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104 Commits

Author SHA1 Message Date
Daniel Agar f8a8675e2d ORB queue depth completely static 2024-03-08 10:47:43 -05:00
Daniel Agar 600b0e6704 Merge remote-tracking branch 'px4/main' into pr-modalai-muorb-updates 2024-03-08 10:08:36 -05:00
Silvan Fuhrer 7884e0a3f7 Navigator: remove vtol_takeoff special handling for RTL (#22844)
We had a special handling for RTL triggered in vtol_takeoff state.
The idea is to wait until the VTOL Takeoff is completed and only
then switch to RTL. On a second thought this special handling isn't
really necessary and for the sake of simplicity should be removed.
This also removes the side effect of the indicated flight mode
after RTL being set to VTOL_Takeoff again.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-03-08 11:40:14 +01:00
Silvan Fuhrer f799141a19 FW Pos Controller: do not publish roll angle constrained warning if landed (#22850)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-03-08 09:40:43 +01:00
Eric Katzfey e20215087f Moving from Qurt specific icm4266p driver to mainline version 2024-03-07 21:14:49 -05:00
bresch 0d0978b3b9 ekf2: update change indicator 2024-03-07 11:06:31 -05:00
bresch 0639f5370c ekf2: fix mag and wind covariance prediction 2024-03-07 11:06:31 -05:00
bresch 2bacb4b65d ekf2: update change indicator 2024-03-07 15:11:47 +01:00
bresch 421f13e4b5 ekf2: fix joseph covariance update for Schmidt-Kalman filter
If part of the Kalman gain is zeroed, the first step of the joseph
update does not produce a symmetrical matrix.
2024-03-07 15:11:47 +01:00
Silvan Fuhrer 1e253a9626 VTOL: treat Descend mode as Land (#22843)
* vtol_type: enable pusher assist also in Descend mode

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>

* vtol_type: treat Descend as Land for pusher assist

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>

---------

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-03-07 10:22:25 +01:00
cuav-liu1 bb5efa5577 ICP201: increase config delay 2024-03-06 21:20:51 -05:00
Daniel Agar 1c741836c0 sensors/vehicle_imu: sensor update loop limit iterations 2024-03-06 21:19:38 -05:00
Daniel Agar 8b6c70e0f2 sensors/vehicle_angular_velocity: sensor update loop limit iterations 2024-03-06 21:19:38 -05:00
Daniel Agar 1fc38aab92 sensors/vehicle_air_data: sensor update loop limit iterations 2024-03-06 21:19:38 -05:00
Daniel Agar 2bf1eeb003 sensors/vehicle_acceleration: sensor update loop limit iterations 2024-03-06 21:19:38 -05:00
Daniel Agar 87960c04d8 mag_bias_estimator: sensor update loop limit iterations 2024-03-06 21:19:38 -05:00
Daniel Agar d96970a2b9 sensor/vehicle_magnetometer: sensor update loop limit iterations
- place upper bound to prevent looping indefinitely (high publish rate, etc)
2024-03-06 21:19:38 -05:00
Silvan Fuhrer c5835a48de FW Position Controller: do not publish roll angle constrain warning in VTOL transition (#22842)
* FW Position Control: some cosmetical changes

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>

* FW Position Control: disable roll constraining warning in VTOL transition

In transitions it is expected that the roll is constrained, and
instead of defining an aribitrary threshold let's rather disable
the user warning in that case.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>

* FW Pos C: define magic numbers for roll constraining warning as constants

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>

---------

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-03-06 15:51:54 +01:00
bresch 6f9a378247 yaw_est: force set gyro bias when at rest
The gyro bias estimate from EFK2 is really good when at rest and should
be used by the yaw estimator to prevent heading drifts due to poor
heading observability.
2024-03-05 14:00:06 -05:00
PX4 BuildBot 67e68783cf Update submodule gz to latest Tue Mar 5 12:39:22 UTC 2024
- gz in PX4/Firmware (5f8f0213a807d327a30a7df05e58f7887cf936ab): https://github.com/PX4/PX4-gazebo-models/commit/222833656802532ec2271986a65fd198cfa48259
    - gz current upstream: https://github.com/PX4/PX4-gazebo-models/commit/6b4ed09d1b495fbff663f098979cc046df013abd
    - Changes: https://github.com/PX4/PX4-gazebo-models/compare/222833656802532ec2271986a65fd198cfa48259...6b4ed09d1b495fbff663f098979cc046df013abd

    6b4ed09 2024-02-23 Sergei Grichine - Added IMU sensor noise to the model, to avoid STALE messages (#34)
953e02b 2024-02-22 frede791 - add imu sensor model noise
2024-03-05 13:59:22 -05:00
Peter van der Perk d1ae242a91 v6x-rt: fix rover build regression 2024-03-05 10:21:41 -05:00
Peter van der Perk 9cef834624 fmu-v6xrt: update px4board enables vtol 2024-03-05 08:18:44 -05:00
Sihyun Noh 23a41299fa mag calibration: minor cleanup (#22830) 2024-03-05 09:00:08 +01:00
Niklas Hauser 0186d687b2 Add minimal Skynode RC13 config to the PAB manifest 2024-03-04 13:33:20 -05:00
Peter van der Perk d28653b605 nuttx: update apps 2024-03-04 13:32:36 -05:00
Peter van der Perk 87d79aeb75 netman: generate default config if file doesn't exist
ENOENT returns if the file doesn't exist yet, when using mtd /fs/mtd_net always exist.
On a filesystem you've to generate the file so if ENOENT returns we've to regenerate the default config as well.
2024-03-04 13:32:36 -05:00
Matthias Grob 1bd65f8beb mantis-edu: remove duplicate RC define 2024-03-04 13:30:28 -05:00
Peter van der Perk e0b49afe81 bmp388: Driver print out start BMP390 identifier when detected 2024-03-04 02:05:37 -05:00
Don Gagne f02b44bec5 Update to latest sitl gazebo camera 2024-03-03 12:18:02 +13:00
Eric Katzfey dd67766f6c Made setting of queue size in orb node based on topic definition 2024-03-01 14:18:52 -08:00
Eric Katzfey 4a043a80f1 Fixed error in macro definition 2024-02-27 20:12:59 -08:00
Eric Katzfey bb617a1a56 Merge branch 'main' of github.com:PX4/PX4-Autopilot into pr-modalai-muorb-updates 2024-02-27 19:57:46 -08:00
Eric Katzfey 01de368616 Removed libfc sensor from format checks 2024-02-27 19:56:59 -08:00
Eric Katzfey 76352765b6 Fixes to the ModalAI muorb implementation 2024-02-27 19:56:17 -08:00
bresch 28db3e1c8c ekf2: update change indicator 2024-02-27 12:33:43 -05:00
bresch e9d43015ce ekf2: fix unit tests failing due to mag fusion changes 2024-02-27 12:33:43 -05:00
bresch b46fc9a67d ekf2 sensor_sim: set correct world mag field 2024-02-27 12:33:43 -05:00
bresch b80f15f7b5 ekf2-mag_auto: always use mag 3D after takeoff 2024-02-27 12:33:43 -05:00
Silvan Fuhrer 086656dc7f FW Attitude Controller: fix manual yaw rate setpoint limit (#22812)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-27 17:23:13 +01:00
bresch 051baec9c4 ekf2: allow wind dead-reckoning after manual position reset
Reset velocity using airspeed and start navigating
2024-02-27 09:34:05 -05:00
Matthias Grob 2491548a0f Jenkinsfile: correct typo, missing comma
Introduced in
2c81c9fdea
2024-02-27 13:32:46 +01:00
DanielePettenuzzo 18f96c16ce fix gimbal driver for mavlink gimbal v2 input and AUX output
The main problem was that during initial negotiation the client would
request the gimbal_manager_information from px4 but px4 would never send
it because in this configuration the device_compid was set to 0.
2024-02-27 09:53:25 +01:00
GuillaumeLaine 63495ddac3 geo: correct unit test 2024-02-27 09:05:39 +01:00
Peter van der Perk efbbd64ec0 fmu-v6xrt: Increase lpwork stack size 2024-02-26 14:01:56 -05:00
Daniel Agar 8001132d33 ekf2: ZeroGyroUpdate move to fuseDirectStateMeasurement 2024-02-26 12:32:59 -05:00
bresch 08a2a6c836 update EKF2 change indicator 2024-02-26 12:32:59 -05:00
bresch d501d8e1d4 ekf2: use Joseph stabilized update in direct state observations 2024-02-26 12:32:59 -05:00
bresch 9d9766c6cf ekf2: use Joseph stabilized covariance update 2024-02-26 12:32:59 -05:00
makekam d988005216 Update injectxmlparams.py
Add extraction of Boolean attributes in injectxmlparams.py.
2024-02-23 11:06:05 -05:00
Silvan Fuhrer 5dfdf8c071 matrix: remove bold printing of diagonal elements
As this was not working in NSH.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-23 11:05:09 -05:00
Daniel Agar b2b7439060 ROMFS: respect kconfig for including romfs files (airframes, etc) (#22571)
* ROMFS: respect kconfig for including romfs files (airframes, etc)

