sensors/vehicle_angular_velocity: add IMU_GYRO_RATEMAX constraints

sensors/vehicle_imu: don't bother checking IMU_GYRO_RATEMAX
boards: NuttX update all boards to preallocated sem holder list
2026-06-20 21:50:35 +08:00 · 2022-06-07 16:23:01 -04:00 · 2022-06-07 16:22:54 -04:00 · 2022-05-29 13:49:01 -04:00 · 2022-05-29 13:48:15 -04:00 · 2022-05-27 16:28:26 -04:00
495 changed files with 6380 additions and 9957 deletions
@@ -61,20 +61,18 @@ pipeline {
                     "holybro_kakutef7_default",
                     "holybro_kakuteh7_default",
                     "holybro_pix32v5_default",
+                     "matek_h743-slim",
                     "matek_gnss-m9n-f4_canbootloader",
                     "matek_gnss-m9n-f4_default",
-                     "matek_h743-mini_default",
-                     "matek_h743-slim_default",
-                     "matek_h743_default",
                     "modalai_fc-v1_default",
                     "modalai_fc-v1_rtps",
                     "modalai_fc-v2_default",
                     "mro_ctrl-zero-f7_default",
                     "mro_ctrl-zero-f7-oem_default",
-                     "mro_ctrl-zero-h7-oem_default",
-                     "mro_ctrl-zero-h7-oem_rtps",
                     "mro_ctrl-zero-h7_default",
                     "mro_ctrl-zero-h7_rtps",
+                     "mro_ctrl-zero-h7-oem_default",
+                     "mro_ctrl-zero-h7-oem_rtps",
                     "mro_pixracerpro_default",
                     "mro_pixracerpro_rtps",
                     "mro_x21-777_default",
@@ -89,26 +87,25 @@ pipeline {
                     "nxp_ucans32k146_canbootloader",
                     "nxp_ucans32k146_default",
                     "omnibus_f4sd_default",
+                     "raspberrypi_pico_default",
                     "px4_fmu-v2_default",
                     "px4_fmu-v2_fixedwing",
-                     "px4_fmu-v2_lto",
                     "px4_fmu-v2_multicopter",
                     "px4_fmu-v2_rover",
                     "px4_fmu-v3_default",
                     "px4_fmu-v4_default",
                     "px4_fmu-v4pro_default",
-                     "px4_fmu-v5_cyphal",
                     "px4_fmu-v5_debug",
                     "px4_fmu-v5_default",
-                     "px4_fmu-v5_lto",
                     "px4_fmu-v5_rtps",
                     "px4_fmu-v5_stackcheck",
                     "px4_fmu-v5_uavcanv0periph",
+                     "px4_fmu-v5_uavcanv1",
                     "px4_fmu-v5x_default",
+                     "px4_fmu-v6c_default",
                     "px4_fmu-v6u_default",
                     "px4_fmu-v6x_default",
                     "px4_io-v2_default",
-                     "raspberrypi_pico_default",
                     "sky-drones_smartap-airlink_default",
                     "spracing_h7extreme_default",
                     "uvify_core_default"
@@ -37,10 +37,8 @@ jobs:
          holybro_kakutef7,
          holybro_kakuteh7,
          holybro_pix32v5,
-          matek_gnss-m9n-f4,
-          matek_h743,
-          matek_h743-mini,
          matek_h743-slim,
+          matek_gnss-m9n-f4,
          modalai_fc-v1,
          modalai_fc-v2,
          mro_ctrl-zero-f7,
@@ -55,15 +53,16 @@ jobs:
          nxp_fmurt1062-v1,
          nxp_ucans32k146,
          omnibus_f4sd,
+          raspberrypi_pico,
          px4_fmu-v2,
          px4_fmu-v3,
          px4_fmu-v4,
          px4_fmu-v4pro,
          px4_fmu-v5,
          px4_fmu-v5x,
+          px4_fmu-v6c,
          px4_fmu-v6u,
          px4_fmu-v6x,
-          raspberrypi_pico,
          sky-drones_smartap-airlink,
          spracing_h7extreme,
          uvify_core
@@ -36,14 +36,14 @@
 [submodule "Tools/jsbsim_bridge"]
 	path = Tools/jsbsim_bridge
 	url = https://github.com/PX4/px4-jsbsim-bridge.git
-[submodule "src/drivers/cyphal/libcanard"]
-	path = src/drivers/cyphal/libcanard
-	url = https://github.com/opencyphal/libcanard.git
-[submodule "src/drivers/cyphal/public_regulated_data_types"]
-	path = src/drivers/cyphal/public_regulated_data_types
-	url = https://github.com/opencyphal/public_regulated_data_types.git
-[submodule "src/drivers/cyphal/legacy_data_types"]
-	path = src/drivers/cyphal/legacy_data_types
+[submodule "src/drivers/uavcan_v1/libcanard"]
+	path = src/drivers/uavcan_v1/libcanard
+	url = https://github.com/UAVCAN/libcanard.git
+[submodule "src/drivers/uavcan_v1/public_regulated_data_types"]
+	path = src/drivers/uavcan_v1/public_regulated_data_types
+	url = https://github.com/UAVCAN/public_regulated_data_types.git
+[submodule "src/drivers/uavcan_v1/legacy_data_types"]
+	path = src/drivers/uavcan_v1/legacy_data_types
 	url = https://github.com/PX4/public_regulated_data_types.git
 	branch = legacy
 [submodule "src/lib/crypto/monocypher"]
@@ -99,7 +99,7 @@
 #
 #=============================================================================

-cmake_minimum_required(VERSION 3.9 FATAL_ERROR)
+cmake_minimum_required(VERSION 3.2 FATAL_ERROR)

 set(PX4_SOURCE_DIR "${CMAKE_CURRENT_SOURCE_DIR}" CACHE FILEPATH "PX4 source directory" FORCE)
 set(PX4_BINARY_DIR "${CMAKE_CURRENT_BINARY_DIR}" CACHE FILEPATH "PX4 binary directory" FORCE)
@@ -234,14 +234,6 @@ message(STATUS "cmake build type: ${CMAKE_BUILD_TYPE}")
 #
 project(px4 CXX C ASM)

-# Check if LTO option and check if toolchain supports it
-if(LTO)
-    include(CheckIPOSupported)
-    check_ipo_supported()
-    message(AUTHOR_WARNING "LTO enabled: LTO is highly experimental and should not be used in production")
-    set(CMAKE_INTERPROCEDURAL_OPTIMIZATION TRUE)
-endif()
-
 set(package-contact "px4users@googlegroups.com")

 set(CMAKE_CXX_STANDARD 14)
@@ -51,13 +51,6 @@ menu "Toolchain"
        string "Architecture"
        default ""

-    config BOARD_LTO
-        bool "(EXPERIMENTAL) Link Time Optimization (LTO)"
-        default n
-        help
-            Enables LTO flag in linker
-            Note: Highly EXPERIMENTAL, furthermore make sure you're using a modern compiler GCC 9 or later
-
    config BOARD_FULL_OPTIMIZATION
        bool "Full optmization (O3)"
        default n
@@ -325,12 +325,13 @@ px4io_update: px4_io-v2_default cubepilot_io-v2_default
 	cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v5/extras/px4_io-v2_default.bin
 	cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v5x/extras/px4_io-v2_default.bin
 	cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v6x/extras/px4_io-v2_default.bin
+	cp build/px4_io-v2_default/px4_io-v2_default.bin boards/px4/fmu-v6c/extras/px4_io-v2_default.bin
 	# cubepilot_io-v2_default
 	cp build/cubepilot_io-v2_default/cubepilot_io-v2_default.bin boards/cubepilot/cubeorange/extras/cubepilot_io-v2_default.bin
 	cp build/cubepilot_io-v2_default/cubepilot_io-v2_default.bin boards/cubepilot/cubeyellow/extras/cubepilot_io-v2_default.bin
 	git status

-bootloaders_update: cuav_nora_bootloader cuav_x7pro_bootloader cubepilot_cubeorange_bootloader holybro_durandal-v1_bootloader matek_h743_bootloader matek_h743-mini_bootloader matek_h743-slim_bootloader modalai_fc-v2_bootloader mro_ctrl-zero-classic_bootloader mro_ctrl-zero-h7_bootloader mro_ctrl-zero-h7-oem_bootloader mro_pixracerpro_bootloader px4_fmu-v6u_bootloader px4_fmu-v6x_bootloader
+bootloaders_update: cuav_nora_bootloader cuav_x7pro_bootloader cubepilot_cubeorange_bootloader holybro_durandal-v1_bootloader holybro_kakuteh7_bootloader matek_h743-slim_bootloader modalai_fc-v2_bootloader mro_ctrl-zero-classic_bootloader mro_ctrl-zero-h7_bootloader mro_ctrl-zero-h7-oem_bootloader mro_pixracerpro_bootloader px4_fmu-v6c_bootloader px4_fmu-v6u_bootloader px4_fmu-v6x_bootloader
 	git status

 .PHONY: coverity_scan
@@ -25,8 +25,6 @@ param set-default FW_P_LIM_MIN -15
 param set-default FW_RR_FF 0.1
 param set-default FW_RR_P 0.3

-param set-default FW_SPOILERS_LND 0.4
-
 param set-default FW_THR_MAX 0.6
 param set-default FW_THR_MIN 0.05
 param set-default FW_THR_CRUISE 0.25
@@ -7,11 +7,6 @@

 . ${R}etc/init.d/rc.vtol_defaults

-# TODO: Enable motor failure detection when the
-# VTOL no longer reports 0A for all ESCs in SITL
-param set-default FD_ACT_EN 0
-param set-default FD_ACT_MOT_TOUT 500
-
 # param set-default SYS_CTRL_ALLOC 1
 param set-default CA_AIRFRAME 2

@@ -9,7 +9,7 @@

 param set-default MAV_TYPE 21

-param set-default SYS_CTRL_ALLOC 1
+# param set-default SYS_CTRL_ALLOC 1
 param set-default CA_AIRFRAME 3

 param set-default CA_ROTOR_COUNT 4
@@ -27,7 +27,9 @@ param set-default CA_ROTOR3_PY 0.1875
 param set-default CA_ROTOR3_KM -0.05

 param set-default CA_ROTOR0_TILT 1
+param set-default CA_ROTOR1_TILT 2
 param set-default CA_ROTOR2_TILT 3
+param set-default CA_ROTOR3_TILT 4
 param set-default CA_SV_CS0_TRQ_R -0.5
 param set-default CA_SV_CS0_TYPE 1
 param set-default CA_SV_CS1_TRQ_R 0.5
@@ -1,4 +1,6 @@

+mixer append /dev/pwm_output0 etc/mixers/mount_legs.aux.mix
+
 mavlink start -x -u 14558 -r 4000 -f -m onboard -o 14530 -p

 # shellcheck disable=SC2154
@@ -61,6 +61,8 @@ param set-default HIL_ACT_FUNC6 400

 param set SYS_HITL 1

+param set UAVCAN_ENABLE 0
+
 # disable some checks to allow to fly
 # - with usb
 param set-default CBRK_USB_CHK 197848
@@ -0,0 +1,40 @@
+#!/bin/sh
+#
+# @name Steadidrone QU4D
+#
+# @type Quadrotor Wide
+# @class Copter
+#
+# @output MAIN1 motor 1
+# @output MAIN2 motor 2
+# @output MAIN3 motor 3
+# @output MAIN4 motor 4
+# @output MAIN5 feed-through of RC AUX1 channel
+# @output MAIN6 feed-through of RC AUX2 channel
+#
+# @output AUX1 feed-through of RC AUX1 channel
+# @output AUX2 feed-through of RC AUX2 channel
+# @output AUX3 feed-through of RC AUX3 channel
+# @output AUX4 feed-through of RC FLAPS channel
+#
+# @maintainer Lorenz Meier <lorenz@px4.io>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.mc_defaults
+
+param set-default BAT1_N_CELLS 4
+
+param set-default MC_ROLL_P 7
+param set-default MC_ROLLRATE_P 0.13
+param set-default MC_ROLLRATE_I 0.05
+param set-default MC_ROLLRATE_D 0.004
+param set-default MC_PITCH_P 7
+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
@@ -15,6 +15,8 @@ set MIXER quad_x

 param set SYS_HITL 1

+param set UAVCAN_ENABLE 0
+
 param set-default CA_ROTOR_COUNT 4
 param set-default CA_ROTOR0_PX 0.15
 param set-default CA_ROTOR0_PY 0.15
@@ -94,6 +94,8 @@ param set-default HIL_ACT_FUNC8 203

 param set SYS_HITL 1

+param set UAVCAN_ENABLE 0
+
 # disable some checks to allow to fly
 # - with usb
 param set-default CBRK_USB_CHK 197848
@@ -0,0 +1,48 @@
+#!/bin/sh
+#
+# @name Steadidrone MAVRIK
+#
+# @type Octo Coax Wide
+# @class Copter
+#
+# @output MAIN1 motor 1
+# @output MAIN2 motor 2
+# @output MAIN3 motor 3
+# @output MAIN4 motor 4
+# @output MAIN5 motor 5
+# @output MAIN6 motor 6
+# @output MAIN7 motor 7
+# @output MAIN8 motor 8
+#
+# @maintainer Simon Wilks <simon@uaventure.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.mc_defaults
+
+
+param set-default MC_PITCH_P 4
+param set-default MC_PITCHRATE_P 0.24
+param set-default MC_PITCHRATE_I 0.09
+param set-default MC_PITCHRATE_D 0.013
+param set-default MC_PITCHRATE_MAX 180
+
+param set-default MC_ROLL_P 4
+param set-default MC_ROLLRATE_P 0.16
+param set-default MC_ROLLRATE_I 0.07
+param set-default MC_ROLLRATE_D 0.009
+param set-default MC_ROLLRATE_MAX 180
+
+param set-default MC_YAW_P 3
+
+param set-default MPC_HOLD_MAX_XY 0.25
+param set-default MPC_THR_MIN 0.15
+param set-default MPC_Z_VEL_MAX_DN 2
+
+param set-default BAT1_N_CELLS 4
+
+set MIXER octo_cox_w
+
+set PWM_OUT 12345678
@@ -0,0 +1,37 @@
+#!/bin/sh
+#
+# @name CruiseAder Claire
+#
+# @type VTOL Tiltrotor
+# @class VTOL
+#
+# @maintainer Samay Siga <samay_s@icloud.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${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
+param set-default PWM_AUX_RATE 50
+
+param set-default PWM_MAIN_MAX 2000
+
+param set-default VT_MOT_ID 1234
+param set-default VT_FW_MOT_OFFID 13
+param set-default VT_IDLE_PWM_MC 1080
+param set-default VT_TILT_FW 0.9
+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 MIXER claire
+set MIXER_AUX claire
+
+set PWM_OUT 1234
@@ -69,9 +69,4 @@ param set-default VT_TYPE 1

 set MIXER vtol_convergence

-if ! ver hwcmp MATEK_H743
-then
-	set PWM_OUT 1234
-else
-	set PWM_OUT 3456
-fi	
+set PWM_OUT 1234
@@ -131,6 +131,7 @@ param set-default VT_F_TRANS_DUR 1
 param set-default VT_IDLE_PWM_MC 1025
 param set-default VT_B_REV_OUT 0.5
 param set-default VT_B_TRANS_THR 0.7
+param set-default VT_FW_PERM_STAB 1
 param set-default VT_TRANS_TIMEOUT 22
 param set-default VT_F_TRANS_RAMP 4

