tfmini_i2c: add Kconfig

- CONFIG_SEM_PREALLOCHOLDERS=32
 - CONFIG_SEM_NNESTPRIO=16 (default)

.ci/Jenkinsfile-compile

@@ -28,7 +28,7 @@ pipeline {
           ]
 
           def base_builds = [
-            target: ["px4_sitl_rtps"],
+            target: ["px4_sitl_default"],
             image: docker_images.base,
             archive: false
           ]
@@ -52,12 +52,14 @@ pipeline {
                      "cuav_x7pro_default",
                      "cubepilot_cubeorange_default",
                      "cubepilot_cubeyellow_default",
+                     "diatone_mamba-f405-mk2_default",
                      "freefly_can-rtk-gps_canbootloader",
                      "freefly_can-rtk-gps_default",
                      "holybro_can-gps-v1_canbootloader",
                      "holybro_can-gps-v1_default",
                      "holybro_durandal-v1_default",
                      "holybro_kakutef7_default",
+                     "holybro_kakuteh7_default",
                      "holybro_pix32v5_default",
                      "matek_h743-slim",
                      "matek_gnss-m9n-f4_canbootloader",
@@ -100,9 +102,11 @@ pipeline {
                      "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",
+                     "sky-drones_smartap-airlink_default",
                      "spracing_h7extreme_default",
                      "uvify_core_default"
             ],

.ci/Jenkinsfile-hardware

@@ -705,18 +705,21 @@ void quickCalibrate() {
 
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "gyro_calibration status || true"'
 
-  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate accel quick"'
+  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate accel quick; sleep 1"'
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_ACC*"'
 
-  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate gyro"'
+  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate gyro; sleep 2"'
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_GYRO*"'
 
-  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate level"'
+  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate level; sleep 2"'
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show SENS*"'
 
-  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate mag quick"'
+  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate mag quick; sleep 1"'
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_MAG*"'
 
+  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "commander calibrate baro; sleep 5"'
+  sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_BARO*"'
+
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "param show CAL_*"' // parameters after
   sh './Tools/HIL/run_nsh_cmd.py --device `find /dev/serial -name *usb-*` --cmd "sensors status"'
 }

.github/workflows/compile_nuttx.yml

@@ -20,6 +20,7 @@ jobs:
           ark_can-flow,
           ark_can-gps,
           ark_can-rtk-gps,
+          ark_cannode,
           atl_mantis-edu,
           av_x-v1,
           bitcraze_crazyflie,
@@ -29,6 +30,7 @@ jobs:
           cuav_x7pro,
           cubepilot_cubeorange,
           cubepilot_cubeyellow,
+          diatone_mamba-f405-mk2,
           freefly_can-rtk-gps,
           holybro_can-gps-v1,
           holybro_durandal-v1,
@@ -58,8 +60,10 @@ jobs:
           px4_fmu-v4pro,
           px4_fmu-v5,
           px4_fmu-v5x,
+          px4_fmu-v6c,
           px4_fmu-v6u,
           px4_fmu-v6x,
+          sky-drones_smartap-airlink,
           spracing_h7extreme,
           uvify_core
           ]

.github/workflows/sitl_tests.yml

@@ -29,9 +29,9 @@ jobs:
         token: ${{ secrets.ACCESS_TOKEN }}
 
     - name: Download MAVSDK
-      run: wget "https://github.com/mavlink/MAVSDK/releases/download/v$(cat test/mavsdk_tests/MAVSDK_VERSION)/mavsdk_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
+      run: wget "https://github.com/mavlink/MAVSDK/releases/download/v$(cat test/mavsdk_tests/MAVSDK_VERSION)/libmavsdk-dev_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
     - name: Install MAVSDK
-      run: dpkg -i "mavsdk_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
+      run: dpkg -i "libmavsdk-dev_$(cat test/mavsdk_tests/MAVSDK_VERSION)_ubuntu20.04_amd64.deb"
 
     - name: Prepare ccache timestamp
       id: ccache_cache_timestamp

.gitmodules

@@ -64,3 +64,6 @@
 	path = src/lib/crypto/libtommath
 	url = https://github.com/PX4/libtommath.git
 	branch = px4
+[submodule "src/modules/microdds_client/Micro-XRCE-DDS-Client"]
+	path = src/modules/microdds_client/Micro-XRCE-DDS-Client
+	url = https://github.com/eProsima/Micro-XRCE-DDS-Client.git

.vscode/.gitignore

@@ -9,3 +9,5 @@ launch.json
 ipch/
 
 browse.vc.db*
+
+*.log

.vscode/cmake-variants.yaml

@@ -121,6 +121,16 @@ CONFIG:
       buildType: MinSizeRel
       settings:
         CONFIG: ark_can-rtk-gps_canbootloader
+    ark_cannode_default:
+      short: ark_cannode_default
+      buildType: MinSizeRel
+      settings:
+        CONFIG: ark_cannode_default
+    ark_cannode_canbootloader:
+      short: ark_cannode_canbootloader
+      buildType: MinSizeRel
+      settings:
+        CONFIG: ark_cannode_canbootloader
     atl_mantis-edu_default:
       short: atl_mantis-edu
       buildType: MinSizeRel

CMakeLists.txt

@@ -412,6 +412,7 @@ endif()
 # subdirectories
 #
 add_library(parameters_interface INTERFACE)
+add_library(kernel_parameters_interface INTERFACE)
 
 include(px4_add_library)
 add_subdirectory(src/lib EXCLUDE_FROM_ALL)
@@ -434,7 +435,13 @@ add_subdirectory(src/lib/metadata EXCLUDE_FROM_ALL)
 
 # must be the last module before firmware
 add_subdirectory(src/lib/parameters EXCLUDE_FROM_ALL)
+
+if(${PX4_PLATFORM} STREQUAL "nuttx" AND NOT CONFIG_BUILD_FLAT)
+target_link_libraries(parameters_interface INTERFACE usr_parameters)
+target_link_libraries(kernel_parameters_interface INTERFACE parameters)
+else()
 target_link_libraries(parameters_interface INTERFACE parameters)
+endif()
 
 # firmware added last to generate the builtin for included modules
 add_subdirectory(platforms/${PX4_PLATFORM})

Makefile

@@ -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-slim_bootloader modalai_fc-v2_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

ROMFS/cannode/init.d/rcS

@@ -88,7 +88,7 @@ unset BOARD_RC_SENSORS
 # Check for flow sensor
 if param compare SENS_EN_PX4FLOW 1
 then
-	px4flow start -X
+	px4flow start -X &
 fi
 
 uavcannode start

ROMFS/px4fmu_common/init.d-posix/airframes/1011_iris_irlock

@@ -10,6 +10,7 @@
 # enable fusion of landing target velocity
 param set-default LTEST_MODE 1
 param set-default PLD_HACC_RAD 0.1
+param set-default RTL_PLD_MD 2
 
 # Start up Landing Target Estimator module
 landing_target_estimator start

ROMFS/px4fmu_common/init.d-posix/airframes/1020_uuv_generic

@@ -8,8 +8,5 @@
 # disable circuit breaker for airspeed sensor
 param set-default CBRK_AIRSPD_CHK 162128
 
-set MAV_TYPE 12
-param set MAV_TYPE ${MAV_TYPE}
-
 set MIXER_FILE etc/mixers-sitl/uuv_x_sitl.main.mix
 set MIXER custom

ROMFS/px4fmu_common/init.d-posix/airframes/1021_uuv_hippocampus

@@ -8,8 +8,5 @@
 # disable circuit breaker for airspeed sensor
 param set-default CBRK_AIRSPD_CHK 162128
 
-set MAV_TYPE 12
-param set MAV_TYPE ${MAV_TYPE}
-
 set MIXER_FILE etc/mixers-sitl/uuv_x_sitl.main.mix
 set MIXER custom

ROMFS/px4fmu_common/init.d-posix/airframes/1022_uuv_bluerov2_heavy

@@ -67,4 +67,3 @@ param set-default PWM_MAIN_FUNC7 107
 param set-default PWM_MAIN_FUNC8 108
 
 set MIXER skip
-

ROMFS/px4fmu_common/init.d-posix/airframes/1040_standard_vtol

@@ -71,7 +71,6 @@ param set-default MPC_XY_VEL_I_ACC 4
 param set-default MPC_XY_VEL_D_ACC 0.1
 
 param set-default NAV_ACC_RAD 5
-param set-default NAV_LOITER_RAD 80
 
 param set-default VT_FWD_THRUST_EN 4
 param set-default VT_F_TRANS_THR 0.75
@@ -80,7 +79,5 @@ param set-default VT_FW_MOT_OFFID 1234
 param set-default VT_B_TRANS_DUR 8
 param set-default VT_TYPE 2
 