* ROMFS: only add R1 airframe with differential drive control

* ROMFS: adapt to differential drive module renaming

---------

Co-authored-by: Matthias Grob <maetugr@gmail.com>
2024-02-23 15:40:00 +01:00
bresch 37a40d3fc2 baro static pressure compensation tuning: remove dependency to baro bias
`estimator_baro_bias` requires to have GNSS and baro hgt active and GNSS as the reference. This is quite restrictive. Instead, we can simply use a high-passed version of the baro error.
2024-02-23 10:07:13 +01:00
Sergei Grichine b405d75553 Added Zero Turn Lawnmower model (#22717)
* Added Lawnmower airframe

* Update 5005_gz_lawnmower

Works all right

* Update 5005_gz_lawnmower

RDD_WHL_SPEED has new name: RDD_WHEEL_SPEED

* Update ROMFS/px4fmu_common/init.d-posix/airframes/5005_gz_lawnmower

Co-authored-by: Per Frivik <94360401+PerFrivik@users.noreply.github.com>

* Update ROMFS/px4fmu_common/init.d-posix/airframes/CMakeLists.txt

Co-authored-by: Per Frivik <94360401+PerFrivik@users.noreply.github.com>

* Renamed 5005_gz_lawnmower to 4011_gz_lawnmower

also pulled latest GZ models hash

---------

Co-authored-by: Per Frivik <94360401+PerFrivik@users.noreply.github.com>
2024-02-22 15:30:12 +01:00
Matthias Grob 4e3bd4f196 MAVSDK tests: shorten Position, Altitude control flights
We get more than 5 meter away much quicker.
2024-02-22 15:29:13 +01:00
Matthias Grob 0cc4b41a51 MAVSDK test: Fix fly_forward_in_altctl() timing 2024-02-22 15:29:13 +01:00
Matthias Grob f602228048 MAVSDK test: increase offboard position threshold
This is a workaround to hotfix CI but the root cause is #22792
(MAVSDK test failing after EKF change, accelerometer simulation issues not learned anymore?)
2024-02-22 15:29:13 +01:00
PerFrivik 9b122adae4 Fix fly_forward_in_posctl() timing 2024-02-22 15:29:13 +01:00
Eric Katzfey 1ec0ba4736 Added param system command to voxl2 slpi build 2024-02-21 11:54:02 -05:00
Eric Katzfey 8da8b88a54 Fixed and added Qurt platform dsp_hitl driver 2024-02-21 11:54:02 -05:00
Eric Katzfey be08c57a0a Changed order of service startup in SLPI DSP muorb since parameter library now needs work queues 2024-02-21 11:54:02 -05:00
Eric Katzfey a436a8f3b8 Fixed unresolved symbol error for qurt platform due to missing sbus library 2024-02-21 11:54:02 -05:00
Eric Katzfey 5ad0e68d8e Fix build error for Qurt platform in pab_manifest.c 2024-02-21 11:54:02 -05:00
Eric Katzfey f07eeaa776 Added special muorb startup ordering in px4_init for posix platform 2024-02-21 11:52:24 -05:00
Daniel Agar 506c60c471 ekf2: declination fusion don't use uninitialized parameter (EKF2_MAG_DECL) 2024-02-21 09:45:44 -05:00
Niklas Hauser 643d3e3bf3 Navigator: Prevent busy-looping if Dataman read/write times out
MissionBase did not initialize its mission data, thus could enter an
infinite loop in updateDatamanCache() if the initMission() failed to
read the mission off, for example, due to the SDCard storage task taking
longer than the timeout to respond.