@@ -0,0 +1,45 @@
+#!/bin/sh
+#
+# @name IO Camflyer
+#
+# @type Flying Wing
+# @class Plane
+#
+# @output MAIN1 left aileron
+# @output MAIN2 right aileron
+# @output MAIN4 throttle
+#
+# @output AUX1 feed-through of RC AUX1 channel
+# @output AUX2 feed-through of RC AUX2 channel
+# @output AUX3 feed-through of RC AUX3 channel
+#
+# @maintainer Simon Wilks <simon@uaventure.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.fw_defaults
+
+param set-default FW_AIRSPD_MAX 15
+param set-default FW_AIRSPD_TRIM 13
+param set-default FW_R_TC 0.3
+param set-default FW_P_TC 0.3
+param set-default FW_L1_DAMPING 0.74
+param set-default FW_L1_PERIOD 16
+param set-default FW_LND_ANG 15
+param set-default FW_LND_FLALT 5
+param set-default FW_LND_HVIRT 13
+param set-default FW_LND_TLALT 5
+param set-default FW_THR_LND_MAX 0
+param set-default FW_PR_FF 0.35
+param set-default FW_RR_FF 0.6
+param set-default FW_RR_P 0.04
+
+param set-default PWM_MAIN_DISARM 1000
+
+
+set MIXER fw_generic_wing
+
+# Provide ESC a constant 1000 us pulse while disarmed
+set PWM_OUT 4
@@ -0,0 +1,29 @@
+#!/bin/sh
+#
+# @name FX-79 Buffalo Flying Wing
+#
+# @type Flying Wing
+# @class Plane
+#
+# @output MAIN1 right aileron
+# @output MAIN2 left aileron
+# @output MAIN4 throttle
+#
+# @output AUX1 feed-through of RC AUX1 channel
+# @output AUX2 feed-through of RC AUX2 channel
+# @output AUX3 feed-through of RC AUX3 channel
+#
+# @maintainer Simon Wilks <simon@uaventure.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.fw_defaults
+
+param set-default FW_AIRSPD_MAX 30
+param set-default FW_AIRSPD_MIN 13
+
+param set-default NAV_LOITER_RAD 150
+
+set MIXER fw_generic_wing
@@ -0,0 +1,23 @@
+#!/bin/sh
+#
+# @name Viper
+#
+# @type Flying Wing
+# @class Plane
+# @output MAIN1 left aileron
+# @output MAIN2 right aileron
+# @output MAIN4 throttle
+#
+# @output AUX1 feed-through of RC AUX1 channel
+# @output AUX2 feed-through of RC AUX2 channel
+# @output AUX3 feed-through of RC AUX3 channel
+#
+# @maintainer Simon Wilks <simon@uaventure.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.fw_defaults
+
+set MIXER Viper
@@ -0,0 +1,53 @@
+#!/bin/sh
+#
+# @name Modified Parrot Disco
+#
+# @url
+#
+# @type Flying Wing
+# @class Plane
+#
+# @output MAIN1 left aileron
+# @output MAIN2 right aileron
+# @output MAIN4 throttle
+#
+# @output AUX1 feed-through of RC AUX1 channel
+# @output AUX2 feed-through of RC AUX2 channel
+# @output AUX3 feed-through of RC AUX3 channel
+#
+# @maintainer Jan Liphardt <JTLiphardt@gmail.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.fw_defaults
+
+####################################
+# Airspeed
+####################################
+param set-default FW_AIRSPD_MAX  27 # = 52 knots
+
+####################################
+# Pitch
+####################################
+
+# Pitch rate feed forward (def = 0.5 %/rad/sec)
+param set-default FW_PR_FF 0.35
+
+####################################
+# Roll
+####################################
+
+# Basic limits (def = 50 deg)
+param set-default FW_R_LIM 40
+
+# Roll rate upper limit (def = 70 deg/s)
+param set-default FW_R_RMAX 50
+
+param set-default PWM_MAIN_DISARM 1000
+
+set MIXER fw_generic_wing.main.mix
+
+# Provide ESC a constant 1000 us pulse
+set PWM_OUT 4
@@ -0,0 +1,21 @@
+#!/bin/sh
+#
+# @name DJI F330 w/ DJI ESCs
+#
+# @type Quadrotor x
+# @class Copter
+#
+# @maintainer Lorenz Meier <lorenz@px4.io>
+# @board px4_fmu-v2 exclude
+#
+
+. ${R}etc/init.d/rc.mc_defaults
+
+param set-default MC_ROLL_P 7
+param set-default MC_ROLLRATE_I 0.05
+param set-default MC_PITCH_P 7
+param set-default MC_PITCHRATE_I 0.05
+
+
+# DJI ESCs do not support calibration and need a higher min
+param set-default PWM_MAIN_MIN 1230
@@ -0,0 +1,20 @@
+#!/bin/sh
+#
+# @name DJI F450 w/ DJI ESCs
+#
+# @type Quadrotor x
+# @class Copter
+#
+# @maintainer Lorenz Meier <lorenz@px4.io>
+#
+
+. ${R}etc/init.d/rc.mc_defaults
+
+param set-default MC_ROLL_P 7
+param set-default MC_ROLLRATE_I 0.05
+param set-default MC_PITCH_P 7
+param set-default MC_PITCHRATE_I 0.05
+param set-default MC_YAWRATE_P 0.3
+
+# DJI ESCs do not support calibration and need a higher min
+param set-default PWM_MAIN_MIN 1230
@@ -0,0 +1,27 @@
+#!/bin/sh
+#
+# @name DJI Matrice 100
+#
+# @type Quadrotor x
+# @class Copter
+#
+# @maintainer James Goppert <james.goppert@gmail.com>
+#
+# @board px4_fmu-v2 exclude
+# @board bitcraze_crazyflie exclude
+#
+
+. ${R}etc/init.d/rc.mc_defaults
+
+param set-default BAT1_N_CELLS 6
+
+param set-default MC_ROLLRATE_P 0.05
+param set-default MC_ROLLRATE_I 0.05
+param set-default MC_ROLLRATE_D 0.001
+param set-default MC_PITCHRATE_P 0.05
+param set-default MC_PITCHRATE_I 0.05
+param set-default MC_PITCHRATE_D 0.001
+
+param set-default MC_YAWRATE_I 0
+
+param set-default PWM_MAIN_MIN 1200
@@ -52,16 +52,22 @@ px4_add_romfs_files(

 	# [3000, 3999] Flying wing"
 	3000_generic_wing
+	3030_io_camflyer
 	3031_phantom
 	3032_skywalker_x5
 	3033_wingwing
+	3034_fx79
+	3035_viper
 	3036_pigeon
+	3037_parrot_disco_mod
 	3100_tbs_caipirinha

 	# [4000, 4999] Quadrotor x"
 	4001_quad_x
 	4003_qavr5
 	4009_qav250
+	4010_dji_f330
+	4011_dji_f450
 	4014_s500
 	4015_holybro_s500
 	4016_holybro_px4vision
@@ -75,6 +81,7 @@ px4_add_romfs_files(
 	4051_s250aq
 	4052_holybro_qav250
 	4053_holybro_kopis2
+	4060_dji_matrice_100
 	4061_atl_mantis_edu
 	4071_ifo
 	4072_draco
@@ -105,6 +112,7 @@ px4_add_romfs_files(
 	# [10000, 10999] Quadrotor Wide arm / H frame"
 	10015_tbs_discovery
 	10016_3dr_iris
+	10017_steadidrone_qu4d
 	10018_tbs_endurance

 	# [11000, 11999] Hexa Cox
@@ -112,6 +120,7 @@ px4_add_romfs_files(

 	# [12000, 12999] Octo Cox
 	12001_octo_cox
+	12002_steadidrone_mavrik

 	# [13000, 13999] VTOL
 	13000_generic_vtol_standard
@@ -124,6 +133,7 @@ px4_add_romfs_files(
 	13007_vtol_AAVVT_quad
 	13008_QuadRanger
 	13009_vtol_spt_ranger
+	13010_claire
 	13012_convergence
 	13013_deltaquad
 	13014_vtol_babyshark
@@ -181,30 +181,6 @@ then
 	pcf8583 start -X -a 0x51
 fi

-# INA226 digital power monitor
-if param compare SENS_EN_INA226 1
-then
-	ina226 -X start
-fi
-
-# INA228 digital power monitor
-if param compare SENS_EN_INA228 1
-then
-	ina228 -X start
-fi
-
-# INA231 digital power monitor
-if param compare SENS_EN_INA231 1
-then
-	ina231 -X start
-fi
-
-# INA238 digital power monitor
-if param compare SENS_EN_INA238 1
-then
-	ina238 -X start
-fi
-
 # probe for optional external I2C devices
 if param compare SENS_EXT_I2C_PRB 1
 then
@@ -298,9 +298,9 @@ else
 			tune_control play error
 		fi
 	else
-		if param greater -s CYPHAL_ENABLE 0
+		if param greater -s UAVCAN_V1_ENABLE 0
 		then
-			cyphal start
+			uavcan_v1 start
 		fi
 	fi

@@ -21,16 +21,14 @@ O:      10000  10000      0 -10000  10000
 S: 0 3      0  20000 -10000 -10000  10000

 # mixer for the left aileron
-M: 2
+M: 1
 O:      10000  10000   0 -10000  10000
 S: 0 0  -10000  -10000    0 -10000  10000
-S: 0 5   10000   10000    0 -10000  10000

 # mixer for the right aileron
-M: 2
+M: 1
 O:      10000  10000   0 -10000  10000
 S: 0 0  10000  10000    0 -10000  10000
-S: 0 5  10000  10000    0 -10000  10000

 # mixer for the elevator
 M: 1
@@ -8,22 +8,22 @@ R: 4x
 # tilt servo motor 1
 M: 1
 O:      10000  10000      0 -10000  10000
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000

 # tilt servo motor 2
 M: 1
 O:      10000  10000      0 -10000  10000
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000

 # tilt servo motor 3
 M: 1
 O:      10000  10000      0 -10000  10000
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000

 # tilt servo motor 4
 M: 1
 O:      10000  10000      0 -10000  10000
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000

 # mixer for the left aileron
 M: 1
@@ -10,7 +10,7 @@ to output 4 and the wheel to output 5.
 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
 (roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up correctly mechanically;
@@ -20,11 +20,11 @@ endpoints to suit.

 M: 2
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5  10000  10000      0 -10000  10000
+S: 0 6  10000  10000      0 -10000  10000

 M: 2
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5 -10000 -10000      0 -10000  10000
+S: 0 6 -10000 -10000      0 -10000  10000

 Elevator mixer
 ------------
@@ -11,7 +11,7 @@ to output 4, the wheel to output 5 and the flaps to output 6 and 7.
 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
 (roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up correctly mechanically;
@@ -21,11 +21,11 @@ endpoints to suit.

 M: 2
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5  10000  10000      0 -10000  10000
+S: 0 6  10000  10000      0 -10000  10000

 M: 2
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5 -10000 -10000      0 -10000  10000
+S: 0 6 -10000 -10000      0 -10000  10000

 V-tail mixers
 -------------
@@ -9,20 +9,20 @@ output 0 and 1, the tail servos to output 2 and 3, the throttle
 to output 4, the wheel to output 5 and the flaps to output 6 and 7.

 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
-(roll), 1 (pitch), 2 (yaw), 3 (thrust) 4 (flaps), 5 (spoiler).
+(roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up mechanically reversed.