-set MAV_TYPE 22
-
 set MIXER_FILE etc/mixers-sitl/standard_vtol_sitl.main.mix
 set MIXER custom

ROMFS/px4fmu_common/init.d-posix/airframes/1041_tailsitter

@@ -7,6 +7,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 20
+
 # param set-default SYS_CTRL_ALLOC 1
 param set-default CA_AIRFRAME 4
 
@@ -68,7 +70,6 @@ param set-default MPC_XY_VEL_I_ACC 4
 param set-default MPC_XY_VEL_D_ACC 0.1
 
 param set-default NAV_ACC_RAD 5
-param set-default NAV_LOITER_RAD 80
 
 param set-default VT_FW_DIFTHR_EN 1
 param set-default VT_FW_DIFTHR_SC 0.5
@@ -78,7 +79,5 @@ param set-default VT_TYPE 0
 
 param set-default WV_EN 0
 
-set MAV_TYPE 20
-
 set MIXER_FILE etc/mixers-sitl/quad_x_vtol.main.mix
 set MIXER custom

ROMFS/px4fmu_common/init.d-posix/airframes/1042_tiltrotor

@@ -7,6 +7,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 21
+
 # param set-default SYS_CTRL_ALLOC 1
 param set-default CA_AIRFRAME 3
 
@@ -80,7 +82,6 @@ param set-default MPC_XY_VEL_I_ACC 4
 param set-default MPC_XY_VEL_D_ACC 0.1
 
 param set-default NAV_ACC_RAD 5
-param set-default NAV_LOITER_RAD 80
 
 param set-default VT_B_TRANS_DUR 8
 param set-default VT_FWD_THRUST_EN 4
@@ -88,7 +89,5 @@ param set-default VT_MOT_ID 1234
 param set-default VT_TILT_TRANS 0.6
 param set-default VT_TYPE 1
 
-set MAV_TYPE 21
-
 set MIXER_FILE etc/mixers-sitl/tiltrotor_sitl.main.mix
 set MIXER custom

ROMFS/px4fmu_common/init.d-posix/airframes/1043_standard_vtol_drop

@@ -38,7 +38,6 @@ param set-default MPC_XY_VEL_I_ACC 4
 param set-default MPC_XY_VEL_D_ACC 0.1
 
 param set-default NAV_ACC_RAD 5
-param set-default NAV_LOITER_RAD 80
 
 param set-default VT_FWD_THRUST_EN 4
 param set-default VT_F_TRANS_THR 0.75
@@ -51,7 +50,5 @@ param set-default RC_MAP_AUX1 8
 param set-default RC_MAP_AUX2 9
 param set-default RC_MAP_AUX3 10
 
-set MAV_TYPE 22
-
 set MIXER_FILE etc/mixers-sitl/standard_vtol_sitl.main.mix
 set MIXER custom

ROMFS/px4fmu_common/init.d-posix/airframes/1060_rover

@@ -37,6 +37,4 @@ param set-default PWM_MAIN_FUNC2 201
 param set-default PWM_MAIN_FUNC6 101
 param set-default PWM_MAIN_FUNC7 101
 
-set MAV_TYPE 10
-
 set MIXER_FILE skip

ROMFS/px4fmu_common/init.d-posix/airframes/1061_r1_rover

@@ -37,6 +37,4 @@ param set-default PWM_MAIN_FUNC2 101
 param set-default PWM_MAIN_FUNC6 102
 param set-default PWM_MAIN_FUNC7 102
 
-set MAV_TYPE 10
-
 set MIXER_FILE skip

ROMFS/px4fmu_common/init.d-posix/airframes/1062_tf-r1

@@ -10,6 +10,8 @@
 
 . ${R}etc/init.d/rc.rover_defaults
 
+param set-default MAV_TYPE 10
+
 param set-default GND_L1_DIST 5
 param set-default GND_SP_CTRL_MODE 1
 param set-default GND_SPEED_D 3
@@ -33,6 +35,4 @@ param set-default CBRK_AIRSPD_CHK 162128
 param set-default GND_MAX_ANG 0.6
 param set-default GND_WHEEL_BASE 3.0
 
-set MAV_TYPE 10
-
 set MIXER_FILE etc/mixers-sitl/rover_ackermann_sitl.main.mix

ROMFS/px4fmu_common/init.d-posix/airframes/1070_boat

@@ -47,6 +47,4 @@ param set-default CA_R_REV 3
 param set-default PWM_MAIN_FUNC1 101
 param set-default PWM_MAIN_FUNC2 102
 
-set MAV_TYPE 11
-
 set MIXER skip

ROMFS/px4fmu_common/init.d-posix/airframes/3011_hexarotor_x

@@ -9,6 +9,8 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+param set-default MAV_TYPE 13
+
 param set-default MC_PITCHRATE_P 0.1
 param set-default MC_PITCHRATE_I 0.05
 param set-default MC_PITCH_P 6.0
@@ -24,6 +26,4 @@ param set-default TRIG_MODE 4
 param set-default MNT_MODE_IN 4
 param set-default MNT_DO_STAB 2
 
-set MAV_TYPE 13
-
 set MIXER hexa_x

ROMFS/px4fmu_common/init.d-posix/airframes/6011_typhoon_h480

@@ -7,6 +7,8 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+param set-default MAV_TYPE 13
+
 param set-default MC_PITCHRATE_P 0.0800
 param set-default MC_PITCHRATE_I 0.0400
 param set-default MC_PITCHRATE_D 0.0010
@@ -26,6 +28,4 @@ param set-default MNT_MODE_IN 4
 param set-default MNT_MODE_OUT 2
 param set-default MAV_PROTO_VER 2
 
-set MAV_TYPE 13
-
 set MIXER hexa_x

ROMFS/px4fmu_common/init.d-posix/airframes/6012_typhoon_h480_ctrlalloc

@@ -7,6 +7,8 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+param set-default MAV_TYPE 13
+
 param set-default SYS_CTRL_ALLOC 1
 
 param set-default MC_PITCHRATE_P 0.0800
@@ -58,7 +60,5 @@ param set-default PWM_MAIN_FUNC4 104
 param set-default PWM_MAIN_FUNC5 105
 param set-default PWM_MAIN_FUNC6 106
 
-set MAV_TYPE 13
-
 set MIXER skip
 set MIXER_AUX none

ROMFS/px4fmu_common/init.d-posix/rcS

@@ -24,7 +24,6 @@ fi
 
 # initialize script variables
 set IO_PRESENT                  no
-set MAV_TYPE                    none
 set MIXER                       none
 set MIXER_AUX                   none
 set MIXER_FILE                  none
@@ -224,6 +223,13 @@ rc_update start
 manual_control start
 sensors start
 commander start
+
+# Configure vehicle type specific parameters.
+# Note: rc.vehicle_setup is the entry point for rc.interface,
+#       rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
+#
+. ${R}etc/init.d/rc.vehicle_setup
+
 navigator start
 
 # Try to start the micrortps_client with UDP transport if module exists
@@ -253,12 +259,6 @@ then
 	gyro_calibration start
 fi
 
-# Configure vehicle type specific parameters.
-# Note: rc.vehicle_setup is the entry point for rc.interface,
-#       rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
-#
-. ${R}etc/init.d/rc.vehicle_setup
-
 #user defined mavlink streams for instances can be in PATH
 . px4-rc.mavlink
 

ROMFS/px4fmu_common/init.d/airframes/1000_rc_fw_easystar.hil

@@ -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

ROMFS/px4fmu_common/init.d/airframes/10017_steadidrone_qu4d

@@ -36,4 +36,5 @@ 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

ROMFS/px4fmu_common/init.d/airframes/1001_rc_quad_x.hil

@@ -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

ROMFS/px4fmu_common/init.d/airframes/1002_standard_vtol.hil

@@ -49,7 +49,6 @@ param set-default MPC_Z_VEL_MAX_DN 1.5
 
 param set-default NAV_ACC_RAD 5
 param set-default NAV_DLL_ACT 2
-param set-default NAV_LOITER_RAD 80
 
 param set-default RTL_DESCEND_ALT 10
 param set-default RTL_RETURN_ALT 30
@@ -95,6 +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
@@ -104,7 +105,7 @@ param set-default CBRK_SUPPLY_CHK 894281
 param set-default COM_PREARM_MODE 0
 param set-default CBRK_IO_SAFETY 22027
 
