1
#define GPIO_SPI1_MOSI GPIO_SPI1_MOSI_1
#define GPIO_SPI1_SCK GPIO_SPI1_SCK_1
#define GPIO_SPI2_MISO GPIO_SPI2_MISO_1 /* PB14 */
#define GPIO_SPI2_MOSI GPIO_SPI2_MOSI_1 /* PB15 */
#define GPIO_SPI2_SCK GPIO_SPI2_SCK_2 /* PB13 */
/* I2C */
#define GPIO_MCU_I2C1_SCL
#define GPIO_MCU_I2C1_SDA
#define GPIO_I2C1_SCL GPIO_I2C1_SCL_1
#define GPIO_I2C1_SDA GPIO_I2C1_SDA_2
#define GPIO_I2C1_SCL_GPIO (GPIO_OUTPUT | GPIO_OPENDRAIN |GPIO_SPEED_50MHz | GPIO_OUTPUT_SET | GPIO_PORTB | GPIO_PIN6)
#define GPIO_I2C1_SDA_GPIO (GPIO_OUTPUT | GPIO_OPENDRAIN |GPIO_SPEED_50MHz | GPIO_OUTPUT_SET | GPIO_PORTB | GPIO_PIN7)
#endif /* __ARCH_BOARD_BOARD_H */
@@ -1,44 +0,0 @@
/****************************************************************************
*
* Copyright (c) 2021 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
* 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.
*
****************************************************************************/
#pragma once
// DMA1 Channel/Stream Selections
//--------------------------------------------//---------------------------//----------------
#define DMACHAN_SPI2_RX DMAMAP_SPI2_RX // DMA1, Stream 3, Channel 0
#define DMACHAN_SPI2_TX DMAMAP_SPI2_TX // DMA1, Stream 4, Channel 0
// DMA2 Channel/Stream Selections
//--------------------------------------------//---------------------------//----------------
#define DMACHAN_SPI1_RX DMAMAP_SPI1_RX_2 // DMA2, Stream 2, Channel 3
#define DMACHAN_SPI1_TX DMAMAP_SPI1_TX_2 // DMA2, Stream 5, Channel 3
@@ -1,161 +0,0 @@
#
# This file is autogenerated: PLEASE DO NOT EDIT IT.
#
# You can use "make menuconfig" to make any modifications to the installed .config file.
# You can then do "make savedefconfig" to generate a new defconfig file that includes your
# modifications.
#
# CONFIG_DISABLE_OS_API is not set
# CONFIG_DISABLE_PSEUDOFS_OPERATIONS is not set
# CONFIG_NSH_DISABLEBG is not set
# CONFIG_NSH_DISABLESCRIPT is not set
# CONFIG_NSH_DISABLE_DF is not set
# CONFIG_NSH_DISABLE_EXEC is not set
# CONFIG_NSH_DISABLE_EXIT is not set
# CONFIG_NSH_DISABLE_GET is not set
# CONFIG_NSH_DISABLE_ITEF is not set
# CONFIG_NSH_DISABLE_LOOPS is not set
# CONFIG_NSH_DISABLE_MKFATFS is not set
# CONFIG_NSH_DISABLE_SEMICOLON is not set
# CONFIG_NSH_DISABLE_TIME is not set
# CONFIG_STM32_DMACAPABLE is not set
CONFIG_ARCH="arm"
CONFIG_ARCH_BOARD_CUSTOM=y
CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/ark/cannode/nuttx-config"
CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