 M: 2
 S: 0 0 -10000 -10000      0 -10000  10000
-S: 0 5  10000  10000      0 -10000  10000
+S: 0 6  10000  10000      0 -10000  10000

 M: 2
 S: 0 0 -10000 -10000      0 -10000  10000
-S: 0 5 -10000 -10000      0 -10000  10000
+S: 0 6 -10000 -10000      0 -10000  10000

 V-tail mixers
 -------------
@@ -40,6 +40,8 @@ px4_add_romfs_files(
 	babyshark.main.mix
 	blade130.main.mix
 	CCPM.main.mix
+	claire.aux.mix
+	claire.main.mix
 	cloudship.main.mix
 	coax.main.mix
 	delta.main.mix
@@ -81,6 +83,7 @@ px4_add_romfs_files(
 	tri_y_yaw-.main.mix
 	uuv_x.main.mix
 	vectored6dof.main.mix
+	Viper.main.mix
 	vtol_AAERT.aux.mix
 	vtol_AAVVT.aux.mix
 	vtol_TTTTAAER.aux.mix
@@ -0,0 +1,66 @@
+Viper Delta-wing mixer
+=================================
+# @board px4_fmu-v2 exclude
+
+Designed for Viper.
+
+TODO (sjwilks): Add mixers for flaps.
+
+This file defines mixers suitable for controlling a delta wing aircraft using
+PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU
+servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is
+assumed to be unused.
+
+Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
+(roll), 1 (pitch) and 3 (thrust).
+
+See the README for more information on the scaler format.
+
+Elevon mixers
+-------------
+Three scalers total (output, roll, pitch).
+
+On the assumption that the two elevon servos are physically reversed, the pitch
+input is inverted between the two servos.
+
+The scaling factor for roll inputs is adjusted to implement differential travel
+for the elevons.
+
+M: 2
+S: 0 0   7500   7500      0 -10000  10000
+S: 0 1   8000   8000      0 -10000  10000
+
+M: 2
+S: 0 0   7500   7500      0 -10000  10000
+S: 0 1  -8000  -8000      0 -10000  10000
+
+Output 2
+--------
+This mixer is empty.
+
+Z:
+
+Motor speed mixer
+-----------------
+Two scalers total (output, thrust).
+
+This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
+range.  Inputs below zero are treated as zero.
+
+M: 1
+S: 0 3      0  20000 -10000 -10000  10000
+
+Inputs to the mixer come from channel group 2 (payload), channels 0
+(bay servo 1), 1 (bay servo 2) and 3 (drop release).
+-----------------------------------------------------
+
+M: 1
+S: 2 0  10000  10000      0 -10000  10000
+
+M: 1
+S: 2 1  10000  10000      0 -10000  10000
+
+M: 1
+S: 2 2  -8000  -8000      0 -10000  10000
+
+
@@ -0,0 +1,28 @@
+# mixer for the CruiseAder Claire tilt mechansim servo and elevons
+
+=======================================================================
+
+
+Tilt mechanism servo mixer
+
+---------------------------
+
+M: 1
+
+
+S: 1 4  10000  10000      0 -10000  10000
+
+
+
+Elevon mixers
+
+-------------
+
+M: 2
+
+S: 1 0   7500   7500      0 -10000  10000
+S: 1 1   7500   7500      0 -10000  10000
+
+M: 2
+S: 1 0    7500    7500    0 -10000  10000
+S: 1 1   -7500   -7500    0 -10000  10000
@@ -0,0 +1,8 @@
+# CruiseAder Claire Main Multirotor mixer for PX4FMU
+# @board px4_fmu-v2 exclude
+
+#
+
+#===========================
+
+R: 4x
@@ -6,7 +6,7 @@
 Tilt mechanism servo mixer
 ---------------------------
 M: 1
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000

 Elevon mixers
 -------------
@@ -5,14 +5,14 @@ Aileron/v-tail/throttle VTOL mixer for PX4FMU

 This file defines mixers suitable for controlling a fixed wing aircraft with
 aileron, v-tail (rudder, elevator) and throttle using PX4FMU.
-The configuration assumes the aileron servos are connected to PX4FMU
+The configuration assumes the aileron servos are connected to PX4FMU 
 AUX servo output 0 and 1, the tail servos to output 2 and 3, the throttle
 to output 4.

 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
 (roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up correctly mechanically;
@@ -22,11 +22,11 @@ endpoints to suit.

 M: 2
 S: 1 0 -10000 -10000      0 -10000  10000
-S: 1 5  10000  10000      0 -10000  10000
+S: 1 6  10000  10000      0 -10000  10000

 M: 2
 S: 1 0 -10000 -10000      0 -10000  10000
-S: 1 5 -10000 -10000      0 -10000  10000
+S: 1 6 -10000 -10000      0 -10000  10000


 V-tail mixers
@@ -6,19 +6,19 @@
 ---------------------------
 # front left up:2000 down:1000
 M: 1
-S: 1 8      0 -20000  10000 -10000  10000
+S: 1 4      0 -20000  10000 -10000  10000

 # front right up:1000 down:2000
 M: 1
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000

 # rear left up:2000 down:1000
 M: 1
-S: 1 8      0 -20000  10000 -10000  10000
+S: 1 4      0 -20000  10000 -10000  10000

 # rear right up:1000 down:2000
 M: 1
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000


 # Aileron mixer
@@ -10,12 +10,12 @@ Tilt mechanism servo mixer
 ---------------------------
 #RIGHT up:2000 down:1000
 M: 2
-S: 1 8      0 -20000  10000 -10000  10000
+S: 1 4      0 -20000  10000 -10000  10000
 S: 0 2   8000   8000      0 -10000  10000

 #LEFT up:1000 down:2000
 M: 2
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000
 S: 0 2   8000   8000      0 -10000  10000

 Elevon mixers
@@ -10,7 +10,7 @@ to output 4 and the wheel to output 5.
 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
 (roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up correctly mechanically;
@@ -21,12 +21,12 @@ endpoints to suit.
 M: 2
 O:      10000  10000      0 -10000  10000
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5  10000  10000      0 -10000  10000
+S: 0 6  10000  10000      0 -10000  10000

 M: 2
 O:      10000  10000      0 -10000  10000
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5 -10000 -10000      0 -10000  10000
+S: 0 6 -10000 -10000      0 -10000  10000

 Elevator mixer
 ------------
@@ -9,9 +9,9 @@ output 0 and 1, the tail servos to output 2 and 3, the throttle
 to output 4, the wheel to output 5 and the flaps to output 6 and 7.

 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
-(roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 5 (spoiler).
+(roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up correctly mechanically;
@@ -22,12 +22,12 @@ endpoints to suit.
 M: 2
 O:      10000  10000      0 -10000  10000
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5  10000  10000      0 -10000  10000
+S: 0 6  10000  10000      0 -10000  10000

 M: 2
 O:      10000  10000      0 -10000  10000
 S: 0 0  10000  10000      0 -10000  10000
-S: 0 5 -10000 -10000      0 -10000  10000
+S: 0 6 -10000 -10000      0 -10000  10000

 V-tail mixers
 -------------
@@ -10,13 +10,13 @@ Tilt mechanism servo mixer
 #RIGHT up:2000 down:1000
 M: 2
 O:      10000  10000      0 -10000  10000
-S: 1 8      0 -20000   9000 -10000  10000
+S: 1 4      0 -20000   9000 -10000  10000
 S: 0 2   4000   4000      0 -10000  10000

 #LEFT up:1000 down:2000
 M: 2
 O:      10000  10000      0 -10000  10000
-S: 1 8      0  20000  -10000 -10000  10000
+S: 1 4      0  20000  -10000 -10000  10000
 S: 0 2   4000   4000      0 -10000  10000

 Elevon mixers
@@ -3,14 +3,14 @@ Aileron/v-tail/throttle VTOL mixer for PX4FMU

 This file defines mixers suitable for controlling a fixed wing aircraft with
 aileron, v-tail (rudder, elevator) and throttle using PX4FMU.
-The configuration assumes the aileron servos are connected to PX4FMU
+The configuration assumes the aileron servos are connected to PX4FMU 
 AUX servo output 0 and 1, the tail servos to output 2 and 3, the throttle
 to output 4.

 Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
-(roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 5 (spoiler).
+(roll), 1 (pitch), 2 (yaw) and 3 (thrust) 4 (flaps) 6 (flaperon).

-Aileron mixer (roll + spoiler)
+Aileron mixer (roll + flaperon)
 ---------------------------------

 This mixer assumes that the aileron servos are set up correctly mechanically;
@@ -21,12 +21,12 @@ endpoints to suit.
 M: 2
 O:      10000  10000      0 -10000  10000
 S: 1 0  10000  10000      0 -10000  10000
-S: 1 5  10000  10000      0 -10000  10000
+S: 1 6  10000  10000      0 -10000  10000

 M: 2
 O:      10000  10000      0 -10000  10000
 S: 1 0  10000  10000      0 -10000  10000
-S: 1 5 -10000 -10000      0 -10000  10000
+S: 1 6 -10000 -10000      0 -10000  10000


 V-tail mixers
@@ -10,13 +10,13 @@ Tilt mechanism servo mixer
 #RIGHT up:2000 down:1000
 M: 2
 O:      10000  10000      0 -10000  10000
-S: 1 8      0 -20000  10000 -10000  10000
+S: 1 4      0 -20000  10000 -10000  10000
 S: 0 2   8000   8000      0 -10000  10000

 #LEFT up:1000 down:2000
 M: 2
 O:      10000  10000      0 -10000  10000
-S: 1 8      0  20000 -10000 -10000  10000
+S: 1 4      0  20000 -10000 -10000  10000
 S: 0 2   8000   8000      0 -10000  10000

 Elevon mixers
@@ -13,7 +13,8 @@ exec find boards msg src platforms test \
    -path platforms/qurt/dspal -prune -o \
    -path src/drivers/uavcan/libuavcan -prune -o \
    -path src/drivers/uavcan/uavcan_drivers/kinetis/driver/include/uavcan_kinetis -prune -o \
-    -path src/drivers/cyphal/libcanard -prune -o \
+    -path src/drivers/uavcan_v1/libcanard -prune -o \
+    -path src/drivers/uavcannode_gps_demo/libcanard -prune -o \
    -path src/lib/crypto/monocypher -prune -o \
    -path src/lib/events/libevents -prune -o \
    -path src/lib/parameters/uthash -prune -o \
@@ -11,7 +11,7 @@ from pyulog import ULog
 from analysis.detectors import InAirDetector, PreconditionError
 from analysis.metrics import calculate_ecl_ekf_metrics
 from analysis.checks import perform_ecl_ekf_checks
-from analysis.post_processing import get_estimator_check_flags
+from analysis.post_processing import get_gps_check_fail_flags

 def analyse_ekf(
        ulog: ULog, check_levels: Dict[str, float], multi_instance: int = 0,
@@ -40,6 +40,11 @@ def analyse_ekf(
    except:
        raise PreconditionError('could not find estimator_status instance', multi_instance)

+    try:
+        estimator_status_flags = ulog.get_dataset('estimator_status_flags', multi_instance).data
+    except:
+        raise PreconditionError('could not find estimator_status_flags instance', multi_instance)
+
    try:
        _ = ulog.get_dataset('estimator_innovations', multi_instance).data
    except:
@@ -61,14 +66,14 @@ def analyse_ekf(
        'in_air_transition_time': round(in_air.take_off + in_air.log_start, 2),
        'on_ground_transition_time': round(in_air.landing + in_air.log_start, 2)}

-    control_mode, innov_flags, gps_fail_flags = get_estimator_check_flags(estimator_status)
+    gps_fail_flags = get_gps_check_fail_flags(estimator_status)

    sensor_checks, innov_fail_checks = find_checks_that_apply(
-        control_mode, estimator_status,
+        estimator_status_flags, estimator_status,
        pos_checks_when_sensors_not_fused=pos_checks_when_sensors_not_fused)

    metrics = calculate_ecl_ekf_metrics(
-        ulog, innov_flags, innov_fail_checks, sensor_checks, in_air, in_air_no_ground_effects,
+        ulog, estimator_status_flags, innov_fail_checks, sensor_checks, in_air, in_air_no_ground_effects,
        multi_instance, red_thresh=red_thresh, amb_thresh=amb_thresh)

    check_status, master_status = perform_ecl_ekf_checks(
@@ -78,12 +83,12 @@ def analyse_ekf(


 def find_checks_that_apply(
-    control_mode: dict, estimator_status: dict, pos_checks_when_sensors_not_fused: bool = False) ->\
+    estimator_status_flags: dict, estimator_status: dict, pos_checks_when_sensors_not_fused: bool = False) ->\
        Tuple[List[str], List[str]]:
    """
    finds the checks that apply and stores them in lists for the std checks and the innovation
    fail checks.
-    :param control_mode:
+    :param estimator_status_flags:
    :param estimator_status:
    :param b_pos_only_when_sensors_fused:
    :return: a tuple of two lists that contain strings for the std checks and for the innovation
@@ -97,7 +102,7 @@ def find_checks_that_apply(
    innov_fail_checks.append('posv')

    # Magnetometer Sensor Checks
-    if (np.amax(control_mode['yaw_aligned']) > 0.5):
+    if (np.amax(estimator_status_flags['cs_yaw_align']) > 0.5):
        sensor_checks.append('mag')

        innov_fail_checks.append('magx')
@@ -106,13 +111,14 @@ def find_checks_that_apply(
        innov_fail_checks.append('yaw')

    # Velocity Sensor Checks
-    if (np.amax(control_mode['using_gps']) > 0.5):
+    if (np.amax(estimator_status_flags['cs_gps']) > 0.5):
        sensor_checks.append('vel')
-        innov_fail_checks.append('vel')
+        innov_fail_checks.append('velh')
+        innov_fail_checks.append('velv')

    # Position Sensor Checks
-    if (pos_checks_when_sensors_not_fused or (np.amax(control_mode['using_gps']) > 0.5)
-        or (np.amax(control_mode['using_evpos']) > 0.5)):
+    if (pos_checks_when_sensors_not_fused or (np.amax(estimator_status_flags['cs_gps']) > 0.5)
+        or (np.amax(estimator_status_flags['cs_ev_pos']) > 0.5)):
        sensor_checks.append('pos')
        innov_fail_checks.append('posh')

@@ -128,7 +134,7 @@ def find_checks_that_apply(
        innov_fail_checks.append('hagl')