-set MAV_TYPE 22
+param set-default MAV_TYPE 22
 
 set MIXER standard_vtol_hitl
 

ROMFS/px4fmu_common/init.d/airframes/1102_tailsitter_duo_sih.hil

@@ -47,7 +47,7 @@ param set-default HIL_ACT_FUNC6 201
 param set-default HIL_ACT_REV 32
 
 param set-default MAV_TYPE 19
-set MAV_TYPE 19
+
 set MIXER vtol_tailsitter_duo_sat
 
 set PWM_OUT 1234

ROMFS/px4fmu_common/init.d/airframes/13000_generic_vtol_standard

@@ -54,7 +54,8 @@ param set-default PWM_AUX_DIS5 950
 param set-default VT_TYPE 2
 param set-default VT_MOT_ID 1234
 param set-default VT_FW_MOT_OFFID 1234
-set MAV_TYPE 22
+
+param set-default MAV_TYPE 22
 
 set MIXER quad_x
 set MIXER_AUX vtol_AAERT

ROMFS/px4fmu_common/init.d/airframes/13001_caipirinha_vtol

@@ -19,7 +19,6 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
-
 param set-default MAV_TYPE 19
 
 param set-default MC_ROLL_P 6
@@ -38,7 +37,6 @@ param set-default VT_IDLE_PWM_MC  1080
 param set-default VT_ELEV_MC_LOCK 0
 param set-default VT_MOT_ID 12
 param set-default VT_TYPE 0
-set MAV_TYPE 19
 
 set MIXER vtol_tailsitter_duo
 

ROMFS/px4fmu_common/init.d/airframes/13002_firefly6

@@ -23,6 +23,7 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 21
 
 param set-default MC_ROLL_P 7
 param set-default MC_ROLLRATE_P 0.19
@@ -45,7 +46,6 @@ param set-default VT_TILT_TRANS 0.5
 param set-default VT_TILT_FW 0.9
 param set-default VT_ELEV_MC_LOCK 0
 param set-default VT_TYPE 1
-set MAV_TYPE 21
 
 set MIXER firefly6
 set MIXER_AUX firefly6

ROMFS/px4fmu_common/init.d/airframes/13003_quad_tailsitter

@@ -13,6 +13,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 20
+
 param set-default CA_AIRFRAME 4
 param set-default CA_ROTOR_COUNT 4
 param set-default CA_ROTOR0_PX 0.15
@@ -38,7 +40,6 @@ param set-default PWM_MAIN_MAX 2000
 param set-default VT_MOT_ID 1234
 param set-default VT_IDLE_PWM_MC  1080
 param set-default VT_TYPE 0
-set MAV_TYPE 20
 
 set MIXER quad_x_vtol
 

ROMFS/px4fmu_common/init.d/airframes/13004_quad+_tailsitter

@@ -7,8 +7,8 @@
 #
 # @output MAIN1 motor 1
 # @output MAIN2 motor 2
-# @output MAIN3 motor 4
-# @output MAIN4 motor 5
+# @output MAIN3 motor 3
+# @output MAIN4 motor 4
 # @output MAIN5 elevon left
 # @output MAIN6 elevon right
 # @output MAIN7 canard surface
@@ -22,13 +22,13 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 20
+
 param set-default PWM_MAIN_MAX 2000
 
 param set-default VT_IDLE_PWM_MC  1080
 param set-default VT_TYPE 0
 
-set MAV_TYPE 20
-
 set MIXER quad_+_vtol
 
 set PWM_OUT 1234

ROMFS/px4fmu_common/init.d/airframes/13005_vtol_AAERT_quad

@@ -52,7 +52,6 @@ param set-default VT_MOT_ID 1234
 param set-default VT_FW_MOT_OFFID 1234
 param set-default VT_IDLE_PWM_MC 1080
 param set-default VT_TYPE 2
-set MAV_TYPE 22
 
 set MIXER quad_x
 set MIXER_AUX vtol_AAERT

ROMFS/px4fmu_common/init.d/airframes/13006_vtol_standard_delta

@@ -41,7 +41,6 @@ param set-default VT_FW_MOT_OFFID 1234
 param set-default VT_F_TRANS_THR 0.75
 param set-default VT_IDLE_PWM_MC 1080
 param set-default VT_TYPE 2
-set MAV_TYPE 22
 
 set MIXER quad_x
 set MIXER_AUX vtol_delta

ROMFS/px4fmu_common/init.d/airframes/13007_vtol_AAVVT_quad

@@ -33,7 +33,6 @@ param set-default VT_MOT_ID 1234
 param set-default VT_FW_MOT_OFFID 1234
 param set-default VT_IDLE_PWM_MC 1080
 param set-default VT_TYPE 2
-set MAV_TYPE 22
 
 set MIXER quad_x
 set MIXER_AUX vtol_AAVVT

ROMFS/px4fmu_common/init.d/airframes/13008_QuadRanger

@@ -46,7 +46,6 @@ param set-default VT_IDLE_PWM_MC 1080
 param set-default VT_MOT_ID 1234
 param set-default VT_FW_MOT_OFFID 1234
 param set-default VT_TYPE 2
-set MAV_TYPE 22
 
 set MIXER quad_x
 set MIXER_AUX vtol_AAERT

ROMFS/px4fmu_common/init.d/airframes/13009_vtol_spt_ranger

@@ -77,8 +77,6 @@ param set-default VT_TRANS_MIN_TM 5
 param set-default VT_TRANS_TIMEOUT    30
 param set-default VT_TYPE 2
 
-set MAV_TYPE 22
-
 set MIXER quad_x
 set MIXER_AUX vtol_AAERT
 

ROMFS/px4fmu_common/init.d/airframes/13010_claire

@@ -13,6 +13,8 @@
 
 . ${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
@@ -28,7 +30,6 @@ param set-default VT_TILT_MC 0.08
 param set-default VT_TILT_TRANS 0.5
 param set-default VT_ELEV_MC_LOCK 0
 param set-default VT_TYPE 1
-set MAV_TYPE 21
 
 set MIXER claire
 set MIXER_AUX claire

ROMFS/px4fmu_common/init.d/airframes/13012_convergence

@@ -22,6 +22,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 21
+
 param set-default CBRK_AIRSPD_CHK 162128
 
 param set-default FW_ARSP_MODE 1
@@ -64,7 +66,6 @@ param set-default VT_TRANS_MIN_TM 1.2
 param set-default VT_TRANS_P2_DUR 1.3
 param set-default VT_ELEV_MC_LOCK 0
 param set-default VT_TYPE 1
-set MAV_TYPE 21
 
 set MIXER vtol_convergence
 

ROMFS/px4fmu_common/init.d/airframes/13013_deltaquad

@@ -22,6 +22,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 22
+
 param set-default BAT1_CAPACITY 23000
 param set-default BAT1_N_CELLS 4
 param set-default BAT1_R_INTERNAL 0.0025
@@ -134,7 +136,6 @@ param set-default VT_TRANS_TIMEOUT 22
 param set-default VT_F_TRANS_RAMP 4
 
 param set-default COM_RC_OVERRIDE 0
-set MAV_TYPE 22
 
 set MIXER deltaquad
 set MIXER_AUX pass

ROMFS/px4fmu_common/init.d/airframes/13014_vtol_babyshark

@@ -23,6 +23,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 22
+
 param set-default BAT1_N_CELLS 6
 
 param set-default FW_AIRSPD_MAX 30
@@ -94,8 +96,6 @@ param set-default VT_PSHER_RMP_DT 2
 param set-default VT_TRANS_MIN_TM 4
 param set-default VT_TYPE 2
 
-set MAV_TYPE 22
-
 set MIXER babyshark
 set MIXER_AUX pass
 

ROMFS/px4fmu_common/init.d/airframes/13030_generic_vtol_quad_tiltrotor

@@ -27,6 +27,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 21
+
 param set-default VT_IDLE_PWM_MC 1100
 param set-default VT_TYPE 1
 param set-default VT_MOT_ID 1234
@@ -57,8 +59,6 @@ param set-default CA_SV_CS3_TRQ_Y 1.0
 param set-default CA_SV_CS3_TYPE 4
 param set-default CA_SV_TL_COUNT 4
 