CONFIG_ARCH_CHIP="stm32"
CONFIG_ARCH_CHIP_STM32=y
CONFIG_ARCH_CHIP_STM32F412CE=y
CONFIG_ARCH_INTERRUPTSTACK=512
CONFIG_ARCH_STACKDUMP=y
CONFIG_ARMV7M_MEMCPY=y
CONFIG_ARMV7M_USEBASEPRI=y
CONFIG_BOARDCTL_RESET=y
CONFIG_BOARD_LOOPSPERMSEC=16717
CONFIG_BOARD_RESET_ON_ASSERT=2
CONFIG_BUILTIN=y
CONFIG_C99_BOOL8=y
CONFIG_CLOCK_MONOTONIC=y
CONFIG_DEBUG_FULLOPT=y
CONFIG_DEBUG_HARDFAULT_ALERT=y
CONFIG_DEBUG_SYMBOLS=y
CONFIG_DEFAULT_SMALL=y
CONFIG_DEV_FIFO_SIZE=0
CONFIG_DEV_PIPE_MAXSIZE=1024
CONFIG_DEV_PIPE_SIZE=70
CONFIG_FDCLONE_STDIO=y
CONFIG_FS_BINFS=y
CONFIG_FS_CROMFS=y
CONFIG_FS_FAT=y
CONFIG_FS_FATTIME=y
CONFIG_FS_PROCFS=y
CONFIG_FS_PROCFS_INCLUDE_PROGMEM=y
CONFIG_FS_PROCFS_REGISTER=y
CONFIG_FS_ROMFS=y
CONFIG_GRAN=y
CONFIG_GRAN_INTR=y
CONFIG_HAVE_CXX=y
CONFIG_HAVE_CXXINITIALIZE=y
CONFIG_I2C=y
CONFIG_I2C_RESET=y
CONFIG_IDLETHREAD_STACKSIZE=750
CONFIG_LIBC_FLOATINGPOINT=y
CONFIG_LIBC_LONG_LONG=y
CONFIG_LIBC_STRERROR=y
CONFIG_MEMSET_64BIT=y
CONFIG_MEMSET_OPTSPEED=y
CONFIG_MM_REGIONS=2
CONFIG_MTD=y
CONFIG_MTD_BYTE_WRITE=y
CONFIG_MTD_PARTITION=y
CONFIG_MTD_RAMTRON=y
CONFIG_NAME_MAX=40
CONFIG_NSH_ARCHINIT=y
CONFIG_NSH_ARGCAT=y
CONFIG_NSH_BUILTIN_APPS=y
CONFIG_NSH_CMDPARMS=y
CONFIG_NSH_CROMFSETC=y
CONFIG_NSH_DISABLE_IFCONFIG=y
CONFIG_NSH_DISABLE_IFUPDOWN=y
CONFIG_NSH_DISABLE_TELNETD=y
CONFIG_NSH_LINELEN=128
CONFIG_NSH_MAXARGUMENTS=15
CONFIG_NSH_NESTDEPTH=8
CONFIG_NSH_QUOTE=y
CONFIG_NSH_ROMFSETC=y
CONFIG_NSH_ROMFSSECTSIZE=128
CONFIG_NSH_STRERROR=y
CONFIG_NSH_VARS=y
CONFIG_PIPES=y
CONFIG_PREALLOC_TIMERS=50
CONFIG_PRIORITY_INHERITANCE=y
CONFIG_PTHREAD_MUTEX_ROBUST=y
CONFIG_PTHREAD_STACK_MIN=512
CONFIG_RAMTRON_SETSPEED=y
CONFIG_RAM_SIZE=262144
CONFIG_RAM_START=0x20000000
CONFIG_RAW_BINARY=y
CONFIG_RTC_DATETIME=y
CONFIG_SCHED_ATEXIT=y
CONFIG_SCHED_HPWORK=y
CONFIG_SCHED_HPWORKPRIORITY=254
CONFIG_SCHED_HPWORKSTACKSIZE=3000
CONFIG_SCHED_INSTRUMENTATION=y
CONFIG_SCHED_INSTRUMENTATION_EXTERNAL=y
CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_WAITPID=y
CONFIG_SEM_NNESTPRIO=8
CONFIG_SEM_PREALLOCHOLDERS=0
CONFIG_SERIAL_TERMIOS=y
CONFIG_SIG_DEFAULT=y
CONFIG_SIG_SIGALRM_ACTION=y
CONFIG_SIG_SIGUSR1_ACTION=y
CONFIG_SIG_SIGUSR2_ACTION=y
CONFIG_SIG_SIGWORK=4
CONFIG_STACK_COLORATION=y
CONFIG_START_DAY=30
CONFIG_START_MONTH=11
CONFIG_STDIO_BUFFER_SIZE=32
CONFIG_STM32_ADC1=y
CONFIG_STM32_DISABLE_IDLE_SLEEP_DURING_DEBUG=y
CONFIG_STM32_DMA1=y
CONFIG_STM32_DMA2=y
CONFIG_STM32_FLASH_CONFIG_G=y
CONFIG_STM32_FLASH_PREFETCH=y
CONFIG_STM32_FLOWCONTROL_BROKEN=y