    # optical flow sensor checks
-    if (np.amax(control_mode['using_optflow']) > 0.5):
+    if (np.amax(estimator_status_flags['cs_opt_flow']) > 0.5):
        innov_fail_checks.append('ofx')
        innov_fail_checks.append('ofy')

@@ -123,7 +123,8 @@ def perform_sensor_innov_checks(
                                              ('magy', 'magy_fail_percentage', 'mag'),
                                              ('magz', 'magz_fail_percentage', 'mag'),
                                              ('yaw', 'yaw_fail_percentage', 'yaw'),
-                                              ('vel', 'vel_fail_percentage', 'vel'),
+                                              ('velh', 'vel_fail_percentage', 'vel'),
+                                              ('velv', 'vel_fail_percentage', 'vel'),
                                              ('posh', 'pos_fail_percentage', 'pos'),
                                              ('tas', 'tas_fail_percentage', 'tas'),
                                              ('hagl', 'hagl_fail_percentage', 'hagl'),
@@ -11,7 +11,7 @@ import numpy as np
 from analysis.detectors import InAirDetector

 def calculate_ecl_ekf_metrics(
-        ulog: ULog, innov_flags: Dict[str, float], innov_fail_checks: List[str],
+        ulog: ULog, estimator_status_flags: Dict[str, float], innov_fail_checks: List[str],
        sensor_checks: List[str], in_air: InAirDetector, in_air_no_ground_effects: InAirDetector,
        multi_instance: int = 0, red_thresh: float = 1.0, amb_thresh: float = 0.5) -> Tuple[dict, dict, dict, dict]:

@@ -20,7 +20,7 @@ def calculate_ecl_ekf_metrics(
        red_thresh=red_thresh, amb_thresh=amb_thresh)

    innov_fail_metrics = calculate_innov_fail_metrics(
-        innov_flags, innov_fail_checks, in_air, in_air_no_ground_effects)
+        estimator_status_flags, innov_fail_checks, in_air, in_air_no_ground_effects)

    imu_metrics = calculate_imu_metrics(ulog, multi_instance, in_air_no_ground_effects)

@@ -90,10 +90,10 @@ def calculate_sensor_metrics(


 def calculate_innov_fail_metrics(
-        innov_flags: dict, innov_fail_checks: List[str], in_air: InAirDetector,
+        estimator_status_flags: dict, innov_fail_checks: List[str], in_air: InAirDetector,
        in_air_no_ground_effects: InAirDetector) -> dict:
    """
-    :param innov_flags:
+    :param estimator_status_flags:
    :param innov_fail_checks:
    :param in_air:
    :param in_air_no_ground_effects:
@@ -103,17 +103,18 @@ def calculate_innov_fail_metrics(
    innov_fail_metrics = dict()

    # calculate innovation check fail metrics
-    for signal_id, signal, result in [('posv', 'posv_innov_fail', 'hgt_fail_percentage'),
-                                      ('magx', 'magx_innov_fail', 'magx_fail_percentage'),
-                                      ('magy', 'magy_innov_fail', 'magy_fail_percentage'),
-                                      ('magz', 'magz_innov_fail', 'magz_fail_percentage'),
-                                      ('yaw', 'yaw_innov_fail', 'yaw_fail_percentage'),
-                                      ('vel', 'vel_innov_fail', 'vel_fail_percentage'),
-                                      ('posh', 'posh_innov_fail', 'pos_fail_percentage'),
-                                      ('tas', 'tas_innov_fail', 'tas_fail_percentage'),
-                                      ('hagl', 'hagl_innov_fail', 'hagl_fail_percentage'),
-                                      ('ofx', 'ofx_innov_fail', 'ofx_fail_percentage'),
-                                      ('ofy', 'ofy_innov_fail', 'ofy_fail_percentage')]:
+    for signal_id, signal, result in [('posv', 'reject_ver_pos', 'hgt_fail_percentage'),
+                                      ('magx', 'reject_mag_x', 'magx_fail_percentage'),
+                                      ('magy', 'reject_mag_y', 'magy_fail_percentage'),
+                                      ('magz', 'reject_mag_z', 'magz_fail_percentage'),
+                                      ('yaw', 'reject_yaw', 'yaw_fail_percentage'),
+                                      ('velh', 'reject_hor_vel', 'vel_fail_percentage'),
+                                      ('velv', 'reject_ver_vel', 'vel_fail_percentage'),
+                                      ('posh', 'reject_hor_pos', 'pos_fail_percentage'),
+                                      ('tas', 'reject_airspeed', 'tas_fail_percentage'),
+                                      ('hagl', 'reject_hagl', 'hagl_fail_percentage'),
+                                      ('ofx', 'reject_optflow_x', 'ofx_fail_percentage'),
+                                      ('ofy', 'reject_optflow_y', 'ofy_fail_percentage')]:

        # only run innov fail checks, if they apply.
        if signal_id in innov_fail_checks:
@@ -125,7 +126,7 @@ def calculate_innov_fail_metrics(
                in_air_detector = in_air

            innov_fail_metrics[result] = calculate_stat_from_signal(
-                innov_flags, 'estimator_status', signal, in_air_detector,
+                estimator_status_flags, 'estimator_status_flags', signal, in_air_detector,
                lambda x: 100.0 * np.mean(x > 0.5))

    return innov_fail_metrics
@@ -152,7 +153,7 @@ def calculate_imu_metrics(ulog: ULog, multi_instance, in_air_no_ground_effects:

            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'),
+                for signal, result in [('gyro_coning_vibration', 'imu_coning'),
                                       ('gyro_vibration_metric', 'imu_hfgyro'),
                                       ('accel_vibration_metric', 'imu_hfaccel')]:

@@ -7,115 +7,6 @@ from typing import Tuple

 import numpy as np

-
-def get_estimator_check_flags(estimator_status: dict) -> Tuple[dict, dict, dict]:
-    """
-    :param estimator_status:
-    :return:
-    """
-    control_mode = get_control_mode_flags(estimator_status)
-    innov_flags = get_innovation_check_flags(estimator_status)
-    gps_fail_flags = get_gps_check_fail_flags(estimator_status)
-    return control_mode, innov_flags, gps_fail_flags
-
-
-def get_control_mode_flags(estimator_status: dict) -> dict:
-    """
-    :param estimator_status:
-    :return:
-    """
-
-    control_mode = dict()
-    # extract control mode metadata from estimator_status.control_mode_flags
-    # 0 - true if the filter tilt alignment is complete
-    # 1 - true if the filter yaw alignment is complete
-    # 2 - true if GPS measurements are being fused
-    # 3 - true if optical flow measurements are being fused
-    # 4 - true if a simple magnetic yaw heading is being fused
-    # 5 - true if 3-axis magnetometer measurement are being fused
-    # 6 - true if synthetic magnetic declination measurements are being fused
-    # 7 - true when the vehicle is airborne
-    # 8 - true when wind velocity is being estimated
-    # 9 - true when baro height is being fused as a primary height reference
-    # 10 - true when range finder height is being fused as a primary height reference
-    # 11 - true when range finder height is being fused as a primary height reference
-    # 12 - true when local position data from external vision is being fused
-    # 13 - true when yaw data from external vision measurements is being fused
-    # 14 - true when height data from external vision measurements is being fused
-    # 15 - true when synthetic sideslip measurements are being fused
-    # 16 - true true when the mag field does not match the expected strength
-    # 17 - true true when the vehicle is operating as a fixed wing vehicle
-    # 18 - true when the magnetometer has been declared faulty and is no longer being used
-    # 19 - true true when airspeed measurements are being fused
-    # 20 - true true when protection from ground effect induced static pressure rise is active
-    # 21 - true when rng data wasn't ready for more than 10s and new rng values haven't changed enough
-    # 22 - true when yaw (not ground course) data from a GPS receiver is being fused
-    # 23 - true when the in-flight mag field alignment has been completed
-    # 24 - true when local earth frame velocity data from external vision measurements are being fused
-    # 25 - true when we are using a synthesized measurement for the magnetometer Z component
-    control_mode['tilt_aligned'] = ((2 ** 0 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['yaw_aligned'] = ((2 ** 1 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_gps'] = ((2 ** 2 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_optflow'] = ((2 ** 3 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_magyaw'] = ((2 ** 4 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_mag3d'] = ((2 ** 5 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_magdecl'] = ((2 ** 6 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['airborne'] = ((2 ** 7 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['estimating_wind'] = ((2 ** 8 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_barohgt'] = ((2 ** 9 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_rnghgt'] = ((2 ** 10 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_gpshgt'] = ((2 ** 11 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_evpos'] = ((2 ** 12 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_evyaw'] = ((2 ** 13 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['using_evhgt'] = ((2 ** 14 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['fuse_beta'] = ((2 ** 15 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['mag_field_disturbed'] = ((2 ** 16 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['fixed_wing'] = ((2 ** 17 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['mag_fault'] = ((2 ** 18 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['fuse_aspd'] = ((2 ** 19 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['gnd_effect'] = ((2 ** 20 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['rng_stuck'] = ((2 ** 21 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['gps_yaw'] = ((2 ** 22 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['mag_aligned_in_flight'] = ((2 ** 23 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['ev_vel'] = ((2 ** 24 & estimator_status['control_mode_flags']) > 0) * 1
-    control_mode['synthetic_mag_z'] = ((2 ** 25 & estimator_status['control_mode_flags']) > 0) * 1
-    return control_mode
-
-def get_innovation_check_flags(estimator_status: dict) -> dict:
-    """
-    :param estimator_status:
-    :return:
-    """
-
-    innov_flags = dict()
-    # innovation_check_flags summary
-    # 0 - true if velocity observations have been rejected
-    # 1 - true if horizontal position observations have been rejected
-    # 2 - true if true if vertical position observations have been rejected
-    # 3 - true if the X magnetometer observation has been rejected
-    # 4 - true if the Y magnetometer observation has been rejected
-    # 5 - true if the Z magnetometer observation has been rejected
-    # 6 - true if the yaw observation has been rejected
-    # 7 - true if the airspeed observation has been rejected
-    # 8 - true if synthetic sideslip observation has been rejected
-    # 9 - true if the height above ground observation has been rejected
-    # 10 - true if the X optical flow observation has been rejected
-    # 11 - true if the Y optical flow observation has been rejected
-    innov_flags['vel_innov_fail'] = ((2 ** 0 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['posh_innov_fail'] = ((2 ** 1 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['posv_innov_fail'] = ((2 ** 2 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['magx_innov_fail'] = ((2 ** 3 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['magy_innov_fail'] = ((2 ** 4 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['magz_innov_fail'] = ((2 ** 5 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['yaw_innov_fail'] = ((2 ** 6 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['tas_innov_fail'] = ((2 ** 7 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['sli_innov_fail'] = ((2 ** 8 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['hagl_innov_fail'] = ((2 ** 9 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['ofx_innov_fail'] = ((2 ** 10 & estimator_status['innovation_check_flags']) > 0) * 1
-    innov_flags['ofy_innov_fail'] = ((2 ** 11 & estimator_status['innovation_check_flags']) > 0) * 1
-    return innov_flags
-
-
 def get_gps_check_fail_flags(estimator_status: dict) -> dict:
    """
    :param estimator_status:
@@ -11,7 +11,7 @@ import numpy as np
 from matplotlib.backends.backend_pdf import PdfPages
 from pyulog import ULog

-from analysis.post_processing import magnetic_field_estimates_from_states, get_estimator_check_flags
+from analysis.post_processing import magnetic_field_estimates_from_states, get_gps_check_fail_flags
 from plotting.data_plots import TimeSeriesPlot, InnovationPlot, ControlModeSummaryPlot, \
    CheckFlagsPlot
 from analysis.detectors import PreconditionError
@@ -33,6 +33,11 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
    except:
        raise PreconditionError('could not find estimator_status instance', multi_instance)

+    try:
+        estimator_status_flags = ulog.get_dataset('estimator_status_flags', multi_instance).data
+    except:
+        raise PreconditionError('could not find estimator_status_flags instance', multi_instance)
+
    try:
        estimator_states = ulog.get_dataset('estimator_states', multi_instance).data
    except:
@@ -68,12 +73,13 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
    except:
        raise PreconditionError('could not find innovation data')

-    control_mode, innov_flags, gps_fail_flags = get_estimator_check_flags(estimator_status)
+    gps_fail_flags = get_gps_check_fail_flags(estimator_status)

    status_time = 1e-6 * estimator_status['timestamp']
+    status_flags_time = 1e-6 * estimator_status_flags['timestamp']

    b_finishes_in_air, b_starts_in_air, in_air_duration, in_air_transition_time, \
-    on_ground_transition_time = detect_airtime(control_mode, status_time)
+    on_ground_transition_time = detect_airtime(estimator_status_flags, status_flags_time)

    with PdfPages(output_plot_filename) as pdf_pages:

@@ -173,9 +179,9 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str

        # plot control mode summary A
        data_plot = ControlModeSummaryPlot(
-            status_time, control_mode, [['tilt_aligned', 'yaw_aligned'],
-            ['using_gps', 'using_optflow', 'using_evpos'], ['using_barohgt', 'using_gpshgt',
-             'using_rnghgt', 'using_evhgt'], ['using_magyaw', 'using_mag3d', 'using_magdecl']],
+            status_flags_time, estimator_status_flags, [['cs_tilt_align', 'cs_yaw_align'],
+            ['cs_gps', 'cs_opt_flow', 'cs_ev_pos'], ['cs_baro_hgt', 'cs_gps_hgt',
+             'cs_rng_hgt', 'cs_ev_hgt'], ['cs_mag_hdg', 'cs_mag_3d', 'cs_mag_dec']],
            x_label='time (sec)', y_labels=['aligned', 'pos aiding', 'hgt aiding', 'mag aiding'],
            annotation_text=[['tilt alignment', 'yaw alignment'], ['GPS aiding', 'optical flow aiding',
             'external vision aiding'], ['Baro aiding', 'GPS aiding', 'rangefinder aiding',
@@ -188,7 +194,7 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
        # plot control mode summary B
        # construct additional annotations for the airborne plot
        airborne_annotations = list()
-        if np.amin(np.diff(control_mode['airborne'])) > -0.5:
+        if np.amin(np.diff(estimator_status_flags['cs_in_air'])) > -0.5:
            airborne_annotations.append(
                (on_ground_transition_time, 'air to ground transition not detected'))
        else:
@@ -197,7 +203,7 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
        if in_air_duration > 0.0:
            airborne_annotations.append(((in_air_transition_time + on_ground_transition_time) / 2,
                                         'duration = {:.1f} sec'.format(in_air_duration)))
-        if np.amax(np.diff(control_mode['airborne'])) < 0.5:
+        if np.amax(np.diff(estimator_status_flags['cs_in_air'])) < 0.5:
            airborne_annotations.append(
                (in_air_transition_time, 'ground to air transition not detected'))
        else:
@@ -205,7 +211,7 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
                (in_air_transition_time, 'in-air at {:.1f} sec'.format(in_air_transition_time)))

        data_plot = ControlModeSummaryPlot(
-            status_time, control_mode, [['airborne'], ['estimating_wind']],
+            status_flags_time, estimator_status_flags, [['cs_in_air'], ['cs_wind']],
            x_label='time (sec)', y_labels=['airborne', 'estimating wind'], annotation_text=[[], []],
            additional_annotation=[airborne_annotations, []],
            plot_title='EKF Control Status - Figure B', pdf_handle=pdf_pages)
@@ -214,15 +220,15 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str

        # plot innovation_check_flags summary
        data_plot = CheckFlagsPlot(
-            status_time, innov_flags, [['vel_innov_fail', 'posh_innov_fail'], ['posv_innov_fail',
-                                                                               'hagl_innov_fail'],
-                                       ['magx_innov_fail', 'magy_innov_fail', 'magz_innov_fail',
-                                        'yaw_innov_fail'], ['tas_innov_fail'], ['sli_innov_fail'],
-                                       ['ofx_innov_fail',
-                                        'ofy_innov_fail']], x_label='time (sec)',
+            status_flags_time, estimator_status_flags, [['reject_hor_vel', 'reject_hor_pos'], ['reject_ver_vel', 'reject_ver_pos',
+                                                                               'reject_hagl'],
+                                       ['reject_mag_x', 'reject_mag_y', 'reject_mag_z',
+                                        'reject_yaw'], ['reject_airspeed'], ['reject_sideslip'],
+                                       ['reject_optflow_x',
+                                        'reject_optflow_y']], x_label='time (sec)',
            y_labels=['failed', 'failed', 'failed', 'failed', 'failed', 'failed'],
            y_lim=(-0.1, 1.1),
-            legend=[['vel NED', 'pos NE'], ['hgt absolute', 'hgt above ground'],
+            legend=[['vel NE', 'pos NE'], ['vel D', 'hgt absolute', 'hgt above ground'],
                    ['mag_x', 'mag_y', 'mag_z', 'yaw'], ['airspeed'], ['sideslip'],
                    ['flow X', 'flow Y']],
            plot_title='EKF Innovation Test Fails', annotate=False, pdf_handle=pdf_pages)
@@ -344,33 +350,33 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
        data_plot.close()


-def detect_airtime(control_mode, status_time):
+def detect_airtime(estimator_status_flags, status_flags_time):
    # define flags for starting and finishing in air
    b_starts_in_air = False
    b_finishes_in_air = False
    # calculate in-air transition time
-    if (np.amin(control_mode['airborne']) < 0.5) and (np.amax(control_mode['airborne']) > 0.5):
-        in_air_transtion_time_arg = np.argmax(np.diff(control_mode['airborne']))
-        in_air_transition_time = status_time[in_air_transtion_time_arg]
-    elif (np.amax(control_mode['airborne']) > 0.5):
-        in_air_transition_time = np.amin(status_time)
+    if (np.amin(estimator_status_flags['cs_in_air']) < 0.5) and (np.amax(estimator_status_flags['cs_in_air']) > 0.5):
+        in_air_transtion_time_arg = np.argmax(np.diff(estimator_status_flags['cs_in_air']))
+        in_air_transition_time = status_flags_time[in_air_transtion_time_arg]
+    elif (np.amax(estimator_status_flags['cs_in_air']) > 0.5):
+        in_air_transition_time = np.amin(status_flags_time)
        print('log starts while in-air at ' + str(round(in_air_transition_time, 1)) + ' sec')
        b_starts_in_air = True
    else:
        in_air_transition_time = float('NaN')
        print('always on ground')
    # calculate on-ground transition time
-    if (np.amin(np.diff(control_mode['airborne'])) < 0.0):
-        on_ground_transition_time_arg = np.argmin(np.diff(control_mode['airborne']))
-        on_ground_transition_time = status_time[on_ground_transition_time_arg]
-    elif (np.amax(control_mode['airborne']) > 0.5):
-        on_ground_transition_time = np.amax(status_time)
+    if (np.amin(np.diff(estimator_status_flags['cs_in_air'])) < 0.0):
+        on_ground_transition_time_arg = np.argmin(np.diff(estimator_status_flags['cs_in_air']))
+        on_ground_transition_time = status_flags_time[on_ground_transition_time_arg]
+    elif (np.amax(estimator_status_flags['cs_in_air']) > 0.5):
+        on_ground_transition_time = np.amax(status_flags_time)
        print('log finishes while in-air at ' + str(round(on_ground_transition_time, 1)) + ' sec')
        b_finishes_in_air = True
    else:
        on_ground_transition_time = float('NaN')
        print('always on ground')
-    if (np.amax(np.diff(control_mode['airborne'])) > 0.5) and (np.amin(np.diff(control_mode['airborne'])) < -0.5):
+    if (np.amax(np.diff(estimator_status_flags['cs_in_air'])) > 0.5) and (np.amin(np.diff(estimator_status_flags['cs_in_air'])) < -0.5):
        if ((on_ground_transition_time - in_air_transition_time) > 0.0):
            in_air_duration = on_ground_transition_time - in_air_transition_time
        else:
@@ -200,12 +200,13 @@ if [[ $INSTALL_SIM == "true" ]]; then

 	if [[ "${UBUNTU_RELEASE}" == "18.04" ]]; then
 		java_version=11
+		gazebo_version=9
 	elif [[ "${UBUNTU_RELEASE}" == "20.04" ]]; then
 		java_version=13
-	elif [[ "${UBUNTU_RELEASE}" == "22.04" ]]; then
-		java_version=11
+		gazebo_version=11
 	else
 		java_version=14
+		gazebo_version=11
 	fi
 	# Java (jmavsim or fastrtps)
 	sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
@@ -219,30 +220,20 @@ if [[ $INSTALL_SIM == "true" ]]; then
 	sudo update-alternatives --set java $(update-alternatives --list java | grep "java-$java_version")

 	# Gazebo
-	if [[ "${UBUNTU_RELEASE}" == "18.04" ]]; then
-		gazebo_version=9
-		gazebo_packages="gazebo$gazebo_version libgazebo$gazebo_version-dev"
-	elif [[ "${UBUNTU_RELEASE}" == "22.04" ]]; then
-		gazebo_packages="gazebo libgazebo-dev"
-	else
-		# default and Ubuntu 20.04
-		gazebo_version=11
-		gazebo_packages="gazebo$gazebo_version libgazebo$gazebo_version-dev"
-	fi
-
 	sudo sh -c 'echo "deb http://packages.osrfoundation.org/gazebo/ubuntu-stable `lsb_release -cs` main" > /etc/apt/sources.list.d/gazebo-stable.list'
 	wget http://packages.osrfoundation.org/gazebo.key -O - | sudo apt-key add -
 	# Update list, since new gazebo-stable.list has been added
 	sudo apt-get update -y --quiet
 	sudo DEBIAN_FRONTEND=noninteractive apt-get -y --quiet --no-install-recommends install \
 		dmidecode \
-		$gazebo_packages \
+		gazebo$gazebo_version \
 		gstreamer1.0-plugins-bad \
 		gstreamer1.0-plugins-base \
 		gstreamer1.0-plugins-good \
 		gstreamer1.0-plugins-ugly \
 		gstreamer1.0-libav \
 		libeigen3-dev \
+		libgazebo$gazebo_version-dev \
 		libgstreamer-plugins-base1.0-dev \
 		libimage-exiftool-perl \
 		libopencv-dev \
@@ -130,8 +130,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDIO_BLOCKSETUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -174,7 +173,7 @@ CONFIG_STM32_SPI1=y
 CONFIG_STM32_SPI2=y
 CONFIG_STM32_SPI4=y
 CONFIG_STM32_SPI4_DMA=y
-CONFIG_STM32_SPI4_DMA_BUFFER=1024
+CONFIG_STM32_SPI4_DMA_BUFFER=512
 CONFIG_STM32_SPI_DMA=y
 CONFIG_STM32_SPI_DMATHRESHOLD=8
 CONFIG_STM32_TIM10=y
@@ -105,8 +105,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -107,8 +107,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -107,8 +107,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -107,8 +107,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_MODE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -162,8 +162,7 @@ CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_MODE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -126,8 +126,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
 CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -125,8 +125,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
 CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -108,8 +108,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -139,8 +139,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -111,6 +111,7 @@ MEMORY
 {
 	ITCM_RAM  (rwx) : ORIGIN = 0x00000000, LENGTH =   64K
 	FLASH      (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
+
 	DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH =   64K
 	DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH =   64K
 	AXI_SRAM  (rwx) : ORIGIN = 0x24000000, LENGTH =  512K /* D1 domain AXI bus */
@@ -186,7 +187,12 @@ SECTIONS
 		*(.gnu.linkonce.d.*)
 		CONSTRUCTORS
 		_edata = ABSOLUTE(.);
-	} > AXI_SRAM AT > FLASH
+
+		/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
+		. = ALIGN(16);
+		FILL(0xffff)
+		. += 16;
+	} > AXI_SRAM AT > FLASH  = 0xffff

 	.bss : {
 		_sbss = ABSOLUTE(.);
@@ -138,8 +138,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -111,6 +111,7 @@ MEMORY
 {
 	ITCM_RAM  (rwx) : ORIGIN = 0x00000000, LENGTH =   64K
 	FLASH      (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
+
 	DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH =   64K
 	DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH =   64K
 	AXI_SRAM  (rwx) : ORIGIN = 0x24000000, LENGTH =  512K /* D1 domain AXI bus */
@@ -186,7 +187,12 @@ SECTIONS
 		*(.gnu.linkonce.d.*)
 		CONSTRUCTORS
 		_edata = ABSOLUTE(.);
-	} > AXI_SRAM AT > FLASH
+
+		/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
+		. = ALIGN(16);
+		FILL(0xffff)
+		. += 16;
+	} > AXI_SRAM AT > FLASH  = 0xffff

 	.bss : {
 		_sbss = ABSOLUTE(.);
@@ -4,7 +4,6 @@ CONFIG_DRIVERS_IRLOCK=n
 CONFIG_DRIVERS_PCA9685=n
 CONFIG_DRIVERS_PCA9685_PWM_OUT=n
 CONFIG_DRIVERS_RPM=n
-CONFIG_DRIVERS_UAVCAN=n
 CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=n
 CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=n
 CONFIG_MODULES_ROVER_POS_CONTROL=n
@@ -140,8 +140,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -187,7 +187,12 @@ SECTIONS
 		*(.gnu.linkonce.d.*)
 		CONSTRUCTORS
 		_edata = ABSOLUTE(.);
-	} > AXI_SRAM AT > FLASH
+
+		/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
+		. = ALIGN(16);
+		FILL(0xffff)
+		. += 16;
+	} > AXI_SRAM AT > FLASH  = 0xffff

 	.bss : {
 		_sbss = ABSOLUTE(.);
@@ -138,8 +138,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -4,7 +4,6 @@ CONFIG_DRIVERS_IRLOCK=n
 CONFIG_DRIVERS_PCA9685=n
 CONFIG_DRIVERS_PCA9685_PWM_OUT=n
 CONFIG_DRIVERS_RPM=n
-CONFIG_DRIVERS_UAVCAN=n
 CONFIG_EXAMPLES_FAKE_GPS=n
 CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=n
 CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=n
@@ -141,8 +141,7 @@ CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_MODE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -4,7 +4,7 @@ CONFIG_BOARD_CONSTRAINED_FLASH=y
 CONFIG_BOARD_NO_HELP=y
 CONFIG_BOARD_CONSTRAINED_MEMORY=y
 CONFIG_BOARD_EXTERNAL_METADATA=y
-CONFIG_BOARD_SERIAL_URT6="/dev/ttyS2"
+CONFIG_BOARD_SERIAL_GPS1="/dev/ttyS2"
 CONFIG_BOARD_SERIAL_TEL2="/dev/ttyS1"
 CONFIG_DRIVERS_ADC_BOARD_ADC=y
 CONFIG_DRIVERS_BAROMETER_BMP280=y
@@ -23,10 +23,10 @@ CONFIG_MODULES_BATTERY_STATUS=y
 CONFIG_MODULES_COMMANDER=y
 CONFIG_MODULES_CONTROL_ALLOCATOR=y
 CONFIG_MODULES_DATAMAN=y
-CONFIG_MODULES_EKF2=y
+CONFIG_MODULES_EKF2=n
 CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
 CONFIG_MODULES_LAND_DETECTOR=y
-CONFIG_MODULES_LOAD_MON=y
+CONFIG_MODULES_LOGGER=y
 CONFIG_MODULES_MANUAL_CONTROL=y
 CONFIG_MODULES_MAVLINK=y
 CONFIG_MODULES_MC_ATT_CONTROL=y
@@ -120,8 +120,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
 CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -158,7 +157,7 @@ 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=1024
+CONFIG_STM32_SPI1_DMA_BUFFER=512
 CONFIG_STM32_SPI2=y
 CONFIG_STM32_SPI2_DMA=y
 CONFIG_STM32_SPI3=y
@@ -122,8 +122,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -108,8 +108,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -109,16 +109,17 @@