This change constrains the loading loop and resets the mission data even
if the data write failed.
2024-02-21 13:31:43 +01:00
Daniel Agar 8243b4f474 ekf2: move vel/pos reset helpers 2024-02-20 13:16:24 -05:00
Daniel Agar 22b957696d ekf2: velocity/position fusion helper minor consistency cleanup 2024-02-20 13:16:24 -05:00
Daniel Agar c338891677 ekf2: split vel_pos_fusion.cpp 2024-02-20 13:16:24 -05:00
Daniel Agar c4c41c49e5 ekf2: move fuseVelPosHeight() -> fuseDirectStateMeasurement()
- don't bother keeping bad_vel_{N,E,D} and bad_pos_{N,E,D} fault status bits
2024-02-20 13:16:24 -05:00
Daniel Agar 021dd0d0af ekf2: fix EV height bias predict call
- needs to be called every iteration
2024-02-20 11:47:53 -05:00
bresch c221da27a7 ekf2: set attitude validity flag using centralized function 2024-02-20 11:33:30 -05:00
Matthias Grob 51fe4351c6 StickTiltXY: Fix too high maximum tilt problem
And add unit tests.
2024-02-20 14:27:49 +01:00
Silvan Fuhrer 8a75733511 Navigator: fix VTOL land waypoint calculation
The setpoint.yaw can be NAN, and this made the calculated land point NAN
as well. Looking at the current yaw is anyway a better way to approximate
the course over ground that fundamentally should be used.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-19 14:54:28 +01:00
Daniel Agar 1032dd3470 ekf: fix measurementUpdate comment typo 2024-02-19 09:41:49 +01:00
Konrad 424c3cd2cb FeasibilityChecker: Add new TakeoffLandAvailable option
ADd a new misison feasiblity checker option to check if a proper landing approach is defined when in air. There must be at least a mission landing or a VTOL approach defined in order for the mission to be accepted. Else, use the same logic as in MIS_TKO_LAND_REQ=4
2024-02-16 10:27:22 +01:00
Konrad 68100650da RTL: publish a status message on currently chosen RTL point 2024-02-16 10:27:22 +01:00
Cyril C 74303a79e1 drivers/batt_smbus: fix BQ40Z80 timeout problem (#22751)
Co-authored-by: cyril.calvez <c.calvez@elistair.com>
2024-02-15 13:24:40 -05:00
Daniel Agar 8dc3975456 ekf2: only populate gnss pos aid src status if ref initialized
- this is a minor logging improvement when plotting the position from the beginning of the log (often a replay session)
2024-02-15 13:13:10 -05:00
Matthias Grob 84a7d42566 rover build: correct differential drive kconfig name 2024-02-15 10:08:51 -05:00
Matthias Grob f26df8492f Update GPS drivers to contain the astyle fix 2024-02-15 15:23:06 +01:00
Konrad cb09dde606 FixedwingPositionControl: Used corrected npfg roll output in path mode 2024-02-13 17:17:44 +01:00
Konrad 1a1891073e FixedwingPositionControl: Only warn user when roll is reduced for a longer period of time 2024-02-13 17:17:44 +01:00
Daniel Agar b8714f8980 ROMFS: rc.simulator EKF2 setup specific to gazebo classic 2024-02-13 11:14:44 -05:00
PX4 BuildBot 0c099f2b56 Update submodule gz to latest Tue Feb 13 12:39:17 UTC 2024
- gz in PX4/Firmware (c9ad60e3cc): https://github.com/PX4/PX4-gazebo-models/commit/c78f7f01417168e8faab7a83ade2129c0d26b39d
    - gz current upstream: https://github.com/PX4/PX4-gazebo-models/commit/f1c461fffb8567d6f0af770fb533f60f6ec62c22
    - Changes: https://github.com/PX4/PX4-gazebo-models/compare/c78f7f01417168e8faab7a83ade2129c0d26b39d...f1c461fffb8567d6f0af770fb533f60f6ec62c22

    f1c461f 2024-02-08 frederik - increase monocam clipping distance
6d5db73 2024-02-07 Sergei Grichine - Added Zero Turn Lawnmower model (#27)
5332071 2024-02-06 Frederik Markus - add navsat plugin to worlds and navsat sensor to models (#26)
2024-02-13 11:13:17 -05:00
Frederik Markus bb53781b8f simulation/gz_bridge: enable navsat plugin for accurate positioning of real life maps in Gazebo (#22638)
* publish the global groundtruth from the navsat callback and rearrange the local groundtruth as the altitude reference now has a dependency on the global groundtruth being initialized

---------

Signed-off-by: frederik <frederik.anilmarkus@gmail.com>
2024-02-13 11:09:35 -05:00
Silvan Fuhrer c9ad60e3cc Update src/modules/navigator/mission_block.cpp
Co-authored-by: Matthias Grob <maetugr@gmail.com>
2024-02-13 10:34:57 +01:00
Silvan Fuhrer a6ef7b6da9 RTL: write out weather vane in comments (instead of WV)
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-13 10:34:57 +01:00
Silvan Fuhrer 6957818603 RTL: clean up naming of function arguments
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-13 10:34:57 +01:00
Matthias Grob cb03835124 RTL: use dest.yaw instead of a separate heading_sp 2024-02-13 10:34:57 +01:00
Silvan Fuhrer b19e35ec7c RTL: change when to set a heading setpoint, generally leave it up to the executer
-remove RTL_HDG_MD
-only set heading setpoint in Navigator::RTL once above landing point,
or when RTL is triggered close to it
-never set a heading during RTL if weather vane is enabled

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2024-02-13 10:34:57 +01:00
PX4 BuildBot dce53a626e boards: update all NuttX defconfigs 2024-02-12 08:58:49 -05:00
Daniel Agar 5f589bdda3 Update submodule GPSDrivers to latest Mon Feb 12 12:39:19 UTC 2024
- GPSDrivers in PX4/Firmware (17ff40898c683e1fe96ff9e2d2790594d188f872): https://github.com/PX4/PX4-GPSDrivers/commit/3393191fbb842f8e13a3f296218efec832640112
    - GPSDrivers current upstream: https://github.com/PX4/PX4-GPSDrivers/commit/f48cc01d31607baa4963bde090f530b44df3de12
    - Changes: https://github.com/PX4/PX4-GPSDrivers/compare/3393191fbb842f8e13a3f296218efec832640112...f48cc01d31607baa4963bde090f530b44df3de12

    f48cc01 2024-02-08 Julian Oes - ubx: separate config for jamming monitor
bc72f55 2024-02-08 Julian Oes - sbf: simplify odd define

Co-authored-by: PX4 BuildBot <bot@px4.io>
2024-02-12 08:58:21 -05:00
Matthias Grob 1998f54ea6 DifferentialDrive: move spoolup consideration to the main module 2024-02-12 14:29:10 +01:00
PerFrivik bef694f9ba Added spoolup and removed temporary timeout for EKF 2024-02-12 14:29:10 +01:00
PerFrivik 560d6a9d4b cleanup + updated acro 2024-02-12 14:29:10 +01:00
PerFrivik f996caa5bd Fixed bug in the guidance logic
After smoothing the linera velocity setpoint, the EKF has trouble initializing, becuase the acceleration is too smooth, to combat this issue, there is a 1 second delay when initializing the mission mode
2024-02-12 14:29:10 +01:00
PerFrivik bb0dfba4e6 added acro mode
Acro mode is manual mode, but with rate control
2024-02-12 14:29:10 +01:00
PerFrivik d197d94889 Fixed guidance logic and added feedforward term to compute the angular velocity 2024-02-12 14:29:10 +01:00
Matthias Grob 396ef222ee DifferentialDrive: Rework structure
3 Components Guidance - Control - Allocation
with their corresponding uORB interface.
2024-02-12 14:29:10 +01:00
Matthias Grob f85144ca76 DifferentialDrive: remove trailing zeros from prameter metadata 2024-02-12 14:29:10 +01:00
Matthias Grob b54b4f7dce Rename module differential_drive_control -> differential_drive 2024-02-12 14:29:10 +01:00
Matthias Grob fc90e235f1 Rename differential drive setpoint topics 2024-02-12 14:29:10 +01:00
Matthias Grob f7baeae1a0 DifferentialDriveControl: only save required parts of uORB message 2024-02-12 14:29:10 +01:00
PerFrivik e457a5baed Differential Drive Guidance: Add guidance
also add dependency on control allocation parameter CA_R_REV