-set MAV_TYPE 21
-
 set MIXER quad_x
 set MIXER_AUX vtol_TTTTAAER
 

ROMFS/px4fmu_common/init.d/airframes/13050_generic_vtol_octo

@@ -31,7 +31,6 @@ param set-default PWM_AUX_DIS5 950
 param set-default VT_TYPE 2
 param set-default VT_MOT_ID 12345678
 param set-default VT_FW_MOT_OFFID 12345678
-set MAV_TYPE 22
 
 set MIXER octo_cox
 set MIXER_AUX vtol_AAERT

ROMFS/px4fmu_common/init.d/airframes/13200_generic_vtol_tailsitter

@@ -19,6 +19,8 @@
 
 . ${R}etc/init.d/rc.vtol_defaults
 
+param set-default MAV_TYPE 19
+
 param set-default VT_ELEV_MC_LOCK 0
 param set-default VT_MOT_COUNT 2
 param set-default VT_TYPE 0
@@ -37,8 +39,6 @@ param set-default CA_SV_CS1_TRQ_P 0.5
 param set-default CA_SV_CS1_TRQ_Y -0.5
 param set-default CA_SV_CS1_TYPE 6
 
-param set-default MAV_TYPE 19
-set MAV_TYPE 19
 set MIXER vtol_tailsitter_duo
 
 set PWM_OUT 1234

ROMFS/px4fmu_common/init.d/airframes/14001_tri_y_yaw+

@@ -18,4 +18,7 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+# MAV_TYPE_TRICOPTER 15
+param set-default MAV_TYPE 15
+
 set MIXER tri_y_yaw+

ROMFS/px4fmu_common/init.d/airframes/14002_tri_y_yaw-

@@ -18,4 +18,7 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+# MAV_TYPE_TRICOPTER 15
+param set-default MAV_TYPE 15
+
 set MIXER tri_y_yaw-

ROMFS/px4fmu_common/init.d/airframes/15001_coax_heli

@@ -17,7 +17,9 @@
 #
 
 . ${R}etc/init.d/rc.mc_defaults
-set MIXER coax
+
+# MAV_TYPE_COAXIAL 3
+param set-default MAV_TYPE 3
 
 param set-default MC_ROLLRATE_P 0.17
 param set-default MC_ROLLRATE_I 0.05
@@ -36,6 +38,9 @@ param set-default PWM_MAIN_RATE 400
 
 param set-default RTL_RETURN_ALT 30
 param set-default RTL_DESCEND_ALT 10
+
+set MIXER coax
+
 # This is the gimbal pass mixer
 set MIXER_AUX pass
 

ROMFS/px4fmu_common/init.d/airframes/16001_helicopter

@@ -20,7 +20,7 @@
 . ${R}etc/init.d/rc.mc_defaults
 
 # Configure as helicopter (number 4 defined in commander_helper.cpp)
-set MAV_TYPE 4
+param set-default MAV_TYPE 4
 
 set MIXER blade130
 

ROMFS/px4fmu_common/init.d/airframes/17003_TF-G2

@@ -41,5 +41,6 @@ param set-default FW_R_LIM 40
 param set-default FW_P_LIM_MAX 25
 param set-default FW_P_LIM_MIN -5
 param set-default FW_P_RMAX_NEG 20
+
 set MIXER TF-G2
 set MIXER_AUX pass

ROMFS/px4fmu_common/init.d/airframes/18001_TF-B1

@@ -24,8 +24,5 @@ param set-default MAV_0_CONFIG 102
 param set-default GPS_UBX_DYNMODEL 8
 param set-default SER_TEL2_BAUD 9600
 
-set MAV_TYPE 8
-param set MAV_TYPE ${MAV_TYPE}
-
 set MIXER IO_pass
 set MIXER_AUX pass

ROMFS/px4fmu_common/init.d/airframes/24001_dodeca_cox

@@ -26,7 +26,7 @@
 # @board px4_fmu-v2 exclude
 #
 
-set VEHICLE_TYPE mc
+. ${R}etc/init.d/rc.mc_defaults
 
 param set-default NAV_ACC_RAD 2
 
@@ -39,6 +39,7 @@ param set-default PWM_MAIN_RATE 400
 
 param set-default RTL_DESCEND_ALT 10
 param set-default RTL_RETURN_ALT 30
+
 set MIXER dodeca_top_cox
 set MIXER_AUX dodeca_bottom_cox
 

ROMFS/px4fmu_common/init.d/airframes/3033_wingwing

@@ -41,9 +41,6 @@ param set-default FW_RR_P 0.04
 
 param set-default PWM_MAIN_DISARM 1000
 
-# Configure this as plane.
-set MAV_TYPE 1
-
 # Set mixer.
 set MIXER fw_generic_wing
 

ROMFS/px4fmu_common/init.d/airframes/4051_s250aq

@@ -24,8 +24,6 @@
 
 set MIXER quad_s250aq
 
-set MAV_TYPE 2
-
 param set-default ATT_BIAS_MAX 0
 
 param set-default CBRK_IO_SAFETY 22027

ROMFS/px4fmu_common/init.d/airframes/4061_atl_mantis_edu

@@ -164,6 +164,8 @@ param set-default RC_MAP_AUX2       5
 param set-default RC_MAP_AUX3       10
 param set-default RC_MAP_AUX4       8
 param set-default RC_MAP_FLTMODE    6
+param set-default RC_MAP_RETURN_SW  7
+
 param set-default RC1_TRIM          1000
 
 

ROMFS/px4fmu_common/init.d/airframes/4071_ifo

@@ -21,10 +21,7 @@
 # @board cuav_x7pro exclude
 #
 
-set VEHICLE_TYPE mc
-set MIXER quad_x
-set PWM_OUT 1234
-
+. ${R}etc/init.d/rc.mc_defaults
 
 # Attitude & rate gains
 param set-default MC_ROLLRATE_D 0.0013

ROMFS/px4fmu_common/init.d/airframes/4073_ifo-s

@@ -21,10 +21,7 @@
 # @maintainer Hyon Lim <lim@uvify.com>
 #
 
-set VEHICLE_TYPE mc
-set MIXER quad_x
-set PWM_OUT 1234
-
+. ${R}etc/init.d/rc.mc_defaults
 
 # Attitude & rate gains
 param set-default MC_ROLLRATE_D 0.0013

ROMFS/px4fmu_common/init.d/airframes/4100_tiltquadrotor

@@ -24,10 +24,6 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
-
-# Configure this as Quadrotor
-# set MAV_TYPE 14
-
 # Set mixer
 set MIXER tilt_quad
 set MIXER_AUX tilt_quad

ROMFS/px4fmu_common/init.d/airframes/50000_generic_ground_vehicle

@@ -48,8 +48,6 @@ param set-default NAV_ACC_RAD 0.5
 param set-default PWM_MAIN_DISARM 1500
 param set-default PWM_MAIN_MAX 2000
 param set-default PWM_MAIN_MIN 1000
-# Configure this as rover
-set MAV_TYPE 10
 
 # Set mixer
 set MIXER rover_generic

ROMFS/px4fmu_common/init.d/airframes/50003_aion_robotics_r1_rover

@@ -76,9 +76,6 @@ param set-default RBCLW_SER_CFG 104
 # Start this driver after setting parameters, because the driver uses some of those parameters.
 # roboclaw start /dev/ttyS3
 
-# Configure this as rover
-set MAV_TYPE 10
-
 # Set mixer
 set MIXER generic_diff_rover
 

ROMFS/px4fmu_common/init.d/airframes/50004_nxpcup_car_dfrobot_gpx

@@ -65,9 +65,6 @@ param set-default PWM_MAIN_MIN4 970
 # Enable Airspeed check circuit breaker because Rovers will have no airspeed sensor
 param set-default CBRK_AIRSPD_CHK 162128
 
-# Configure this as rover
-set MAV_TYPE 10
-
 # Set mixer
 set MIXER rover_diff_and_servo
 

ROMFS/px4fmu_common/init.d/airframes/60000_uuv_generic

@@ -16,7 +16,4 @@
 # disable circuit breaker for airspeed sensor
 param set-default CBRK_AIRSPD_CHK 162128
 
-set MAV_TYPE 12
-param set MAV_TYPE ${MAV_TYPE}
-
 set MIXER uuv_x

ROMFS/px4fmu_common/init.d/airframes/60001_uuv_hippocampus

@@ -16,7 +16,4 @@
 # disable circuit breaker for airspeed sensor
 param set-default CBRK_AIRSPD_CHK 162128
 
-set MAV_TYPE 12
-param set MAV_TYPE ${MAV_TYPE}
-
 set MIXER uuv_x

ROMFS/px4fmu_common/init.d/airframes/6001_hexa_x

@@ -23,6 +23,9 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+# MAV_TYPE_HEXAROTOR 13
+param set-default MAV_TYPE 13
+
 param set-default CA_ROTOR_COUNT 6
 param set-default CA_ROTOR0_PX 0.0
 param set-default CA_ROTOR0_PY 0.5