 MEMORY
 {
-	itcm  (rwx) : ORIGIN = 0x00000000, LENGTH =   64K
-	flash (rx)  : ORIGIN = 0x08020000, LENGTH = 1920K
-	dtcm1 (rwx) : ORIGIN = 0x20000000, LENGTH =   64K
-	dtcm2 (rwx) : ORIGIN = 0x20010000, LENGTH =   64K
-	sram  (rwx) : ORIGIN = 0x24000000, LENGTH =  512K
-	sram1 (rwx) : ORIGIN = 0x30000000, LENGTH =  128K
-	sram2 (rwx) : ORIGIN = 0x30020000, LENGTH =  128K
-	sram3 (rwx) : ORIGIN = 0x30040000, LENGTH =   32K
-	sram4 (rwx) : ORIGIN = 0x38000000, LENGTH =   64K
-	bbram (rwx) : ORIGIN = 0x38800000, LENGTH =    4K
+	ITCM_RAM  (rwx) : ORIGIN = 0x00000000, LENGTH =   64K
+	FLASH      (rx) : ORIGIN = 0x08020000, LENGTH = 1920K
+
+	DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH =   64K
+	DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH =   64K
+	AXI_SRAM  (rwx) : ORIGIN = 0x24000000, LENGTH =  512K /* D1 domain AXI bus */
+	SRAM1     (rwx) : ORIGIN = 0x30000000, LENGTH =  128K /* D2 domain AHB bus */
+	SRAM2     (rwx) : ORIGIN = 0x30020000, LENGTH =  128K /* D2 domain AHB bus */
+	SRAM3     (rwx) : ORIGIN = 0x30040000, LENGTH =   32K /* D2 domain AHB bus */
+	SRAM4     (rwx) : ORIGIN = 0x38000000, LENGTH =   64K /* D3 domain */
+	BKPRAM    (rwx) : ORIGIN = 0x38800000, LENGTH =    4K
 }

 OUTPUT_ARCH(arm)
@@ -156,7 +157,7 @@ SECTIONS
 		*(.gnu.linkonce.r.*)
 		_etext = ABSOLUTE(.);

-	} > flash
+	} > FLASH

 	/*
 	 * Init functions (static constructors and the like)
@@ -165,17 +166,17 @@ SECTIONS
 		_sinit = ABSOLUTE(.);
 		KEEP(*(.init_array .init_array.*))
 		_einit = ABSOLUTE(.);
-	} > flash
+	} > FLASH


 	.ARM.extab : {
 		*(.ARM.extab*)
-	} > flash
+	} > FLASH

 	__exidx_start = ABSOLUTE(.);
 	.ARM.exidx : {
 		*(.ARM.exidx*)
-	} > flash
+	} > FLASH
 	__exidx_end = ABSOLUTE(.);

 	_eronly = ABSOLUTE(.);
@@ -186,7 +187,12 @@ SECTIONS
 		*(.gnu.linkonce.d.*)
 		CONSTRUCTORS
 		_edata = ABSOLUTE(.);
-	} > sram AT > flash
+
+		/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
+		. = ALIGN(16);
+		FILL(0xffff)
+		. += 16;
+	} > AXI_SRAM AT > FLASH  = 0xffff

 	.bss : {
 		_sbss = ABSOLUTE(.);
@@ -195,7 +201,7 @@ SECTIONS
 		*(COMMON)
 		. = ALIGN(4);
 		_ebss = ABSOLUTE(.);
-	} > sram
+	} > AXI_SRAM

 	/* Emit the the D3 power domain section for locating BDMA data */

@@ -204,7 +210,7 @@ SECTIONS
 		*(.sram4)
 		. = ALIGN(4);
 		_sram4_heap_start = ABSOLUTE(.);
-	} > sram4
+	} > SRAM4

 	/* Stabs debugging sections. */
 	.stab 0 : { *(.stab) }
@@ -31,6 +31,7 @@ CONFIG_MODULES_MC_RATE_CONTROL=y
 CONFIG_MODULES_NAVIGATOR=y
 CONFIG_MODULES_RC_UPDATE=y
 CONFIG_MODULES_SENSORS=y
+CONFIG_SYSTEMCMDS_HARDFAULT_LOG=y
 CONFIG_SYSTEMCMDS_MIXER=y
 CONFIG_SYSTEMCMDS_PARAM=y
 CONFIG_SYSTEMCMDS_PWM=y
@@ -140,8 +140,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
 CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
 CONFIG_SIG_SIGALRM_ACTION=y
@@ -30,7 +30,7 @@ CONFIG_BOARD_RESET_ON_ASSERT=2
 CONFIG_C99_BOOL8=y
 CONFIG_CDCACM=y
 CONFIG_CDCACM_IFLOWCONTROL=y
-CONFIG_CDCACM_PRODUCTID=0x0050
+CONFIG_CDCACM_PRODUCTID=0x004b
 CONFIG_CDCACM_PRODUCTSTR="PX4 BL Holybro KakuteH7"
 CONFIG_CDCACM_RXBUFSIZE=600
 CONFIG_CDCACM_TXBUFSIZE=12000
@@ -139,8 +139,7 @@ CONFIG_SCHED_LPWORKPRIORITY=50
 CONFIG_SCHED_LPWORKSTACKSIZE=1632
 CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -109,16 +109,17 @@

 MEMORY
 {
-	itcm  (rwx) : ORIGIN = 0x00000000, LENGTH =   64K
-	flash (rx)  : ORIGIN = 0x08020000, LENGTH = 1792K /* params in last sector */
-	dtcm1 (rwx) : ORIGIN = 0x20000000, LENGTH =   64K
-	dtcm2 (rwx) : ORIGIN = 0x20010000, LENGTH =   64K
-	sram  (rwx) : ORIGIN = 0x24000000, LENGTH =  512K
-	sram1 (rwx) : ORIGIN = 0x30000000, LENGTH =  128K
-	sram2 (rwx) : ORIGIN = 0x30020000, LENGTH =  128K
-	sram3 (rwx) : ORIGIN = 0x30040000, LENGTH =   32K
-	sram4 (rwx) : ORIGIN = 0x38000000, LENGTH =   64K
-	bbram (rwx) : ORIGIN = 0x38800000, LENGTH =    4K
+	ITCM_RAM  (rwx) : ORIGIN = 0x00000000, LENGTH =   64K
+	FLASH      (rx) : ORIGIN = 0x08020000, LENGTH = 1792K /* params in last sector */
+
+	DTCM1_RAM (rwx) : ORIGIN = 0x20000000, LENGTH =   64K
+	DTCM2_RAM (rwx) : ORIGIN = 0x20010000, LENGTH =   64K
+	AXI_SRAM  (rwx) : ORIGIN = 0x24000000, LENGTH =  512K /* D1 domain AXI bus */
+	SRAM1     (rwx) : ORIGIN = 0x30000000, LENGTH =  128K /* D2 domain AHB bus */
+	SRAM2     (rwx) : ORIGIN = 0x30020000, LENGTH =  128K /* D2 domain AHB bus */
+	SRAM3     (rwx) : ORIGIN = 0x30040000, LENGTH =   32K /* D2 domain AHB bus */
+	SRAM4     (rwx) : ORIGIN = 0x38000000, LENGTH =   64K /* D3 domain */
+	BKPRAM    (rwx) : ORIGIN = 0x38800000, LENGTH =    4K
 }

 OUTPUT_ARCH(arm)
@@ -156,7 +157,7 @@ SECTIONS
 		*(.gnu.linkonce.r.*)
 		_etext = ABSOLUTE(.);

-	} > flash
+	} > FLASH

 	/*
 	 * Init functions (static constructors and the like)
@@ -165,17 +166,17 @@ SECTIONS
 		_sinit = ABSOLUTE(.);
 		KEEP(*(.init_array .init_array.*))
 		_einit = ABSOLUTE(.);
-	} > flash
+	} > FLASH


 	.ARM.extab : {
 		*(.ARM.extab*)
-	} > flash
+	} > FLASH

 	__exidx_start = ABSOLUTE(.);
 	.ARM.exidx : {
 		*(.ARM.exidx*)
-	} > flash
+	} > FLASH
 	__exidx_end = ABSOLUTE(.);

 	_eronly = ABSOLUTE(.);
@@ -186,7 +187,12 @@ SECTIONS
 		*(.gnu.linkonce.d.*)
 		CONSTRUCTORS
 		_edata = ABSOLUTE(.);
-	} > sram AT > flash
+
+		/* Pad out last section as the STM32H7 Flash write size is 256 bits. 32 bytes */
+		. = ALIGN(16);
+		FILL(0xffff)
+		. += 16;
+	} > AXI_SRAM AT > FLASH  = 0xffff

 	.bss : {
 		_sbss = ABSOLUTE(.);
@@ -195,7 +201,7 @@ SECTIONS
 		*(COMMON)
 		. = ALIGN(4);
 		_ebss = ABSOLUTE(.);
-	} > sram
+	} > AXI_SRAM

 	/* Emit the the D3 power domain section for locating BDMA data */

@@ -204,7 +210,7 @@ SECTIONS
 		*(.sram4)
 		. = ALIGN(4);
 		_sram4_heap_start = ABSOLUTE(.);
-	} > sram4
+	} > SRAM4