Differential Drive Guidance: Added mission logic

Differential Drive Guidance

Differential Drive Guidance

Differential Guidance: Inlcude library

Differential Guidance: Compiles, does not work though

Differential Guidance: Works somewhat

Differential Guidance: Temp

Differential Guidance: Tuning

Differeital Drive Guidance: Remove waypoint mover

Differential Guidance: Fixed accuracy issue by converting from float to double

Differential Guidance: rebased on differentialdrive and improved waypoint accuracy

Temp

Differential Guidance: cleanup

temp
2024-02-12 14:29:10 +01:00
181 changed files with 3344 additions and 4069 deletions
+1 -1
View File
@@ -120,7 +120,7 @@ pipeline {
"px4_fmu-v6xrt_rover",
"px4_io-v2_default",
"raspberrypi_pico_default",
"siyi_n7_default"
"siyi_n7_default",
"sky-drones_smartap-airlink_default",
"spracing_h7extreme_default",
"thepeach_k1_default",
@@ -0,0 +1,80 @@
#!/bin/sh
# @name Gazebo lawnmower
# @type Rover
# @class Rover
. ${R}etc/init.d/rc.rover_differential_defaults
PX4_SIMULATOR=${PX4_SIMULATOR:=gz}
PX4_GZ_WORLD=${PX4_GZ_WORLD:=default}
PX4_SIM_MODEL=${PX4_SIM_MODEL:=lawnmower}
param set-default SIM_GZ_EN 1 # Gazebo bridge
# Simulated sensors
param set-default SENS_EN_GPSSIM 1
param set-default SENS_EN_BAROSIM 0
param set-default SENS_EN_MAGSIM 1
param set-default SENS_EN_ARSPDSIM 1
# We can arm and drive in manual mode when it slides and GPS check fails:
param set-default COM_ARM_WO_GPS 1
# Set Differential Drive Kinematics Library parameters:
param set RDD_WHEEL_BASE 0.9
param set RDD_WHEEL_RADIUS 0.22
param set RDD_WHEEL_SPEED 10.0 # Maximum wheel speed rad/s, approx 8 km/h
# Actuator mapping - set SITL motors/servos output parameters:
# "Motors" - motor channels 0 (Right) and 1 (Left) - via Wheels GZ bridge:
param set-default SIM_GZ_WH_FUNC1 101 # right wheel
#param set-default SIM_GZ_WH_MIN1 0
#param set-default SIM_GZ_WH_MAX1 200
#param set-default SIM_GZ_WH_DIS1 100
#param set-default SIM_GZ_WH_FAIL1 100
param set-default SIM_GZ_WH_FUNC2 102 # left wheel
#param set-default SIM_GZ_WH_MIN2 0
#param set-default SIM_GZ_WH_MAX2 200
#aram set-default SIM_GZ_WH_DIS2 100
#param set-default SIM_GZ_WH_FAIL2 100
param set-default SIM_GZ_WH_REV 0 # no need to reverse any wheels
# Note: The servo configurations ( SIM_GZ_SV_FUNC*) outlined below are intended for educational purposes in this simulation.
# They do not have physical effects in the simulated environment, except for actuating the joints. Their definitions are meant to demonstrate
# how actuators could be mapped and configured in a real-world application, providing a foundation for understanding and implementing actuator
# controls in practical scenarios.
# Cutter deck blades clutch, PCA9685 servo channel 3, "RC FLAPS" (406) - leftmost switch, or "Servo 3" (203):
param set-default SIM_GZ_SV_FUNC3 203
param set-default SIM_GZ_SV_MIN3 0
param set-default SIM_GZ_SV_MAX3 1000
param set-default SIM_GZ_SV_DIS3 500
param set-default SIM_GZ_SV_FAIL3 500
# Gas engine throttle, PCA9685 servo channel 4, "RC AUX1" (407) - left knob, or "Servo 4" (204):
# - on minimum when disarmed or failed:
param set-default SIM_GZ_SV_FUNC4 204
param set-default SIM_GZ_SV_MIN4 0
param set-default SIM_GZ_SV_MAX4 1000
param set-default SIM_GZ_SV_DIS4 500
param set-default SIM_GZ_SV_FAIL4 500
# Controlling PCA9685 servos 5,6,7,8 directly via "Servo 5..8" setting, by publishing actuator_servos.control[]:
# Strobes, PCA9685 servo channel 5, "Servo 5" (205) - flashing indicates Mission mode:
#param set-default SIM_GZ_SV_FUNC5 205
#param set-default SIM_GZ_SV_MIN5 1000
#param set-default SIM_GZ_SV_MAX5 2000
#param set-default SIM_GZ_SV_DIS5 1000
#param set-default SIM_GZ_SV_FAIL5 1000
# Horn, PCA9685 servo channel 6, "Servo 6" (206) - for alarms like GPS failure:
#param set-default SIM_GZ_SV_FUNC6 206
# Spare PCA9685 servo channel 7 on "RC AUX2" (408) - right knob, or "Servo 7" (207):
#param set-default SIM_GZ_SV_FUNC7 207
# Spare PCA9685 servo channel 8 - "Servo 8" (208):
#param set-default SIM_GZ_SV_FUNC8 208
@@ -82,6 +82,7 @@ px4_add_romfs_files(
4008_gz_advanced_plane
4009_gz_r1_rover
4010_gz_x500_mono_cam
4011_gz_lawnmower
6011_gazebo-classic_typhoon_h480
6011_gazebo-classic_typhoon_h480.post
@@ -41,19 +41,6 @@ elif [ "$PX4_SIMULATOR" = "gz" ] || [ "$(param show -q SIM_GZ_EN)" = "1" ]; then
echo "INFO [init] Gazebo simulator"
# set local coordinate frame reference
if [ -n "${PX4_HOME_LAT}" ]; then
param set SIM_GZ_HOME_LAT ${PX4_HOME_LAT}
fi
if [ -n "${PX4_HOME_LON}" ]; then
param set SIM_GZ_HOME_LON ${PX4_HOME_LON}
fi
if [ -n "${PX4_HOME_ALT}" ]; then
param set SIM_GZ_HOME_ALT ${PX4_HOME_ALT}
fi
# Only start up Gazebo if PX4_GZ_STANDALONE is not set.
if [ -z "${PX4_GZ_STANDALONE}" ]; then
@@ -180,6 +167,12 @@ elif [ "$PX4_SIM_MODEL" = "jmavsim_iris" ] || [ "$(param show -q SYS_AUTOSTART)"