CONFIG_STM32_I2C1=y
CONFIG_STM32_JTAG_SW_ENABLE=y
CONFIG_STM32_PWR=y
CONFIG_STM32_RTC=y
CONFIG_STM32_RTC_HSECLOCK=y
CONFIG_STM32_RTC_MAGIC=0xfacefeee
CONFIG_STM32_RTC_MAGIC_REG=1
CONFIG_STM32_RTC_MAGIC_TIME_SET=0xfacefeef
CONFIG_STM32_SERIALBRK_BSDCOMPAT=y
CONFIG_STM32_SERIAL_DISABLE_REORDERING=y
CONFIG_STM32_SPI1=y
CONFIG_STM32_SPI1_DMA=y
CONFIG_STM32_SPI1_DMA_BUFFER=2048
CONFIG_STM32_SPI2=y
CONFIG_STM32_SPI2_DMA=y
CONFIG_STM32_SPI2_DMA_BUFFER=2048
CONFIG_STM32_SPI_DMA=y
CONFIG_STM32_USART1=y
CONFIG_STM32_USART2=y
CONFIG_STM32_USART_BREAKS=y
CONFIG_STM32_WWDG=y
CONFIG_SYSTEM_NSH=y
CONFIG_TASK_NAME_SIZE=24
CONFIG_USART1_BAUD=57600
CONFIG_USART1_RXBUFSIZE=600
CONFIG_USART1_TXBUFSIZE=1100
CONFIG_USART2_BAUD=57600
CONFIG_USART2_RXBUFSIZE=600
CONFIG_USART2_SERIAL_CONSOLE=y
CONFIG_USART2_TXBUFSIZE=1100
CONFIG_USEC_PER_TICK=1000
CONFIG_USERMAIN_STACKSIZE=2624
CONFIG_USER_ENTRYPOINT="nsh_main"
@@ -1,134 +0,0 @@
/****************************************************************************
* nuttx-config/scripts/canbootloader_script.ld
*
* Copyright (C) 2015 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* 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 NuttX 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.
*
****************************************************************************/
/* The STM32F412 has 512Kb of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x10000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08000000, LENGTH = 32K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
@@ -1,146 +0,0 @@
/****************************************************************************
* scripts/ld.script
*
* Copyright (C) 2011 Gregory Nutt. All rights reserved.
* Author: Gregory Nutt <gnutt@nuttx.org>
*
* 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 NuttX 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.
*
****************************************************************************/
/* The STM32F412CG has 1Mb of FLASH beginning at address 0x0800:0000 and
* 256Kb of SRAM. SRAM is split up into three blocks:
*
* 1) 112Kb of SRAM beginning at address 0x2000:0000
* 2) 16Kb of SRAM beginning at address 0x2001:c000
* 3) 64Kb of SRAM beginning at address 0x2002:0000
* 4) 64Kb of TCM SRAM beginning at address 0x1000:0000
*
* When booting from FLASH, FLASH memory is aliased to address 0x0000:0000
* where the code expects to begin execution by jumping to the entry point in
* the 0x0800:0000 address range.