 	/* Stabs debugging sections. */
 	.stab 0 : { *(.stab) }
@@ -140,8 +140,7 @@ CONFIG_SCHED_WAITPID=y
 CONFIG_SDCLONE_DISABLE=y
 CONFIG_SDMMC1_SDIO_MODE=y
 CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
+CONFIG_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -126,8 +126,7 @@ 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_SEM_PREALLOCHOLDERS=32
 CONFIG_SERIAL_PASSTHRU_UBLOX=y
 CONFIG_SERIAL_TERMIOS=y
 CONFIG_SIG_DEFAULT=y
@@ -1,90 +0,0 @@
-CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
-CONFIG_BOARD_ARCHITECTURE="cortex-m7"
-CONFIG_BOARD_SERIAL_GPS1="/dev/ttyS1"
-CONFIG_BOARD_SERIAL_TEL1="/dev/ttyS2"
-CONFIG_BOARD_SERIAL_TEL2="/dev/ttyS3"
-CONFIG_BOARD_SERIAL_TEL3="/dev/ttyS5"
-CONFIG_BOARD_SERIAL_TEL4="/dev/ttyS6"
-CONFIG_DRIVERS_ADC_BOARD_ADC=y
-CONFIG_DRIVERS_BAROMETER_DPS310=y
-CONFIG_DRIVERS_CAMERA_CAPTURE=n
-CONFIG_DRIVERS_CAMERA_TRIGGER=n
-CONFIG_DRIVERS_DSHOT=y
-CONFIG_DRIVERS_GPS=y
-CONFIG_DRIVERS_IMU_INVENSENSE_MPU6000=y
-CONFIG_DRIVERS_IMU_INVENSENSE_ICM20602=y
-CONFIG_DRIVERS_IMU_INVENSENSE_ICM42605=y
-CONFIG_DRIVERS_MAGNETOMETER_QMC5883L=y
-CONFIG_COMMON_DISTANCE_SENSOR=n
-CONFIG_COMMON_LIGHT=n
-CONFIG_COMMON_MAGNETOMETER=n
-CONFIG_COMMON_OPTICAL_FLOW=y
-CONFIG_DRIVERS_OSD=y
-CONFIG_DRIVERS_PWM_OUT=y
-CONFIG_DRIVERS_PWM_OUT_SIM=n
-CONFIG_DRIVERS_RC_INPUT=y
-CONFIG_DRIVERS_RPM=n
-CONFIG_COMMON_TELEMETRY=y
-CONFIG_DRIVERS_TONE_ALARM=y
-CONFIG_DRIVERS_UAVCAN=y
-CONFIG_BOARD_UAVCAN_INTERFACES=1
-CONFIG_MODULES_ATTITUDE_ESTIMATOR_Q=y
-CONFIG_MODULES_BATTERY_STATUS=y
-CONFIG_MODULES_COMMANDER=y
-CONFIG_MODULES_CONTROL_ALLOCATOR=y
-CONFIG_MODULES_DATAMAN=y
-CONFIG_MODULES_EKF2=y
-CONFIG_MODULES_EVENTS=y
-CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
-CONFIG_MODULES_FW_ATT_CONTROL=y
-CONFIG_MODULES_FW_POS_CONTROL_L1=y
-CONFIG_MODULES_GYRO_CALIBRATION=y
-CONFIG_MODULES_GYRO_FFT=y
-CONFIG_MODULES_LAND_DETECTOR=y
-CONFIG_MODULES_LANDING_TARGET_ESTIMATOR=y
-CONFIG_MODULES_LOAD_MON=y
-CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=y
-CONFIG_MODULES_LOGGER=y
-CONFIG_MODULES_MAG_BIAS_ESTIMATOR=y
-CONFIG_MODULES_MANUAL_CONTROL=y
-CONFIG_MODULES_MAVLINK=y
-CONFIG_MODULES_MC_ATT_CONTROL=y
-CONFIG_MODULES_MC_AUTOTUNE_ATTITUDE_CONTROL=n
-CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
-CONFIG_MODULES_MC_POS_CONTROL=y
-CONFIG_MODULES_MC_RATE_CONTROL=y
-CONFIG_MODULES_NAVIGATOR=y
-CONFIG_MODULES_RC_UPDATE=y
-CONFIG_MODULES_SENSORS=y
-CONFIG_MODULES_TEMPERATURE_COMPENSATION=n
-CONFIG_MODULES_VTOL_ATT_CONTROL=y
-CONFIG_MODULES_GIMBAL=n
-CONFIG_SYSTEMCMDS_BL_UPDATE=n
-CONFIG_SYSTEMCMDS_ACTUATOR_TEST=y
-CONFIG_SYSTEMCMDS_DMESG=y
-CONFIG_SYSTEMCMDS_DUMPFILE=n
-CONFIG_SYSTEMCMDS_GPIO=y
-CONFIG_SYSTEMCMDS_HARDFAULT_LOG=y
-CONFIG_SYSTEMCMDS_I2CDETECT=y
-CONFIG_SYSTEMCMDS_LED_CONTROL=n
-CONFIG_SYSTEMCMDS_MFT=n
-CONFIG_SYSTEMCMDS_MIXER=y
-CONFIG_SYSTEMCMDS_MOTOR_TEST=n
-CONFIG_SYSTEMCMDS_MTD=n
-CONFIG_SYSTEMCMDS_NSHTERM=y
-CONFIG_SYSTEMCMDS_PARAM=y
-CONFIG_SYSTEMCMDS_PERF=y
-CONFIG_SYSTEMCMDS_PWM=y
-CONFIG_SYSTEMCMDS_REBOOT=y
-CONFIG_SYSTEMCMDS_SD_BENCH=n
-CONFIG_SYSTEMCMDS_SD_STRESS=n
-CONFIG_SYSTEMCMDS_SERIAL_TEST=n
-CONFIG_SYSTEMCMDS_SYSTEM_TIME=y
-CONFIG_SYSTEMCMDS_TOP=y
-CONFIG_SYSTEMCMDS_TOPIC_LISTENER=y
-CONFIG_SYSTEMCMDS_TUNE_CONTROL=n
-CONFIG_SYSTEMCMDS_UORB=y
-CONFIG_SYSTEMCMDS_USB_CONNECTED=y
-CONFIG_SYSTEMCMDS_VER=y
-CONFIG_SYSTEMCMDS_WORK_QUEUE=y
-CONFIG_EXAMPLES_FAKE_GPS=n
@@ -1,13 +0,0 @@
-{
-    "board_id": 1013,
-    "magic": "PX4FWv1",
-    "description": "Firmware for the MatekH743-slim board",
-    "image": "",
-    "build_time": 0,
-    "summary": "MatekH743-mini",
-    "version": "0.1",
-    "image_size": 0,
-    "image_maxsize": 1966080,
-    "git_identity": "",
-    "board_revision": 0
-}
@@ -1,16 +0,0 @@
-#!/bin/sh
-#
-# board specific extras init
-#------------------------------------------------------------------------------
-
-# if ! param compare OSD_ATXXXX_CFG 0
-# then
-# 	atxxxx start -s
-# fi
-
-atxxxx start -s
-
-
-# DShot telemetry is always on UART7
-# dshot telemetry /dev/ttyS5
-
@@ -1,22 +0,0 @@
-#!/bin/sh
-#
-# board specific sensors init
-#------------------------------------------------------------------------------
-
-board_adc start
-
-# Internal SPI bus ICM-42605
-if ! icm42605 -R 14 -s start
-then
-	# internal SPI bus ICM-20602
-	icm20602 -R 12 -s start
-fi
-
-# Internal SPI bus MPU-6000
-mpu6000 -R 12 -s start
-
-# Internal baro
-dps310 -I start -a 118
-
-# External mag
-qmc5883l -X start -a 13
@@ -1,225 +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_ENVIRON is not set
-# CONFIG_DISABLE_PSEUDOFS_OPERATIONS is not set
-# CONFIG_MMCSD_HAVE_CARDDETECT is not set
-# CONFIG_MMCSD_HAVE_WRITEPROTECT is not set
-# CONFIG_MMCSD_MMCSUPPORT is not set
-# CONFIG_MMCSD_SPI 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_SEMICOLON is not set
-# CONFIG_NSH_DISABLE_TIME is not set
-CONFIG_ARCH="arm"
-CONFIG_ARCH_BOARD_CUSTOM=y
-CONFIG_ARCH_BOARD_CUSTOM_DIR="../../../../boards/matek/h743-mini/nuttx-config"
-CONFIG_ARCH_BOARD_CUSTOM_DIR_RELPATH=y
-CONFIG_ARCH_BOARD_CUSTOM_NAME="px4"
-CONFIG_ARCH_CHIP="stm32h7"
-CONFIG_ARCH_CHIP_STM32H743VI=y
-CONFIG_ARCH_CHIP_STM32H7=y
-CONFIG_ARCH_INTERRUPTSTACK=512
-CONFIG_ARCH_STACKDUMP=y
-CONFIG_ARMV7M_BASEPRI_WAR=y
-CONFIG_ARMV7M_DCACHE=y
-CONFIG_ARMV7M_DTCM=y
-CONFIG_ARMV7M_ICACHE=y
-CONFIG_ARMV7M_MEMCPY=y
-CONFIG_ARMV7M_USEBASEPRI=y
-CONFIG_BOARDCTL_RESET=y
-CONFIG_BOARD_CRASHDUMP=y
-CONFIG_BOARD_LOOPSPERMSEC=95150
-CONFIG_BOARD_RESET_ON_ASSERT=2
-CONFIG_BUILTIN=y
-CONFIG_C99_BOOL8=y
-CONFIG_CDCACM=y
-CONFIG_CDCACM_PRODUCTID=0x0036
-CONFIG_CDCACM_PRODUCTSTR="MatekH743-mini"
-CONFIG_CDCACM_RXBUFSIZE=600
-CONFIG_CDCACM_TXBUFSIZE=12000
-CONFIG_CDCACM_VENDORID=0x1B8C
-CONFIG_CDCACM_VENDORSTR="Matek"
-CONFIG_CLOCK_MONOTONIC=y
-CONFIG_DEBUG_FULLOPT=y
-CONFIG_DEBUG_HARDFAULT_ALERT=y
-CONFIG_DEBUG_MEMFAULT=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_EXPERIMENTAL=y
-CONFIG_FAT_DMAMEMORY=y
-CONFIG_FAT_LCNAMES=y
-CONFIG_FAT_LFN=y
-CONFIG_FAT_LFN_ALIAS_HASH=y
-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_MAX_TASKS=64
-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_MMCSD=y
-CONFIG_MMCSD_SDIO=y
-CONFIG_MMCSD_SDIOWAIT_WRCOMPLETE=y
-CONFIG_MM_REGIONS=4
-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_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_OTG_ID_GPIO_DISABLE=y
-CONFIG_PIPES=y
-CONFIG_PREALLOC_TIMERS=50
-CONFIG_PRIORITY_INHERITANCE=y
-CONFIG_PTHREAD_MUTEX_ROBUST=y
-CONFIG_PTHREAD_STACK_MIN=512
-CONFIG_RAM_SIZE=245760
-CONFIG_RAM_START=0x20010000
-CONFIG_RAW_BINARY=y
-CONFIG_RTC_DATETIME=y
-CONFIG_SCHED_ATEXIT=y
-CONFIG_SCHED_HPWORK=y
-CONFIG_SCHED_HPWORKPRIORITY=249
-CONFIG_SCHED_HPWORKSTACKSIZE=1280
-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_SDCLONE_DISABLE=y
-CONFIG_SDMMC1_SDIO_PULLUP=y
-CONFIG_SEM_NNESTPRIO=8
-CONFIG_SEM_PREALLOCHOLDERS=0
-CONFIG_SERIAL_IFLOWCONTROL_WATERMARKS=y
-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=256
-CONFIG_STM32H7_ADC1=y
-CONFIG_STM32H7_ADC3=y
-CONFIG_STM32H7_BBSRAM=y
-CONFIG_STM32H7_BBSRAM_FILES=5
-CONFIG_STM32H7_BDMA=y
-CONFIG_STM32H7_BKPSRAM=y
-CONFIG_STM32H7_DMA1=y
-CONFIG_STM32H7_DMA2=y
-CONFIG_STM32H7_DMACAPABLE=y
-CONFIG_STM32H7_FLOWCONTROL_BROKEN=y
-CONFIG_STM32H7_I2C1=y
-CONFIG_STM32H7_I2C2=y
-CONFIG_STM32H7_I2C_DYNTIMEO=y
-CONFIG_STM32H7_I2C_DYNTIMEO_STARTSTOP=10
-CONFIG_STM32H7_OTGFS=y
-CONFIG_STM32H7_PROGMEM=y
-CONFIG_STM32H7_RTC=y
-CONFIG_STM32H7_RTC_HSECLOCK=y
-CONFIG_STM32H7_RTC_MAGIC_REG=1
-CONFIG_STM32H7_SAVE_CRASHDUMP=y
-CONFIG_STM32H7_SDMMC1=y
-CONFIG_STM32H7_SERIALBRK_BSDCOMPAT=y
-CONFIG_STM32H7_SERIAL_DISABLE_REORDERING=y
-CONFIG_STM32H7_SPI1=y
-CONFIG_STM32H7_SPI1_DMA=y
-CONFIG_STM32H7_SPI1_DMA_BUFFER=2048
-CONFIG_STM32H7_SPI2=y
-CONFIG_STM32H7_SPI3=y
-CONFIG_STM32H7_SPI4=y
-CONFIG_STM32H7_SPI4_DMA=y
-CONFIG_STM32H7_SPI4_DMA_BUFFER=2048
-CONFIG_STM32H7_SPI_DMA=y
-CONFIG_STM32H7_SPI_DMATHRESHOLD=8
-CONFIG_STM32H7_TIM15=y
-CONFIG_STM32H7_TIM1=y
-CONFIG_STM32H7_TIM2=y
-CONFIG_STM32H7_TIM4=y
-CONFIG_STM32H7_TIM5=y
-CONFIG_STM32H7_TIM8=y
-CONFIG_STM32H7_UART4=y
-CONFIG_STM32H7_UART7=y
-CONFIG_STM32H7_UART8=y
-CONFIG_STM32H7_USART1=y
-CONFIG_STM32H7_USART2=y
-CONFIG_STM32H7_USART3=y
-CONFIG_STM32H7_USART6=y
-CONFIG_STM32H7_USART_BREAKS=y
-CONFIG_STM32H7_USART_INVERT=y
-CONFIG_STM32H7_USART_SINGLEWIRE=y
-CONFIG_STM32H7_USART_SWAP=y
-CONFIG_SYSTEM_CDCACM=y
-CONFIG_SYSTEM_NSH=y
-CONFIG_TASK_NAME_SIZE=24
-CONFIG_UART4_BAUD=57600
-CONFIG_UART4_RXBUFSIZE=600
-CONFIG_UART4_TXBUFSIZE=1500
-CONFIG_UART7_BAUD=57600
-CONFIG_UART7_IFLOWCONTROL=y
-CONFIG_UART7_OFLOWCONTROL=y
-CONFIG_UART7_RXBUFSIZE=600
-CONFIG_UART7_TXBUFSIZE=1500
-CONFIG_UART8_BAUD=57600
-CONFIG_UART8_RXBUFSIZE=600
-CONFIG_UART8_TXBUFSIZE=1500
-CONFIG_USART1_BAUD=57600
-CONFIG_USART1_RXBUFSIZE=600
-CONFIG_USART1_SERIAL_CONSOLE=y
-CONFIG_USART1_TXBUFSIZE=1500
-CONFIG_USART2_BAUD=57600
-CONFIG_USART2_RXBUFSIZE=600
-CONFIG_USART2_TXBUFSIZE=1500
-CONFIG_USART3_BAUD=57600
-CONFIG_USART3_RXBUFSIZE=600
-CONFIG_USART3_TXBUFSIZE=1500
-CONFIG_USART6_BAUD=57600
-CONFIG_USART6_RXBUFSIZE=600
-CONFIG_USART6_TXBUFSIZE=1500
-CONFIG_USBDEV=y
-CONFIG_USBDEV_BUSPOWERED=y
-CONFIG_USBDEV_MAXPOWER=500
-CONFIG_USEC_PER_TICK=1000
-CONFIG_USERMAIN_STACKSIZE=2944
-CONFIG_USER_ENTRYPOINT="nsh_main"
-CONFIG_WATCHDOG=y
@@ -1,237 +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.
- *
- ****************************************************************************/
-
-/**
- * @file board_config.h
- *
- * Board internal definitions
- */
-
-#pragma once
-
-/****************************************************************************************************
- * Included Files
- ****************************************************************************************************/
-
-#include <px4_platform_common/px4_config.h>
-#include <nuttx/compiler.h>
-#include <stdint.h>
-
-#include <stm32_gpio.h>
-
-/****************************************************************************************************
- * Definitions
- ****************************************************************************************************/
-
-// #define FLASH_BASED_PARAMS
-
-
-/* LEDs are driven with push open drain to support Anode to 5V or 3.3V */
-
-#define GPIO_nLED_BLUE          /* PE3 */  (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN3)
-#define GPIO_nLED_GREEN         /* PE4 */  (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_50MHz|GPIO_OUTPUT_SET|GPIO_PORTE|GPIO_PIN4)
-
-#define BOARD_HAS_CONTROL_STATUS_LEDS   1
-#define BOARD_ARMED_STATE_LED           1 // Green LED
-#define BOARD_OVERLOAD_LED              0 // Blue LED
-
-
-/*
- * ADC channels
- *
- * These are the channel numbers of the ADCs of the microcontroller that
- * can be used by the Px4 Firmware in the adc driver
- */
-
-/* ADC defines to be used in sensors.cpp to read from a particular channel */
-#define ADC1_CH(n)                  (n)
-
-/* Define GPIO pins used as ADC N.B. Channel numbers must match below  */
-#define PX4_ADC_GPIO  \
-	/* PC0  */  GPIO_ADC123_INP10, \
-	/* PC1  */  GPIO_ADC123_INP11, \
-	/* PA4  */  GPIO_ADC12_INP18, \
-	/* PA7  */  GPIO_ADC12_INP7, \
-	/* PC4  */  GPIO_ADC12_INP4, \
-	/* PC5  */  GPIO_ADC12_INP8
-
-/* Define Channel numbers must match above GPIO pin IN(n)*/