else
# otherwise start simulator (mavlink) module
# EKF2 specifics
param set-default EKF2_GPS_DELAY 10
param set-default EKF2_MULTI_IMU 3
param set-default SENS_IMU_MODE 0
simulator_tcp_port=$((4560+px4_instance))
# Check if PX4_SIM_HOSTNAME environment variable is empty
-4
View File
@@ -164,10 +164,6 @@ param set-default COM_RC_IN_MODE 1
# Speedup SITL startup
param set-default EKF2_REQ_GPS_H 0.5
# Multi-EKF
param set-default EKF2_MULTI_IMU 3
param set-default SENS_IMU_MODE 0
param set-default IMU_GYRO_FFT_EN 1
param set-default MAV_PROTO_VER 2 # Ensures QGC does not drop the first few packets after a SITL restart due to MAVLINK 1 packets
+71 -20
View File
@@ -34,28 +34,79 @@
add_subdirectory(airframes)
px4_add_romfs_files(
rc.airship_apps
rc.airship_defaults
rc.autostart_ext
rc.balloon_apps
rc.balloon_defaults
rc.boat_defaults
rc.fw_apps
rc.fw_defaults
rc.heli_defaults
rc.logging
rc.mc_apps
rc.mc_defaults
rcS
rc.sensors
rc.thermal_cal
rc.rover_apps
rc.rover_defaults
rc.rover_differential_apps
rc.rover_differential_defaults
rc.uuv_apps
rc.uuv_defaults
rc.vehicle_setup
rc.vtol_apps
rc.vtol_defaults
# TODO
rc.balloon_apps
rc.balloon_defaults
)
if(CONFIG_MODULES_AIRSHIP_ATT_CONTROL)
px4_add_romfs_files(
rc.airship_apps
rc.airship_defaults
)
endif()
if(CONFIG_MODULES_FW_RATE_CONTROL)
px4_add_romfs_files(
rc.fw_apps
rc.fw_defaults
)
endif()
if(CONFIG_MODULES_MC_RATE_CONTROL)
px4_add_romfs_files(
rc.heli_defaults
rc.mc_apps
rc.mc_defaults
)
endif()
if(CONFIG_MODULES_ROVER_POS_CONTROL)
px4_add_romfs_files(
rc.rover_apps
rc.rover_defaults
rc.boat_defaults # hack
)
endif()
if(CONFIG_MODULES_DIFFERENTIAL_DRIVE)
px4_add_romfs_files(
rc.rover_differential_apps
rc.rover_differential_defaults
)
endif()
if(CONFIG_MODULES_UUV_ATT_CONTROL)
px4_add_romfs_files(
rc.uuv_apps
rc.uuv_defaults
)
endif()
if(CONFIG_MODULES_VTOL_ATT_CONTROL)
px4_add_romfs_files(
rc.vtol_apps
rc.vtol_defaults
)
endif()
if(CONFIG_MODULES_LOGGER)
px4_add_romfs_files(
rc.logging
)
endif()
if(CONFIG_MODULES_TEMPERATURE_COMPENSATION)
px4_add_romfs_files(
rc.thermal_cal
)
endif()
@@ -32,94 +32,127 @@
############################################################################
px4_add_romfs_files(
# [0-999] Reserved (historical)"
# [1000, 1999] Simulation setups"
1001_rc_quad_x.hil
1002_standard_vtol.hil
1100_rc_quad_x_sih.hil
1101_rc_plane_sih.hil
1102_tailsitter_duo_sih.hil
# [2000, 2999] Standard planes"
2100_standard_plane
2106_albatross
2507_cloudship
# [3000, 3999] Flying wing"
3000_generic_wing
# [4000, 4999] Quadrotor x"
4001_quad_x
4014_s500
4015_holybro_s500
4016_holybro_px4vision
4017_nxp_hovergames
4019_x500_v2
4020_holybro_px4vision_v1_5
4041_beta75x
4050_generic_250
4052_holybro_qav250
4053_holybro_kopis2
4061_atl_mantis_edu
4071_ifo
4073_ifo-s
4500_clover4
4901_crazyflie21
# [5000, 5999] Quadrotor +"
5001_quad_+
# [6000, 6999] Hexarotor x"
6001_hexa_x
6002_draco_r
# [7000, 7999] Hexarotor +"
7001_hexa_+
# [8000, 8999] Octorotor +"
8001_octo_x
# [9000, 9999] Octorotor +"
9001_octo_+
# [11000, 11999] Hexa Cox
11001_hexa_cox
# [12000, 12999] Octo Cox
12001_octo_cox
# [13000, 13999] VTOL
13000_generic_vtol_standard
13100_generic_vtol_tiltrotor
13013_deltaquad
13014_vtol_babyshark
13030_generic_vtol_quad_tiltrotor
13200_generic_vtol_tailsitter
# [14000, 14999] MC with tilt
14001_generic_mc_with_tilt
16001_helicopter
# [17000, 17999] Autogyro
17002_TF-AutoG2
17003_TF-G2
# [0-999] Reserved (historical)
# [18000, 18999] High-altitude balloons
18001_TF-B1
# [22000, 22999] Reserve for custom models
24001_dodeca_cox
50000_generic_ground_vehicle
50004_nxpcup_car_dfrobot_gpx
50003_aion_robotics_r1_rover
# [60000, 61000] (Unmanned) Underwater Robots
60000_uuv_generic
60001_uuv_hippocampus
60002_uuv_bluerov2_heavy
)
if(CONFIG_MODULES_SIMULATION_PWM_OUT_SIM)
px4_add_romfs_files(
# [1000, 1999] Simulation setups
1001_rc_quad_x.hil
1002_standard_vtol.hil
1100_rc_quad_x_sih.hil
1101_rc_plane_sih.hil
1102_tailsitter_duo_sih.hil
)
endif()
if(CONFIG_MODULES_MC_RATE_CONTROL)
px4_add_romfs_files(
# [4000, 4999] Quadrotor x
4001_quad_x
4014_s500
4015_holybro_s500
4016_holybro_px4vision
4017_nxp_hovergames
4019_x500_v2
4020_holybro_px4vision_v1_5
4041_beta75x
4050_generic_250
4052_holybro_qav250
4053_holybro_kopis2
4061_atl_mantis_edu
4071_ifo
4073_ifo-s
4500_clover4
4901_crazyflie21
# [5000, 5999] Quadrotor +
5001_quad_+
# [6000, 6999] Hexarotor x
6001_hexa_x
6002_draco_r
# [7000, 7999] Hexarotor +
7001_hexa_+
# [8000, 8999] Octorotor +
8001_octo_x
# [9000, 9999] Octorotor +
9001_octo_+
# [11000, 11999] Hexa Cox
11001_hexa_cox
# [12000, 12999] Octo Cox
12001_octo_cox
# [14000, 14999] MC with tilt
14001_generic_mc_with_tilt
16001_helicopter
24001_dodeca_cox
)
endif()
if(CONFIG_MODULES_FW_RATE_CONTROL)
px4_add_romfs_files(