ROMFS/px4fmu_common/init.d/airframes/6002_draco_r

@@ -27,9 +27,8 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
-set MIXER hexa_x
-set PWM_OUT 12345678
-
+# MAV_TYPE_HEXAROTOR 13
+param set-default MAV_TYPE 13
 
 ###############################################
 # Attitude & rate gains
@@ -120,3 +119,7 @@ param set-default MAV_1_MODE 2
 param set-default MAV_1_FORWARD 1
 param set-default MAV_1_RATE 800000
 param set-default SER_TEL2_BAUD 921600
+
+
+set MIXER hexa_x
+set PWM_OUT 12345678

ROMFS/px4fmu_common/init.d/airframes/7001_hexa_+

@@ -23,6 +23,9 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+# MAV_TYPE_HEXAROTOR 13
+param set-default MAV_TYPE 13
+
 param set-default CA_ROTOR_COUNT 6
 param set-default CA_ROTOR0_PX 0.5
 param set-default CA_ROTOR0_PY 0.0

ROMFS/px4fmu_common/init.d/airframes/8001_octo_x

@@ -25,6 +25,9 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+# MAV_TYPE_OCTOROTOR 14
+param set-default MAV_TYPE 14
+
 param set-default CA_ROTOR_COUNT 8
 param set-default CA_ROTOR0_KM -0.05
 param set-default CA_ROTOR0_PX 0.46

ROMFS/px4fmu_common/init.d/airframes/9001_octo_+

@@ -25,6 +25,9 @@
 
 . ${R}etc/init.d/rc.mc_defaults
 
+# MAV_TYPE_OCTOROTOR 14
+param set-default MAV_TYPE 14
+
 set MIXER octo_+
 
 set PWM_OUT 12345678

ROMFS/px4fmu_common/init.d/rc.airship_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE airship
 
+# MAV_TYPE_AIRSHIP 7
+param set-default MAV_TYPE 7
+
 #
 # This is the gimbal pass mixer.
 #

ROMFS/px4fmu_common/init.d/rc.balloon_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE fw
 
+# MAV_TYPE_FREE_BALLOON 8
+param set-default MAV_TYPE 8
+
 #
 # Default parameters for balloon UAVs.
 #

ROMFS/px4fmu_common/init.d/rc.boat_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE rover
 
+# MAV_TYPE_SURFACE_BOAT 11
+param set-default MAV_TYPE 11
+
 #
 # Default parameters for UGVs.
 #

ROMFS/px4fmu_common/init.d/rc.fw_defaults

@@ -7,14 +7,15 @@
 
 set VEHICLE_TYPE fw
 
+# MAV_TYPE_FIXED_WING 1
+param set-default MAV_TYPE 1
+
 #
 # Default parameters for fixed wing UAVs.
 #
 param set-default COM_POS_FS_DELAY 5
 param set-default COM_POS_FS_EPH 15
 param set-default COM_POS_FS_EPV 30
-param set-default COM_POS_FS_GAIN 0
-param set-default COM_POS_FS_PROB 1
 param set-default COM_VEL_FS_EVH 5
 # Disable preflight disarm to not interfere with external launching
 param set-default COM_DISARM_PRFLT -1

ROMFS/px4fmu_common/init.d/rc.mc_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE mc
 
+# MAV_TYPE_QUADROTOR 2
+param set-default MAV_TYPE 2
+
 if param compare IMU_GYRO_RATEMAX 400
 then
 	param set-default IMU_GYRO_RATEMAX 800

ROMFS/px4fmu_common/init.d/rc.rover_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE rover
 
+# MAV_TYPE_GROUND_ROVER 10
+param set-default MAV_TYPE 10
+
 #
 # Default parameters for UGVs.
 #

ROMFS/px4fmu_common/init.d/rc.sensors

@@ -58,6 +58,11 @@ then
 	pga460 start
 fi
 
+if param greater -s SENS_EN_TFI2C 0
+then
+	tfmini_i2c start -X
+fi
+
 # Lightware i2c lidar sensor
 if param greater -s SENS_EN_SF1XX 0
 then
@@ -83,18 +88,24 @@ then
 	teraranger start -X
 fi
 
-# Possible external pmw3901 optical flow sensor
-if param greater -s SENS_EN_PMW3901 0
+# paa3905 optical flow sensor (external SPI)
+if param greater -s SENS_EN_PAA3905 0
 then
-	pmw3901 -S start
+	paa3905 -S start
 fi
 
-# Possible external paw3902 optical flow sensor
+# paw3902 optical flow sensor (external SPI)
 if param greater -s SENS_EN_PAW3902 0
 then
 	paw3902 -S start
 fi
 
+# pmw3901 optical flow sensor (external SPI)
+if param greater -s SENS_EN_PMW3901 0
+then
+	pmw3901 -S start
+fi
+
 # vl53l1x i2c distance sensor
 if param compare -s SENS_EN_VL53L1X 1
 then
@@ -123,30 +134,36 @@ fi
 # Sensirion SDP3X differential pressure sensor external I2C
 if param compare -s SENS_EN_SDP3X 1
 then
-	if ! sdp3x_airspeed start -X
+	if ! sdp3x start -X
 	then
 		# try another common address
-		sdp3x_airspeed start -X -a 0x22
+		sdp3x start -X -a 0x22
 	fi
 fi
 
-# SHT3x temperature and hygrometer sensor, external I2C
-if param compare -s SENS_EN_SHT3X 1
+# TE MS4515 differential pressure sensor external I2C
+if param compare -s SENS_EN_MS4515 1
 then
-	sht3x start -X
-	sht3x start -X -a 0x45
+	ms4515 start -X
 fi
 
-# TE MS4525 differential pressure sensor external I2C
-if param compare -s SENS_EN_MS4525 1
+# TE MS4525DO differential pressure sensor external I2C
+if param compare -s SENS_EN_MS4525DO 1
 then
-	ms4525_airspeed start -X
+	ms4525do start -X
 fi
 
-# TE MS5525 differential pressure sensor external I2C
-if param compare -s SENS_EN_MS5525 1
+# TE MS5525DSO differential pressure sensor external I2C
+if param compare -s SENS_EN_MS5525DS 1
 then
-	ms5525_airspeed start -X
+	ms5525dso start -X
+fi
+
+# SHT3x temperature and hygrometer sensor, external I2C
+if param compare -s SENS_EN_SHT3X 1
+then
+	sht3x start -X
+	sht3x start -X -a 0x45
 fi
 
 # IR-LOCK sensor external I2C
@@ -155,6 +172,13 @@ then
 	irlock start -X
 fi
 
+# SPL06 sensor external I2C
+if param compare -s SENS_EN_SPL06 1
+then
+	spl06 -X start
+	spl06 -X -a 0x77 start
+fi
+
 # PCF8583 counter (RPM sensor)
 if param compare -s SENS_EN_PCF8583 1
 then
@@ -179,9 +203,3 @@ then
 	# start last (wait for possible icm20948 passthrough mode)
 	ak09916 -X -q start
 fi
-
-###############################################################################
-#                            End Optional drivers                             #
-###############################################################################
-
-sensors start

ROMFS/px4fmu_common/init.d/rc.uuv_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE uuv
 
+# MAV_TYPE_SUBMARINE 12
+param set-default MAV_TYPE 12
+
 param set-default PWM_MAIN_MAX 1950
 param set-default PWM_MAIN_MIN 1050
 param set-default PWM_MAIN_DISARM 1500

ROMFS/px4fmu_common/init.d/rc.vehicle_setup

@@ -12,19 +12,9 @@ if [ $VEHICLE_TYPE = fw ]
 then
 	if [ $MIXER = none ]
 	then
-		# Set default mixer for fixed wing if not defined.
-		set MIXER AERT
+		echo "FW mixer undefined"
 	fi
 
-	if [ $MAV_TYPE = none ]
-	then
-		# Set a default MAV_TYPE = 1 if not defined.
-		set MAV_TYPE 1
-	fi
-
-	# Set the mav type parameter.
-	param set MAV_TYPE ${MAV_TYPE}
-
 	# Load mixer and configure outputs.
 	. ${R}etc/init.d/rc.interface
 