*
* The first 0x10000 of flash is reserved for the bootloader.
*/
MEMORY
{
flash (rx) : ORIGIN = 0x08010000, LENGTH = 928K
sram (rwx) : ORIGIN = 0x20000000, LENGTH = 192K
}
OUTPUT_ARCH(arm)
ENTRY(__start) /* treat __start as the anchor for dead code stripping */
EXTERN(_vectors) /* force the vectors to be included in the output */
/*
* Ensure that abort() is present in the final object. The exception handling
* code pulled in by libgcc.a requires it (and that code cannot be easily avoided).
*/
EXTERN(abort)
EXTERN(_bootdelay_signature)
SECTIONS
{
.text : {
_stext = ABSOLUTE(.);
*(.vectors)
. = ALIGN(8);
/*
* This section positions the app_descriptor_t used
* by the make_can_boot_descriptor.py tool to set
* the application image's descriptor so that the
* uavcan bootloader has the ability to validate the
* image crc, size etc
*/
KEEP(*(.app_descriptor))
*(.text .text.*)
*(.fixup)
*(.gnu.warning)
*(.rodata .rodata.*)
*(.gnu.linkonce.t.*)
*(.got)
*(.gcc_except_table)
*(.gnu.linkonce.r.*)
_etext = ABSOLUTE(.);
} > flash
/*
* Init functions (static constructors and the like)
*/
.init_section : {
_sinit = ABSOLUTE(.);
KEEP(*(.init_array .init_array.*))
_einit = ABSOLUTE(.);
} > flash
.ARM.extab : {
*(.ARM.extab*)
} > flash
__exidx_start = ABSOLUTE(.);
.ARM.exidx : {
*(.ARM.exidx*)
} > flash
__exidx_end = ABSOLUTE(.);
_eronly = ABSOLUTE(.);
.data : {
_sdata = ABSOLUTE(.);
*(.data .data.*)
*(.gnu.linkonce.d.*)
CONSTRUCTORS
_edata = ABSOLUTE(.);
} > sram AT > flash
.bss : {
_sbss = ABSOLUTE(.);
*(.bss .bss.*)
*(.gnu.linkonce.b.*)
*(COMMON)
. = ALIGN(4);
_ebss = ABSOLUTE(.);
} > sram
/* Stabs debugging sections. */
.stab 0 : { *(.stab) }
.stabstr 0 : { *(.stabstr) }
.stab.excl 0 : { *(.stab.excl) }
.stab.exclstr 0 : { *(.stab.exclstr) }
.stab.index 0 : { *(.stab.index) }
.stab.indexstr 0 : { *(.stab.indexstr) }
.comment 0 : { *(.comment) }
.debug_abbrev 0 : { *(.debug_abbrev) }
.debug_info 0 : { *(.debug_info) }
.debug_line 0 : { *(.debug_line) }
.debug_pubnames 0 : { *(.debug_pubnames) }
.debug_aranges 0 : { *(.debug_aranges) }
}
-68
View File
@@ -1,68 +0,0 @@
############################################################################
#
# Copyright (c) 2020 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
# 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.
#
############################################################################
if("${PX4_BOARD_LABEL}" STREQUAL "canbootloader")
add_library(drivers_board
boot_config.h
boot.c
led.c
led.h
)
target_link_libraries(drivers_board
PRIVATE
nuttx_arch
nuttx_drivers
canbootloader
)
target_include_directories(drivers_board PRIVATE ${PX4_SOURCE_DIR}/platforms/nuttx/src/canbootloader)
else()
add_library(drivers_board
can.c
i2c.cpp
init.c
led.c
spi.cpp
timer_config.cpp
)
target_link_libraries(drivers_board
PRIVATE
arch_spi
drivers__led # drv_led_start
nuttx_arch
nuttx_drivers
px4_layer
)
endif()

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