# [2000, 2999] Standard planes
2100_standard_plane
2106_albatross
# [3000, 3999] Flying wing
3000_generic_wing
# [17000, 17999] Autogyro
17002_TF-AutoG2
17003_TF-G2
)
endif()
if(CONFIG_MODULES_AIRSHIP_ATT_CONTROL)
px4_add_romfs_files(
2507_cloudship
)
endif()
if(CONFIG_MODULES_VTOL_ATT_CONTROL)
px4_add_romfs_files(
# [13000, 13999] VTOL
13000_generic_vtol_standard
13100_generic_vtol_tiltrotor
13013_deltaquad
13014_vtol_babyshark
13030_generic_vtol_quad_tiltrotor
13200_generic_vtol_tailsitter
)
endif()
if(CONFIG_MODULES_ROVER_POS_CONTROL)
px4_add_romfs_files(
50000_generic_ground_vehicle
50004_nxpcup_car_dfrobot_gpx
)
endif()
if(CONFIG_MODULES_DIFFERENTIAL_DRIVE)
px4_add_romfs_files(
50003_aion_robotics_r1_rover
)
endif()
if(CONFIG_MODULES_UUV_ATT_CONTROL)
px4_add_romfs_files(
# [60000, 61000] (Unmanned) Underwater Robots
60000_uuv_generic
60001_uuv_hippocampus
60002_uuv_bluerov2_heavy
)
endif()
@@ -28,7 +28,6 @@ param set-default EKF2_ARSP_THR 8
param set-default EKF2_FUSE_BETA 1
param set-default EKF2_GPS_CHECK 21
param set-default EKF2_MAG_ACCLIM 0
param set-default EKF2_MAG_YAWLIM 0
param set-default EKF2_REQ_EPH 10
param set-default EKF2_REQ_EPV 10
param set-default EKF2_REQ_HDRIFT 0.5
@@ -5,7 +5,7 @@
ekf2 start &
# Start rover differential drive controller.
differential_drive_control start
differential_drive start
# Start Land Detector.
land_detector start rover
+12 -2
View File
@@ -439,7 +439,12 @@ else
#
# Start a thermal calibration if required.
#
. ${R}etc/init.d/rc.thermal_cal
set RC_THERMAL_CAL ${R}etc/init.d/rc.thermal_cal
if [ -f ${RC_THERMAL_CAL} ]
then
. ${RC_THERMAL_CAL}
fi
unset RC_THERMAL_CAL
#
# Start gimbal to control mounts such as gimbals, disabled by default.
@@ -500,7 +505,12 @@ else
#
# Start the logger.
#
. ${R}etc/init.d/rc.logging
set RC_LOGGING ${R}etc/init.d/rc.logging
if [ -f ${RC_LOGGING} ]
then
. ${RC_LOGGING}
fi
unset RC_LOGGING
#
# Set additional parameters and env variables for selected AUTOSTART.
@@ -30,4 +30,5 @@ exec find boards msg src platforms test \
-path src/lib/cdrstream/cyclonedds -prune -o \
-path src/lib/cdrstream/rosidl -prune -o \
-path src/modules/zenoh/zenoh-pico -prune -o \
-path src/modules/muorb/apps/libfc-sensor-api -prune -o \
-type f \( -name "*.c" -o -name "*.h" -o -name "*.cpp" -o -name "*.hpp" \) | grep $PATTERN
+8 -1
View File
@@ -73,9 +73,16 @@ struct_size, padding_end_size = add_padding_bytes(sorted_fields, search_path)
#include <lib/matrix/matrix/math.hpp>
#include <lib/mathlib/mathlib.h>
@{
queue_length = 1
for constant in spec.constants:
if constant.name == 'ORB_QUEUE_LENGTH':
queue_length = constant.val
}@
@[for topic in topics]@
static_assert(static_cast<orb_id_size_t>(ORB_ID::@topic) == @(all_topics.index(topic)), "ORB_ID index mismatch");
ORB_DEFINE(@topic, struct @uorb_struct, @(struct_size-padding_end_size), @(message_hash)u, static_cast<orb_id_size_t>(ORB_ID::@topic));
ORB_DEFINE(@topic, struct @uorb_struct, @(struct_size-padding_end_size), @(message_hash)u, static_cast<orb_id_size_t>(ORB_ID::@topic), @queue_length);
@[end for]
void print_message(const orb_metadata *meta, const @uorb_struct& message)
-3
View File
@@ -64,9 +64,6 @@
// Hacks for MAVLink RC button input
#define ATL_MANTIS_RC_INPUT_HACKS
// Hacks for MAVLink RC button input
#define ATL_MANTIS_RC_INPUT_HACKS
/*
* ADC channels
*
+2 -1
View File
@@ -4,13 +4,13 @@ CONFIG_DRIVERS_ACTUATORS_VOXL_ESC=y
CONFIG_DRIVERS_BAROMETER_INVENSENSE_ICP101XX=y
CONFIG_DRIVERS_DISTANCE_SENSOR_VL53L0X=y
CONFIG_DRIVERS_DISTANCE_SENSOR_VL53L1X=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM42688P=y
CONFIG_DRIVERS_LIGHTS_RGBLED_NCP5623C=y
CONFIG_DRIVERS_MAGNETOMETER_ISENTEK_IST8308=y
CONFIG_DRIVERS_MAGNETOMETER_ISENTEK_IST8310=y
CONFIG_DRIVERS_MAGNETOMETER_QMC5883L=y
CONFIG_DRIVERS_POWER_MONITOR_VOXLPM=y
CONFIG_DRIVERS_QSHELL_QURT=y
CONFIG_DRIVERS_VOXL2_IO=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_EKF2=y
@@ -28,4 +28,5 @@ CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_SENSORS=y
CONFIG_MODULES_SIMULATION_PWM_OUT_SIM=y
CONFIG_SYSTEMCMDS_UORB=y
CONFIG_SYSTEMCMDS_PARAM=y
CONFIG_ORB_COMMUNICATOR=y
+1 -2
View File
@@ -44,11 +44,10 @@ add_library(drivers_board
)
# Add custom drivers for SLPI
# add_subdirectory(${PX4_BOARD_DIR}/src/drivers/icm42688p)
add_subdirectory(${PX4_BOARD_DIR}/src/drivers/rc_controller)
add_subdirectory(${PX4_BOARD_DIR}/src/drivers/mavlink_rc_in)
# add_subdirectory(${PX4_BOARD_DIR}/src/drivers/spektrum_rc)
# add_subdirectory(${PX4_BOARD_DIR}/src/drivers/ghst_rc)
# add_subdirectory(${PX4_BOARD_DIR}/src/drivers/dsp_hitl)
add_subdirectory(${PX4_BOARD_DIR}/src/drivers/dsp_hitl)
# add_subdirectory(${PX4_BOARD_DIR}/src/drivers/dsp_sbus)
add_subdirectory(${PX4_BOARD_DIR}/src/drivers/elrs_led)
@@ -989,10 +989,10 @@ handle_message_hil_gps_dsp(mavlink_message_t *msg)