@@ -42,41 +32,6 @@ then
 		echo "MC mixer undefined"
 	fi
 
-	if [ $MAV_TYPE = none ]
-	then
-		# Set a default MAV_TYPE = 2 if not defined.
-		set MAV_TYPE 2
-
-		# Use mixer to detect vehicle type
-		if [ $MIXER = coax ]
-		then
-			set MAV_TYPE 3
-		fi
-		if [ $MIXER = hexa_x -o $MIXER = hexa_+ ]
-		then
-			set MAV_TYPE 13
-		fi
-		if [ $MIXER = hexa_cox ]
-		then
-			set MAV_TYPE 13
-		fi
-		if [ $MIXER = octo_x -o $MIXER = octo_+ ]
-		then
-			set MAV_TYPE 14
-		fi
-		if [ $MIXER = octo_cox -o $MIXER = octo_cox_w ]
-		then
-			set MAV_TYPE 14
-		fi
-		if [ $MIXER = tri_y_yaw- -o $MIXER = tri_y_yaw+ ]
-		then
-			set MAV_TYPE 15
-		fi
-	fi
-
-	# Set the mav type parameter.
-	param set MAV_TYPE ${MAV_TYPE}
-
 	# Load mixer and configure outputs.
 	. ${R}etc/init.d/rc.interface
 
@@ -91,19 +46,9 @@ if [ $VEHICLE_TYPE = rover ]
 then
 	if [ $MIXER = none ]
 	then
-		# Set default mixer for UGV if not defined.
-		set MIXER rover_generic
-	fi
-
-	if [ $MAV_TYPE = none ]
-	then
-		# Set a default MAV_TYPE = 10 if not defined.
-		set MAV_TYPE 10
+		echo "rover mixer undefined"
 	fi
 
-	# Set the mav type parameter.
-	param set MAV_TYPE ${MAV_TYPE}
-
 	# Load mixer and configure outputs.
 	. ${R}etc/init.d/rc.interface
 
@@ -121,25 +66,6 @@ then
 		echo "VTOL mixer undefined"
 	fi
 
-	if [ $MAV_TYPE = none ]
-	then
-		# Set a default MAV_TYPE = 19 if not defined.
-		set MAV_TYPE 19
-
-		# Use mixer to detect vehicle type.
-		if [ $MIXER = firefly6 ]
-		then
-			set MAV_TYPE 21
-		fi
-		if [ $MIXER = quad_x_pusher_vtol ]
-		then
-			set MAV_TYPE 22
-		fi
-	fi
-
-	# Set the mav type parameter.
-	param set MAV_TYPE ${MAV_TYPE}
-
 	# Load mixer and configure outputs.
 	. ${R}etc/init.d/rc.interface
 
@@ -157,15 +83,6 @@ then
 		echo "Airship mixer undefined"
 	fi
 
-	if [ $MAV_TYPE = none ]
-	then
-		# Set a default MAV_TYPE = 7 if not defined.
-		set MAV_TYPE 7
-	fi
-
-	# Set the mav type parameter.
-	param set MAV_TYPE ${MAV_TYPE}
-
 	# Load mixer and configure outputs.
 	. ${R}etc/init.d/rc.interface
 
@@ -183,19 +100,11 @@ then
 		echo "UUV mixer undefined"
 	fi
 
-	if [ $MAV_TYPE = none ]
-	then
-		# Set default MAV_TYPE to submarine if not defined
-		set MAV_TYPE 12
-	fi
-
-	param set MAV_TYPE ${MAV_TYPE}
 	# Load mixer and configure outputs.
 	. ${R}etc/init.d/rc.interface
 
 	# Start standard vtol apps.
 	. ${R}etc/init.d/rc.uuv_apps
-
 fi
 
 

ROMFS/px4fmu_common/init.d/rc.vtol_defaults

@@ -7,6 +7,9 @@
 
 set VEHICLE_TYPE vtol
 
+# MAV_TYPE_VTOL_FIXEDROTOR 22
+param set-default MAV_TYPE 22
+
 param set-default MIS_TAKEOFF_ALT 20
 param set-default MIS_YAW_TMT 10
 

ROMFS/px4fmu_common/init.d/rcS

@@ -29,7 +29,6 @@ set IOFW "/etc/extras/px4_io-v2_default.bin"
 set IO_PRESENT no
 set LOGGER_ARGS ""
 set LOGGER_BUF 8
-set MAV_TYPE none
 set MIXER none
 set MIXER_AUX none
 set MIXER_FILE none
@@ -406,9 +405,17 @@ else
 			battery_status start
 		fi
 
+		sensors start
 		commander start
 	fi
 
+	#
+	# Configure vehicle type specific parameters.
+	# Note: rc.vehicle_setup is the entry point for rc.interface,
+	#       rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
+	#
+	. ${R}etc/init.d/rc.vehicle_setup
+
 	# Pre-takeoff continuous magnetometer calibration
 	if param compare -s MBE_ENABLE 1
 	then
@@ -459,13 +466,6 @@ else
 		fi
 	fi
 
-	#
-	# Configure vehicle type specific parameters.
-	# Note: rc.vehicle_setup is the entry point for rc.interface,
-	#       rc.fw_apps, rc.mc_apps, rc.rover_apps, and rc.vtol_apps.
-	#
-	. ${R}etc/init.d/rc.vehicle_setup
-
 	#
 	# Play the startup tune (if not disabled or there is an error)
 	#
@@ -493,12 +493,6 @@ else
 		gimbal start
 	fi
 
-	# Check for flow sensor
-	if param compare -s SENS_EN_PX4FLOW 1
-	then
-		px4flow start -X
-	fi
-
 	# Blacksheep telemetry
 	if param compare -s TEL_BST_EN 1
 	then
@@ -515,6 +509,12 @@ else
 		gyro_calibration start
 	fi
 
+	# Check for px4flow sensor
+	if param compare -s SENS_EN_PX4FLOW 1
+	then
+		px4flow start -X &
+	fi
+
 	#
 	# Optional board supplied extras: rc.board_extras
 	#
@@ -573,7 +573,6 @@ unset IO_PRESENT
 unset IOFW
 unset LOGGER_ARGS
 unset LOGGER_BUF
-unset MAV_TYPE
 unset MIXER
 unset MIXER_AUX
 unset MIXER_FILE

ROMFS/px4fmu_common/mixers/quad_x_vtol.main.mix

@@ -1,5 +1,7 @@
 Mixer for Tailsitter with x motor configuration and elevons
 ===========================================================
+# @board px4_fmu-v2 exclude
+# @board omnibus_f4sd exclude
 
 This file defines a single mixer for tailsitter with motors in X configuration.  All controls
 are mixed 100%.

ROMFS/px4fmu_test/init.d/rc.sensors

@@ -16,15 +16,15 @@ if board_adc start
 then
 fi
 
-if sdp3x_airspeed start -X
+if sdp3x start -X
 then
 fi
 
-if ms5525_airspeed start -X
+if ms5525dso start -X
 then
 fi
 
-if ms4525_airspeed start -X
+if ms4525do start -X
 then
 fi
 

Tools/astyle/files_to_check_code_style.sh

@@ -27,4 +27,5 @@ exec find boards msg src platforms test \
     -path src/lib/crypto/monocypher -prune -o \
     -path src/lib/crypto/libtomcrypt -prune -o \
     -path src/lib/crypto/libtommath -prune -o \
+    -path src/modules/microdds_client/Micro-XRCE-DDS-Client -prune -o \
     -type f \( -name "*.c" -o -name "*.h" -o -name "*.cpp" -o -name "*.hpp" \) | grep $PATTERN

Tools/ecl_ekf/analyse_logdata_ekf.py

@@ -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')
 

Tools/ecl_ekf/analysis/checks.py

@@ -55,7 +55,7 @@ def perform_imu_checks(
 
     # perform the vibration check
     imu_status['imu_vibration_check'] = 'Pass'
-    for imu_vibr_metric in ['imu_coning', 'imu_hfdang', 'imu_hfdvel']:
+    for imu_vibr_metric in ['imu_coning', 'imu_hfgyro', 'imu_hfaccel']:
         mean_metric = '{:s}_mean'.format(imu_vibr_metric)
         peak_metric = '{:s}_peak'.format(imu_vibr_metric)
         if imu_metrics[mean_metric] > check_levels['{:s}_warn'.format(mean_metric)] \
@@ -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'),

Tools/ecl_ekf/analysis/metrics.py

@@ -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
@@ -144,17 +145,27 @@ def calculate_imu_metrics(ulog: ULog, multi_instance, in_air_no_ground_effects:
         imu_metrics[result] = calculate_stat_from_signal(
             estimator_status_data, 'estimator_status', signal, in_air_no_ground_effects, np.median)
 