-#define ADC_BATTERY_VOLTAGE_CHANNEL     /* PC0  */  ADC1_CH(10)
-#define ADC_BATTERY_CURRENT_CHANNEL     /* PC1  */  ADC1_CH(11)
-#define ADC_BATTERY2_VOLTAGE_CHANNEL    /* PA4  */  ADC1_CH(18)
-#define ADC_BATTERY2_CURRENT_CHANNEL    /* PA7  */  ADC1_CH(7)
-#define ADC_AIRSPEED_IN_CHANNEL         /* PC4  */  ADC1_CH(4)
-#define ADC_RSSI_IN_CHANNEL             /* PC5  */  ADC1_CH(8)
-
-#define ADC_CHANNELS \
-	((1 << ADC_BATTERY_VOLTAGE_CHANNEL) | \
-	 (1 << ADC_BATTERY_CURRENT_CHANNEL) | \
-	 (1 << ADC_BATTERY2_VOLTAGE_CHANNEL) | \
-	 (1 << ADC_BATTERY2_CURRENT_CHANNEL) | \
-	 (1 << ADC_AIRSPEED_IN_CHANNEL) | \
-	 (1 << ADC_RSSI_IN_CHANNEL))
-
-
-/* Define Battery 1 Voltage Divider and A per V
- */
-
-#define BOARD_BATTERY1_V_DIV         (11.0f)     /* measured with the provided PM board */
-#define BOARD_BATTERY1_A_PER_V       (40.0f)
-#define BOARD_BATTERY2_V_DIV         (11.0f)     /* measured with the provided PM board */
-
-
-/* CAN Silence
- *
- * Silent mode control \ ESC Mux select
- */
-
-#define GPIO_CAN1_SILENT_S0  /* PD3  */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTD|GPIO_PIN3)
-
-
-/* PWM
- */
-#define DIRECT_PWM_OUTPUT_CHANNELS   12
-#define DIRECT_INPUT_TIMER_CHANNELS  12
-
-#define BOARD_HAS_PWM  DIRECT_PWM_OUTPUT_CHANNELS
-
-
-/* Spare GPIO */
-
-// #define GPIO_PG6                        /* PG6  */  (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN6)
-// #define GPIO_PD15                       /* PD15 */  (GPIO_INPUT|GPIO_FLOAT|GPIO_PORTD|GPIO_PIN15)
-// #define GPIO_PG15                       /* PG15 */  (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTG|GPIO_PIN15)
-
-
-/* Tone alarm output */
-
-#define GPIO_TONE_ALARM_IDLE    /* PA15 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN15)
-#define GPIO_TONE_ALARM_GPIO    /* PA15 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN15)
-
-// #define TONE_ALARM_TIMER        2  /* Timer 2 */
-// #define TONE_ALARM_CHANNEL      1  /* PA15 GPIO_TIM2_CH1OUT_2 */
-// #define GPIO_TONE_ALARM_IDLE    /* PA15 */ (GPIO_OUTPUT|GPIO_PUSHPULL|GPIO_SPEED_2MHz|GPIO_OUTPUT_CLEAR|GPIO_PORTA|GPIO_PIN15)
-// #define GPIO_TONE_ALARM         GPIO_TIM2_CH1OUT_2
-
-
-/* USB OTG FS
- *
- * PE2  OTG_FS_VBUS VBUS sensing
- */
-
-#define GPIO_OTGFS_VBUS         /* PE2 */ (GPIO_INPUT|GPIO_PULLDOWN|GPIO_SPEED_100MHz|GPIO_PORTE|GPIO_PIN2)
-
-
-/* High-resolution timer */
-#define HRT_TIMER               2  /* use timer8 for the HRT */
-#define HRT_TIMER_CHANNEL       1  /* use capture/compare channel 3 */
-
-
-/* RC Serial port */
-#define RC_SERIAL_PORT          "/dev/ttyS4"
-#define BOARD_SUPPORTS_RC_SERIAL_PORT_OUTPUT
-
-// #define GPIO_RSSI_IN            /* PC5  */ (GPIO_INPUT|GPIO_PULLUP|GPIO_PORTC|GPIO_PIN5)
-
-
-/* SD Card */
-#define SDIO_SLOTNO             0  /* Only one slot */
-#define SDIO_MINOR              0
-
-/* This board provides a DMA pool and APIs */
-#define BOARD_DMA_ALLOC_POOL_SIZE 5120
-
-/* This board provides the board_on_reset interface */
-#define BOARD_HAS_ON_RESET 1
-
-
-#define PX4_GPIO_INIT_LIST { \
-		PX4_ADC_GPIO, \
-		GPIO_CAN1_TX, \
-		GPIO_CAN1_RX, \
-		GPIO_CAN1_SILENT_S0, \
-		GPIO_nLED_BLUE, \
-		GPIO_nLED_GREEN, \
-		GPIO_TONE_ALARM_IDLE, \
-	}
-
-#define BOARD_ENABLE_CONSOLE_BUFFER
-
-#define BOARD_NUM_IO_TIMERS 4
-
-
-__BEGIN_DECLS
-
-/****************************************************************************************************
- * Public Types
- ****************************************************************************************************/
-
-/****************************************************************************************************
- * Public data
- ****************************************************************************************************/
-
-#ifndef __ASSEMBLY__
-
-/****************************************************************************************************
- * Public Functions
- ****************************************************************************************************/
-
-/****************************************************************************
- * Name: stm32_sdio_initialize
- *
- * Description:
- *   Initialize SDIO-based MMC/SD card support
- *
- ****************************************************************************/
-
-int stm32_sdio_initialize(void);
-
-/****************************************************************************************************
- * Name: stm32_spiinitialize
- *
- * Description:
- *   Called to configure SPI chip select GPIO pins for the board.
- *
- ****************************************************************************************************/
-
-extern void stm32_spiinitialize(void);
-
-extern void stm32_usbinitialize(void);
-
-extern void board_peripheral_reset(int ms);
-
-#include <px4_platform_common/board_common.h>
-
-#endif /* __ASSEMBLY__ */
-
-__END_DECLS
--- a/Show More
+++ b/Show More
Author	SHA1	Message	Date
Daniel Agar	6823cbc414	sensors/vehicle_angular_velocity: add IMU_GYRO_RATEMAX constraints	2022-06-07 16:23:01 -04:00
Daniel Agar	beaebe4d0b	sensors/vehicle_imu: don't bother checking IMU_GYRO_RATEMAX	2022-06-07 16:22:54 -04:00
Daniel Agar	0bddca6b9b	boards: NuttX update all boards to preallocated sem holder list - CONFIG_SEM_PREALLOCHOLDERS=32 - CONFIG_SEM_NNESTPRIO=16 (default)	2022-05-29 13:49:01 -04:00
Daniel Agar	c50c1e3982	update NuttX and apps to latest with sem holder fixes and updated ostest	2022-05-29 13:48:15 -04:00
Daniel Agar	a249b77647	boards: reduce SPI DMA buffers on older STM32F4 boards - on common IMUs like the mpu6000, mpu9250, icm20602, etc each FIFO sample is only 12 bytes so this is still more than large enough for the worst case transfer	2022-05-27 16:28:26 -04:00
Daniel Agar	17de164e95	boards: pixhawk 2 cube skip starting low quality l3gd20 gyro to save memory and cpu - free memory is getting tight on these older boards (depending on configuratoin) and the pixhawk 2 cube still has 2 other superior IMUs, so this is just dropping dead weight	2022-05-27 16:28:22 -04:00
David Sidrane	a057b38c40	Update all H7 Bootloders	2022-05-27 14:52:00 -04:00
David Sidrane	39e53711d5	flash_cache:Flush complete cache line	2022-05-27 14:44:54 -04:00
David Sidrane	1294851bb6	boards: STM32H7 pad to 256 bit - 32 bytes (#19724 )	2022-05-27 14:44:51 -04:00
David Sidrane	1c15a1a7f4	px4_fmu-v6c:Fix mag rotation	2022-05-27 14:43:47 -04:00
David Sidrane	21567ca187	boards: new px4_fmu-v6c board support (#19544 )	2022-05-27 14:42:55 -04:00
bresch	8e789bcc7f	ekf2_post-processing: use estimator_status_flags instead of bitmasks	2022-05-24 10:30:52 -04:00
Julian Oes	d699d5f27e	sitl_gazebo: update submodule This fixes the issue where HITL doesn't connect over USB.	2022-05-24 09:43:05 -04:00
Julian Oes	4ae97c505f	commander: lockdown is not termination We use lockdown to prevent outputs like motors and servos from being active in HITL simulation. This means that we can't treat the lockdown flag as a flight_terminated, otherwise we can't arm in HITL at all.	2022-05-24 09:42:38 -04:00
Daniel Agar	b8ce2a6039	icm42688p: only check configured registers periodically (as intended)	2022-05-23 14:58:37 -04:00
bresch	1f399e5b33	ekf2: use explicit flags instead of bitmask position This prevents bitmask mismatch when a new flag is inserted	2022-05-23 14:57:17 -04:00
Serhat Aksun	d67cddae7d	sensors/vehicle_magnetometer: fix multi_mode check Signed-off-by: Serhat Aksun <serhat.aksun@maxwell-innovations.com>	2022-05-23 10:10:22 -04:00
Julian Oes	0290282b17	ROMFS: disable UAVCAN in HITL Without this, uavcan creates MixingOutput classes which then create empty actuator_outputs publications. This then prevents the motor output in HITL to be forwarded to the simulator via mavlink.	2022-05-22 10:27:07 -04:00
Nicolas MARTIN	39d1c79f48	HITL: undefined time_remaining_s should be NAN	2022-05-20 09:40:28 -04:00
Nico van Duijn	ad410a2512	Commander: ignore MAV_CMD_REQUEST_MSG This commit adds the MAV_CMD_REQUEST_MESSAGE to the list of vehicle commands which are ignored without generating a warning sound.	2022-05-20 09:40:22 -04:00
Daniel Agar	453acdce31	.vscode/.gitignore ignore all log files	2022-05-20 09:40:07 -04:00
Beat Küng	afb2538da3	output drivers: init SmartLock after exit_and_cleanup This fixes an invalid memory access when exiting the module: exit_and_cleanup destroys the object, but lock_guard is destructed after and accesses the lock.	2022-05-12 08:17:15 -04:00
alexklimaj	af58c412c3	Fix uavcan battery causing immediate RTL time remaining low	2022-05-11 21:49:13 -04:00
Daniel Agar	d5226b28ce	drivers/rc_input: ensure RC inversion is disabled initially and latch RC_INPUT_PROTO conservatively - this allows jumping straight to a non-SBUS RC protocol - increased the scan time per protocol 300->500 ms, which the newer DSM parser seems to need in some cases. - only set RC_INPUT_PROTO if we've had a successful RC lock for > 3 seconds	2022-05-11 14:31:51 -04:00
Beat Küng	b091ea9fd9	log_writer_file: fix corner case when mission log is enabled Normally _should_run for mission is only ever true if _should_run for the normal log is. There are exceptions though: - the log buffer fails to allocate - there was a write failure (e.g. due to SD card removal) In that situation, the writer would not wait anymore but busy-loop.	2022-05-11 10:07:46 -04:00
Beat Küng	9e91ca8294	log_writer_file: protect access to _should_run, use px4::atomicbool for _exit_thread	2022-05-11 10:07:46 -04:00
Igor Mišić	8302f076e7	uavcan: use timer 6 by default on stm32f7	2022-05-10 12:43:26 -04:00
Thomas Stastny	de26ffa6e0	fw pos ctrl: turn back to takeoff point with npfg	2022-05-06 13:08:07 -04:00
Thomas Stastny	f60d38db65	fw pos ctrl: add missing guidance control interval setting to control_manual_position()	2022-05-06 13:08:07 -04:00
Thomas Stastny	5e3c8d2fa0	fw pos ctrl: fix state switching logic for takeoff and landing	2022-05-06 13:08:07 -04:00
Matthias Grob	90998837ec	Commander: ensure diconnected battery is cleared from bit field	2022-05-06 10:46:40 -04:00
Beat Küng	8cff9a1e04	commander: fix incorrect return in set_link_loss_nav_state() If both local position and altitude were not valid, then both RC loss and datalink loss would not trigger any failsafe at all, independently from the configured action.	2022-05-06 10:15:30 -04:00
bresch	f8ff34f82d	ekf2: optimize KHP computation Calculating K(HP) takes less operations than (KH)P because K and H are vectors. Without considering the sparsity optimization: - KH (2424 operations) is then a 24x24 matrix an it takes 24^3 operations to multiply it with P. Total: 14400 op - HP (24(24+24-1) operations) is a row vector and it takes 24 operations to left-multiply it by K. Total:1152 op	2022-05-06 10:15:26 -04:00
Beat Küng	e69d9ec48f	dshot: avoid using pwm failsafe params when dynamic mixing is enabled	2022-05-02 11:43:51 +02:00
Beat Küng	f033e164fe	fix dshot: remove setAllFailsafeValues Fixes a regression from `c1e5e666f0`, where with static mixers the dshot outputs would go to max instead of 0 in a failsafe case.	2022-04-28 13:29:40 -04:00
Daniel Agar	41191765ad	drivers/rc_input: RC_INPUT_PROTO parameter minimal implementation (#19539 ) Co-authored-by: chris1seto <chris12892@gmail.com> Co-authored-by: chris1seto <chris12892@gmail.com>	2022-04-28 13:27:15 -04:00