gps.device_id = device_id.devid;
gps.lat = hil_gps.lat;
gps.lon = hil_gps.lon;
gps.alt = hil_gps.alt;
gps.alt_ellipsoid = hil_gps.alt;
gps.latitude_deg = hil_gps.lat;
gps.longitude_deg = hil_gps.lon;
gps.altitude_msl_m = hil_gps.alt;
gps.altitude_ellipsoid_m = hil_gps.alt;
gps.s_variance_m_s = 0.25f;
gps.c_variance_rad = 0.5f;
@@ -1,991 +0,0 @@
/****************************************************************************
*
* Copyright (c) 2020 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include "ICM42688P.hpp"
bool hitl_mode = false;
using namespace time_literals;
static constexpr int16_t combine(uint8_t msb, uint8_t lsb)
{
return (msb << 8u) | lsb;
}
ICM42688P::ICM42688P(const I2CSPIDriverConfig &config) :
// SPI(DRV_IMU_DEVTYPE_ICM42688P, MODULE_NAME, bus, device, spi_mode, bus_frequency),
// I2CSPIDriver(MODULE_NAME, px4::device_bus_to_wq(get_device_id()), bus_option, bus),
// _drdy_gpio(drdy_gpio)
SPI(config),
I2CSPIDriver(config),
_drdy_gpio(config.drdy_gpio),
_px4_accel(get_device_id(), config.rotation),
_px4_gyro(get_device_id(), config.rotation)
{
if (config.drdy_gpio != 0) {
_drdy_missed_perf = perf_alloc(PC_COUNT, MODULE_NAME": DRDY missed");
}
if (!hitl_mode) {
// _px4_accel = std::make_shared<PX4Accelerometer>(get_device_id(), rotation);
// _px4_gyro = std::make_shared<PX4Gyroscope>(get_device_id(), rotation);
ConfigureSampleRate(_px4_gyro.get_max_rate_hz());
// _imu_server_pub.advertise();
} else {
ConfigureSampleRate(0);
}
}
ICM42688P::~ICM42688P()
{
perf_free(_bad_register_perf);
perf_free(_bad_transfer_perf);
perf_free(_fifo_empty_perf);
perf_free(_fifo_overflow_perf);
perf_free(_fifo_reset_perf);
perf_free(_drdy_missed_perf);
// if (!hitl_mode){
// _imu_server_pub.unadvertise();
// }
}
int ICM42688P::init()
{
int ret = SPI::init();
if (ret != PX4_OK) {
DEVICE_DEBUG("SPI::init failed (%i)", ret);
return ret;
}
return Reset() ? 0 : -1;
}
bool ICM42688P::Reset()
{
_state = STATE::RESET;
DataReadyInterruptDisable();
ScheduleClear();
ScheduleNow();
return true;
}
void ICM42688P::exit_and_cleanup()
{
DataReadyInterruptDisable();
I2CSPIDriverBase::exit_and_cleanup();
}
void ICM42688P::print_status()
{
I2CSPIDriverBase::print_status();
PX4_INFO("FIFO empty interval: %d us (%.1f Hz)", _fifo_empty_interval_us, 1e6 / _fifo_empty_interval_us);
perf_print_counter(_bad_register_perf);
perf_print_counter(_bad_transfer_perf);
perf_print_counter(_fifo_empty_perf);
perf_print_counter(_fifo_overflow_perf);
perf_print_counter(_fifo_reset_perf);
perf_print_counter(_drdy_missed_perf);
}
int ICM42688P::probe()
{
for (int i = 0; i < 3; i++) {
uint8_t whoami = RegisterRead(Register::BANK_0::WHO_AM_I);
if (whoami == WHOAMI) {
PX4_INFO("ICM42688P::probe successful!");
return PX4_OK;
} else {
DEVICE_DEBUG("unexpected WHO_AM_I 0x%02x", whoami);
uint8_t reg_bank_sel = RegisterRead(Register::BANK_0::REG_BANK_SEL);
int bank = reg_bank_sel >> 4;
if (bank >= 1 && bank <= 3) {
DEVICE_DEBUG("incorrect register bank for WHO_AM_I REG_BANK_SEL:0x%02x, bank:%d", reg_bank_sel, bank);
// force bank selection and retry
SelectRegisterBank(REG_BANK_SEL_BIT::USER_BANK_0, true);
}
}
}
return PX4_ERROR;
}
void ICM42688P::RunImpl()
{
PX4_INFO(">>> ICM42688P this: %p", this);
const hrt_abstime now = hrt_absolute_time();
switch (_state) {
case STATE::RESET:
// DEVICE_CONFIG: Software reset configuration
RegisterWrite(Register::BANK_0::DEVICE_CONFIG, DEVICE_CONFIG_BIT::SOFT_RESET_CONFIG);
_reset_timestamp = now;
_failure_count = 0;
_state = STATE::WAIT_FOR_RESET;
ScheduleDelayed(2_ms); // to be safe wait 2 ms for soft reset to be effective
break;
case STATE::WAIT_FOR_RESET:
if ((RegisterRead(Register::BANK_0::WHO_AM_I) == WHOAMI)
&& (RegisterRead(Register::BANK_0::DEVICE_CONFIG) == 0x00)
&& (RegisterRead(Register::BANK_0::INT_STATUS) & INT_STATUS_BIT::RESET_DONE_INT)) {
_state = STATE::CONFIGURE;
ScheduleDelayed(10_ms); // 30 ms gyro startup time, 10 ms accel from sleep to valid data
} else {
// RESET not complete
if (hrt_elapsed_time(&_reset_timestamp) > 1000_ms) {
PX4_DEBUG("Reset failed, retrying");
_state = STATE::RESET;
ScheduleDelayed(100_ms);
} else {
PX4_DEBUG("Reset not complete, check again in 10 ms");
ScheduleDelayed(10_ms);
}
}
break;
case STATE::CONFIGURE:
if (Configure()) {
// Wakeup accel and gyro after configuring registers
ScheduleDelayed(1_ms); // add a delay here to be safe
RegisterWrite(Register::BANK_0::PWR_MGMT0, PWR_MGMT0_BIT::GYRO_MODE_LOW_NOISE | PWR_MGMT0_BIT::ACCEL_MODE_LOW_NOISE);
ScheduleDelayed(30_ms); // 30 ms gyro startup time, 10 ms accel from sleep to valid data
// if configure succeeded then start reading from FIFO
_state = STATE::FIFO_READ;
if (DataReadyInterruptConfigure()) {
_data_ready_interrupt_enabled = true;
// backup schedule as a watchdog timeout
ScheduleDelayed(100_ms);