+
     # calculates peak and mean for IMU vibration checks
-    for signal, result in [('vibe[0]', 'imu_coning'),
-                           ('vibe[1]', 'imu_hfdang'),
-                           ('vibe[2]', 'imu_hfdvel')]:
-        peak = calculate_stat_from_signal(
-            estimator_status_data, 'estimator_status', signal, in_air_no_ground_effects, np.amax)
-        if peak > 0.0:
-            imu_metrics['{:s}_peak'.format(result)] = peak
-            imu_metrics['{:s}_mean'.format(result)] = calculate_stat_from_signal(
-                estimator_status_data, 'estimator_status', signal,
-                in_air_no_ground_effects, np.mean)
+    for imu_status_instance in range(4):
+        try:
+            vehicle_imu_status_data = ulog.get_dataset('vehicle_imu_status', imu_status_instance).data
+
+            if vehicle_imu_status_data['accel_device_id'][0] == estimator_status_data['accel_device_id'][0]:
+
+                for signal, result in [('gyro_coning_vibration', 'imu_coning'),
+                                       ('gyro_vibration_metric', 'imu_hfgyro'),
+                                       ('accel_vibration_metric', 'imu_hfaccel')]:
+
+                    peak = calculate_stat_from_signal(vehicle_imu_status_data, 'vehicle_imu_status', signal, in_air_no_ground_effects, np.amax)
+
+                    if peak > 0.0:
+                        imu_metrics['{:s}_peak'.format(result)] = peak
+                        imu_metrics['{:s}_mean'.format(result)] = calculate_stat_from_signal(vehicle_imu_status_data, 'vehicle_imu_status', signal, in_air_no_ground_effects, np.mean)
+
+        except:
+            pass
+
 
     # IMU bias checks
     estimator_states_data = ulog.get_dataset('estimator_states', multi_instance).data

Tools/ecl_ekf/analysis/post_processing.py

@@ -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:

Tools/ecl_ekf/batch_process_metadata_ekf.py

@@ -48,7 +48,7 @@ for filename in os.listdir(metadata_directory):
 
 #        # print out the check levels
 #        print('\n'+'The following metadata loaded from '+filename+' were used'+'\n')
-#        val = population_data.get(filename, {}).get('imu_hfdang_mean')
+#        val = population_data.get(filename, {}).get('imu_hfgyro_mean')
 #        print(val)
 
 # Open pdf file for plotting
@@ -90,10 +90,10 @@ population_results = {
 'ofy_fail_pct_avg':[float('NaN'),'The mean percentage of innovation test fails for the Y axis optical flow sensor'],
 'imu_coning_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU delta angle coning vibration level (mrad)'],
 'imu_coning_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta angle coning vibration level (mrad)'],
-'imu_hfdang_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency delta angle vibration level (mrad)'],
-'imu_hfdang_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency delta angle vibration level (mrad)'],
-'imu_hfdvel_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency delta velocity vibration level (m/s)'],
-'imu_hfdvel_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency delta velocity vibration level (m/s)'],
+'imu_hfgyro_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency gyro vibration level (rad/s)'],
+'imu_hfgyro_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency gyro vibration level (rad/s)'],
+'imu_hfaccel_max_avg':[float('NaN'),'The mean of the maximum in-flight values of the IMU high frequency accel vibration level (m/s/s)'],
+'imu_hfaccel_mean_avg':[float('NaN'),'The mean of the mean in-flight value of the IMU delta high frequency accel vibration level (m/s/s)'],
 'obs_ang_median_avg':[float('NaN'),'The mean of the median in-flight value of the output observer angular tracking error magnitude (mrad)'],
 'obs_vel_median_avg':[float('NaN'),'The mean of the median in-flight value of the output observer velocity tracking error magnitude (m/s)'],
 'obs_pos_median_avg':[float('NaN'),'The mean of the median in-flight value of the output observer position tracking error magnitude (m)'],
@@ -360,54 +360,54 @@ if (len(result1) > 0 and len(result2) > 0):
     plt.close(8)
 
 # IMU high frequency delta angle vibration levels
-temp = np.asarray([population_data[k].get('imu_hfdang_peak') for k in found_keys])
+temp = np.asarray([population_data[k].get('imu_hfgyro_peak') for k in found_keys])
 result1 = 1000.0 * temp[np.isfinite(temp)]
-temp = np.asarray([population_data[k].get('imu_hfdang_mean') for k in found_keys])
+temp = np.asarray([population_data[k].get('imu_hfgyro_mean') for k in found_keys])
 result2 = 1000.0 * temp[np.isfinite(temp)]
 
 if (len(result1) > 0 and len(result2) > 0):
-    population_results['imu_hfdang_max_avg'][0] = np.mean(result1)
-    population_results['imu_hfdang_mean_avg'][0] = np.mean(result2)
+    population_results['imu_hfgyro_max_avg'][0] = np.mean(result1)
+    population_results['imu_hfgyro_mean_avg'][0] = np.mean(result2)
 
     plt.figure(9,figsize=(20,13))
 
     plt.subplot(2,1,1)
     plt.hist(result1)
-    plt.title("Gaussian Histogram - IMU HF Delta Angle Vibration Peak")
-    plt.xlabel("imu_hfdang_max (mrad)")
+    plt.title("Gaussian Histogram - IMU HF Gyroscope Vibration Peak")
+    plt.xlabel("imu_hfgyro_max (rad/s)")
     plt.ylabel("Frequency")
 
     plt.subplot(2,1,2)
     plt.hist(result2)
-    plt.title("Gaussian Histogram - IMU HF Delta Angle Vibration Mean")
-    plt.xlabel("imu_hfdang_mean (mrad)")
+    plt.title("Gaussian Histogram - IMU HF Gyroscope Vibration Mean")
+    plt.xlabel("imu_hfgyro_mean (rad/s)")
     plt.ylabel("Frequency")
 
     pp.savefig()
     plt.close(9)
 
-# IMU high frequency delta velocity vibration levels
-temp = np.asarray([population_data[k].get('imu_hfdvel_peak') for k in found_keys])
+# IMU high frequency accel vibration levels
+temp = np.asarray([population_data[k].get('imu_hfaccel_peak') for k in found_keys])
 result1 = temp[np.isfinite(temp)]
-temp = np.asarray([population_data[k].get('imu_hfdvel_mean') for k in found_keys])
+temp = np.asarray([population_data[k].get('imu_hfaccel_mean') for k in found_keys])
 result2 = temp[np.isfinite(temp)]
 
 if (len(result1) > 0 and len(result2) > 0):
-    population_results['imu_hfdvel_max_avg'][0] = np.mean(result1)
-    population_results['imu_hfdvel_mean_avg'][0] = np.mean(result2)
+    population_results['imu_hfaccel_max_avg'][0] = np.mean(result1)
+    population_results['imu_hfaccel_mean_avg'][0] = np.mean(result2)
 
     plt.figure(10,figsize=(20,13))
 
     plt.subplot(2,1,1)
     plt.hist(result1)
-    plt.title("Gaussian Histogram - IMU HF Delta Velocity Vibration Peak")
-    plt.xlabel("imu_hfdvel_max (m/s)")
+    plt.title("Gaussian Histogram - IMU HF Accelerometer Vibration Peak")
+    plt.xlabel("imu_hfaccel_max (m/s/s)")
     plt.ylabel("Frequency")
 
     plt.subplot(2,1,2)
     plt.hist(result2)
-    plt.title("Gaussian Histogram - IMU HF Delta Velocity Vibration Mean")
-    plt.xlabel("imu_hfdvel_mean (m/s)")
+    plt.title("Gaussian Histogram - IMU HF Accelerometer Vibration Mean")
+    plt.xlabel("imu_hfaccel_mean (m/s/s)")
     plt.ylabel("Frequency")
 
