fixup! Update submodule nuttx

uavcan_v1: Add Publishers dir to includes
uavcan_v1: SocketCAN set 'can_fd' based on CONFIG
2026-05-26 19:30:04 +08:00 · 2022-03-18 10:56:44 -07:00 · 2022-03-18 09:03:48 -07:00 · 2022-03-18 09:03:06 -07:00 · 2022-03-18 09:02:00 -07:00 · 2022-03-17 17:01:54 -07:00
580 changed files with 11016 additions and 65525 deletions
@@ -28,7 +28,7 @@ pipeline {
          ]

          def base_builds = [
-            target: ["px4_sitl_default"],
+            target: ["px4_sitl_rtps"],
            image: docker_images.base,
            archive: false
          ]
@@ -58,7 +58,6 @@ 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",
@@ -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"'
 }
@@ -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,
@@ -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
@@ -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
@@ -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
@@ -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})
@@ -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
@@ -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

@@ -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.
 #
@@ -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.
 #
@@ -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
@@ -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

@@ -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%.
@@ -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
@@ -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)] \
@@ -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
@@ -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.'],
@@ -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
@@ -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)
@@ -1,55 +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
@@ -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 = {
@@ -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
@@ -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
@@ -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
@@ -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_airspeed start -X
-	then
-		# try another common address
-		sdp3x_airspeed 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 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
-
-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) }
-}
--- a/Show More
+++ b/Show More
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