     pp.savefig()
@@ -535,12 +535,12 @@ single_log_results = {
 'hgt_sensor_status':['Pass','Height sensor check summary. This sensor data can be sourced from either Baro, GPS, range fidner or external vision system. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required'],
 'hgt_test_max':[float('NaN'),'The maximum in-flight value of the height sensor innovation consistency test ratio.'],
 'hgt_test_mean':[float('NaN'),'The mean in-flight value of the height sensor innovation consistency test ratio.'],
-'imu_coning_mean':[float('NaN'),'Mean in-flight value of the IMU delta angle coning vibration metric (rad)'],
-'imu_coning_peak':[float('NaN'),'Peak in-flight value of the IMU delta angle coning vibration metric (rad)'],
-'imu_hfdang_mean':[float('NaN'),'Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)'],
-'imu_hfdang_peak':[float('NaN'),'Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)'],
-'imu_hfdvel_mean':[float('NaN'),'Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)'],
-'imu_hfdvel_peak':[float('NaN'),'Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)'],
+'imu_coning_mean':[float('NaN'),'Mean in-flight value of the IMU delta angle coning vibration metric (rad^2)'],
+'imu_coning_peak':[float('NaN'),'Peak in-flight value of the IMU delta angle coning vibration metric (rad^2)'],
+'imu_hfgyro_mean':[float('NaN'),'Mean in-flight value of the IMU gyro high frequency vibration metric (rad/s)'],
+'imu_hfgyro_peak':[float('NaN'),'Peak in-flight value of the IMU gyro high frequency vibration metric (rad/s)'],
+'imu_hfaccel_mean':[float('NaN'),'Mean in-flight value of the IMU accel high frequency vibration metric (m/s/s)'],
+'imu_hfaccel_peak':[float('NaN'),'Peak in-flight value of the IMU accel high frequency vibration metric (m/s/s)'],
 'imu_sensor_status':['Pass','IMU sensor check summary. A Fail result indicates a significant error that caused a significant reduction in vehicle navigation performance was detected. A Warning result indicates that error levels higher than normal were detected but these errors did not significantly impact navigation performance. A Pass result indicates that no amonalies were detected and no further investigation is required'],
 'in_air_transition_time':[float('NaN'),'The time in seconds measured from startup that the EKF transtioned into in-air mode. Set to a nan if a transition event is not detected.'],
 'mag_percentage_amber':[float('NaN'),'The percentage of in-flight consolidated magnetic field sensor innovation consistency test values > 0.5.'],

Tools/ecl_ekf/check_level_dict.csv

@@ -21,10 +21,10 @@ hagl_amber_warn_pct,5.0
 tas_amber_warn_pct,5.0
 imu_coning_peak_warn,1.8E-5
 imu_coning_mean_warn,3.6E-6
-imu_hfdang_peak_warn,3.0E-3
-imu_hfdang_mean_warn,6.0E-4
-imu_hfdvel_peak_warn,9.0E-2
-imu_hfdvel_mean_warn,1.8E-2
+imu_hfgyro_peak_warn,12
+imu_hfgyro_mean_warn,2.4
+imu_hfaccel_peak_warn,360
+imu_hfaccel_mean_warn,72
 obs_ang_err_median_warn,8.0E-3
 obs_vel_err_median_warn,0.05
 obs_pos_err_median_warn,0.15

Tools/ecl_ekf/check_table.csv

@@ -49,12 +49,12 @@ hagl_test_mean, The mean in-flight value of the height above ground sensor innov
 ofx_fail_percentage, The percentage of in-flight recorded failure events for the optical flow sensor X-axis innovation consistency test.
 ofy_fail_percentage, The percentage of in-flight recorded failure events for the optical flow sensor Y-axis innovation consistency test.
 filter_faults_max, Largest recorded value of the filter internal fault bitmask. Should always be zero.
-imu_coning_peak, Peak in-flight value of the IMU delta angle coning vibration metric (rad)
-imu_coning_mean, Mean in-flight value of the IMU delta angle coning vibration metric (rad)
-imu_hfdang_peak, Peak in-flight value of the IMU delta angle high frequency vibration metric (rad)
-imu_hfdang_mean, Mean in-flight value of the IMU delta angle high frequency vibration metric (rad)
-imu_hfdvel_peak, Peak in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
-imu_hfdvel_mean, Mean in-flight value of the IMU delta velocity high frequency vibration metric (m/s)
+imu_coning_peak, Peak in-flight value of the IMU delta angle coning vibration metric (rad^2)
+imu_coning_mean, Mean in-flight value of the IMU delta angle coning vibration metric (rad^2)
+imu_hfgyro_peak, Peak in-flight value of the IMU accel high frequency vibration metric (rad/s)
+imu_hfgyro_mean, Mean in-flight value of the IMU accel high frequency vibration metric (rad/s)
+imu_hfaccel_peak, Peak in-flight value of the IMU accel high frequency vibration metric (m/s/s)
+imu_hfaccel_mean, Mean in-flight value of the IMU accel high frequency vibration metric (m/s/s)
 output_obs_ang_err_median, Median in-flight value of the output observer angular error (rad)
 output_obs_vel_err_median, Median in-flight value of the output observer velocity error (m/s)
 output_obs_pos_err_median, Median in-flight value of the output observer position error (m)

Tools/ecl_ekf/plotting/pdf_report.py

@@ -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)
@@ -250,18 +256,32 @@ def create_pdf_report(ulog: ULog, multi_instance: int, output_plot_filename: str
         data_plot.save()
         data_plot.close()
 
+
         # Plot the EKF IMU vibration metrics
-        scaled_estimator_status = {'vibe[0]': 1000. * estimator_status['vibe[0]'],
-                                   'vibe[1]': 1000. * estimator_status['vibe[1]'],
-                                   'vibe[2]': estimator_status['vibe[2]']
-                                   }
-        data_plot = CheckFlagsPlot(
-            status_time, scaled_estimator_status, [['vibe[0]'], ['vibe[1]'], ['vibe[2]']],
-            x_label='time (sec)', y_labels=['Del Ang Coning (mrad)', 'HF Del Ang (mrad)',
-                                            'HF Del Vel (m/s)'], plot_title='IMU Vibration Metrics',
-            pdf_handle=pdf_pages, annotate=True)
-        data_plot.save()
-        data_plot.close()
+        for imu_status_instance in range(4):
+            try:
+                vehicle_imu_status_data = ulog.get_dataset('vehicle_imu_status', imu_status_instance).data
+
+                imu_status_time = 1e-6 * vehicle_imu_status_data['timestamp']
+
+                if vehicle_imu_status_data['accel_device_id'][0] == estimator_status['accel_device_id'][0]:
+
+                    scaled_estimator_status = {'delta_angle_coning_metric': 1000. * vehicle_imu_status_data['delta_angle_coning_metric'],
+                                               'gyro_vibration_metric': vehicle_imu_status_data['gyro_vibration_metric'],
+                                               'accel_vibration_metric': vehicle_imu_status_data['accel_vibration_metric']
+                                              }
+                    data_plot = CheckFlagsPlot(
+                        imu_status_time, scaled_estimator_status, [['delta_angle_coning_metric'], ['gyro_vibration_metric'], ['accel_vibration_metric']],
+                        x_label='time (sec)',
+                        y_labels=['Del Ang Coning (mrad^2)', 'HF Gyro (rad/s)', 'HF accel (m/s/s)'],
+                        plot_title='IMU Vibration Metrics',
+                        pdf_handle=pdf_pages, annotate=True)
+                    data_plot.save()
+                    data_plot.close()
+
+            except:
+                pass
+
 
         # Plot the EKF output observer tracking errors
         scaled_innovations = {
@@ -330,33 +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:

Tools/kconfig/cmake_kconfig_lut.txt

@@ -139,6 +139,7 @@ mc_hover_thrust_estimator,CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
 mc_pos_control,CONFIG_MODULES_MC_POS_CONTROL=y
 mc_rate_control,CONFIG_MODULES_MC_RATE_CONTROL=y
 micrortps_bridge,CONFIG_MODULES_MICRORTPS_BRIDGE=y
+microdds_client,CONFIG_MODULES_MICRODDS_CLIENT=y
 navigator,CONFIG_MODULES_NAVIGATOR=y
 px4iofirmware,CONFIG_MODULES_PX4IOFIRMWARE=y
 rc_update,CONFIG_MODULES_RC_UPDATE=y

Tools/sitl_gazebo

@@ -1 +1 @@
-Subproject commit 25138e803ee8525ee5fe4e6d511506e88e3f819c
+Subproject commit 48440d7b5c78a21182415266334981f1163f4b2c

boards/airmind/mindpx-v2/nuttx-config/nsh/defconfig

@@ -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

boards/ark/can-flow/nuttx-config/nsh/defconfig

@@ -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

boards/ark/can-gps/nuttx-config/nsh/defconfig

@@ -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

boards/ark/can-rtk-gps/nuttx-config/nsh/defconfig

@@ -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

boards/ark/cannode/canbootloader.px4board

@@ -0,0 +1,6 @@
+CONFIG_BOARD_TOOLCHAIN="arm-none-eabi"
+CONFIG_BOARD_ARCHITECTURE="cortex-m4"
+CONFIG_BOARD_ROMFSROOT=""
+CONFIG_BOARD_CONSTRAINED_MEMORY=y
+CONFIG_DRIVERS_BOOTLOADERS=y
+CONFIG_NSH_BUILTIN_APPS=y