} else {
PX4_ERR("ICM42688P::RunImpl interrupt configuration failed");
_data_ready_interrupt_enabled = false;
ScheduleOnInterval(_fifo_empty_interval_us, _fifo_empty_interval_us);
}
FIFOReset();
} else {
PX4_ERR("ICM42688P::RunImpl configuration failed");
// CONFIGURE not complete
if (hrt_elapsed_time(&_reset_timestamp) > 1000_ms) {
PX4_DEBUG("Configure failed, resetting");
_state = STATE::RESET;
} else {
PX4_DEBUG("Configure failed, retrying");
}
ScheduleDelayed(100_ms);
}
break;
case STATE::FIFO_READ: {
#ifndef __PX4_QURT
uint32_t samples = 0;
if (_data_ready_interrupt_enabled) {
// scheduled from interrupt if _drdy_fifo_read_samples was set as expected
if (_drdy_fifo_read_samples.fetch_and(0) != _fifo_gyro_samples) {
perf_count(_drdy_missed_perf);
} else {
samples = _fifo_gyro_samples;
}
// push backup schedule back
ScheduleDelayed(_fifo_empty_interval_us * 2);
}
if (samples == 0) {
// check current FIFO count
const uint16_t fifo_count = FIFOReadCount();
if (fifo_count >= FIFO::SIZE) {
FIFOReset();
perf_count(_fifo_overflow_perf);
} else if (fifo_count == 0) {
perf_count(_fifo_empty_perf);
} else {
// FIFO count (size in bytes)
samples = (fifo_count / sizeof(FIFO::DATA));
if (samples > FIFO_MAX_SAMPLES) {
// not technically an overflow, but more samples than we expected or can publish
FIFOReset();
perf_count(_fifo_overflow_perf);
samples = 0;
}
}
}
bool success = false;
if (samples >= 1) {
if (FIFORead(now, samples)) {
success = true;
if (_failure_count > 0) {
_failure_count--;
}
}
}
if (!success) {
_failure_count++;
// full reset if things are failing consistently
if (_failure_count > 10) {
Reset();
return;
}
}
// check configuration registers periodically or immediately following any failure
if (RegisterCheck(_register_bank0_cfg[_checked_register_bank0])
&& RegisterCheck(_register_bank1_cfg[_checked_register_bank1])
&& RegisterCheck(_register_bank2_cfg[_checked_register_bank2])
) {
_last_config_check_timestamp = now;
_checked_register_bank0 = (_checked_register_bank0 + 1) % size_register_bank0_cfg;
_checked_register_bank1 = (_checked_register_bank1 + 1) % size_register_bank1_cfg;
_checked_register_bank2 = (_checked_register_bank2 + 1) % size_register_bank2_cfg;
} else {
// register check failed, force reset
perf_count(_bad_register_perf);
Reset();
}
#endif
}
break;
}
}
void ICM42688P::ConfigureSampleRate(int sample_rate)
{
if (sample_rate == 0) {
sample_rate = 800; // default to 800 Hz
}
// round down to nearest FIFO sample dt
const float min_interval = FIFO_SAMPLE_DT;
_fifo_empty_interval_us = math::max(roundf((1e6f / (float)sample_rate) / min_interval) * min_interval, min_interval);
_fifo_gyro_samples = roundf(math::min((float)_fifo_empty_interval_us / (1e6f / GYRO_RATE), (float)FIFO_MAX_SAMPLES));
// recompute FIFO empty interval (us) with actual gyro sample limit
_fifo_empty_interval_us = _fifo_gyro_samples * (1e6f / GYRO_RATE);
ConfigureFIFOWatermark(_fifo_gyro_samples);
}
void ICM42688P::ConfigureFIFOWatermark(uint8_t samples)
{
// FIFO watermark threshold in number of bytes
const uint16_t fifo_watermark_threshold = samples * sizeof(FIFO::DATA);
for (auto &r : _register_bank0_cfg) {
if (r.reg == Register::BANK_0::FIFO_CONFIG2) {
// FIFO_WM[7:0] FIFO_CONFIG2
r.set_bits = fifo_watermark_threshold & 0xFF;
} else if (r.reg == Register::BANK_0::FIFO_CONFIG3) {
// FIFO_WM[11:8] FIFO_CONFIG3
r.set_bits = (fifo_watermark_threshold >> 8) & 0x0F;
}
}
}
void ICM42688P::SelectRegisterBank(enum REG_BANK_SEL_BIT bank, bool force)
{
if (bank != _last_register_bank || force) {
// select BANK_0
uint8_t cmd_bank_sel[2] {};
cmd_bank_sel[0] = static_cast<uint8_t>(Register::BANK_0::REG_BANK_SEL);
cmd_bank_sel[1] = bank;
transfer(cmd_bank_sel, cmd_bank_sel, sizeof(cmd_bank_sel));
_last_register_bank = bank;
}
}
bool ICM42688P::Configure()
{
// first set and clear all configured register bits
for (const auto &reg_cfg : _register_bank0_cfg) {
RegisterSetAndClearBits(reg_cfg.reg, reg_cfg.set_bits, reg_cfg.clear_bits);
}
for (const auto &reg_cfg : _register_bank1_cfg) {
RegisterSetAndClearBits(reg_cfg.reg, reg_cfg.set_bits, reg_cfg.clear_bits);
}
for (const auto &reg_cfg : _register_bank2_cfg) {
RegisterSetAndClearBits(reg_cfg.reg, reg_cfg.set_bits, reg_cfg.clear_bits);
}
// now check that all are configured
bool success = true;
for (const auto &reg_cfg : _register_bank0_cfg) {
if (!RegisterCheck(reg_cfg)) {
success = false;
}
}
for (const auto &reg_cfg : _register_bank1_cfg) {
if (!RegisterCheck(reg_cfg)) {
success = false;
}
}
for (const auto &reg_cfg : _register_bank2_cfg) {
if (!RegisterCheck(reg_cfg)) {
success = false;
}
}
// // 20-bits data format used
// // the only FSR settings that are operational are ±2000dps for gyroscope and ±16g for accelerometer
if (!hitl_mode) {
_px4_accel.set_range(16.f * CONSTANTS_ONE_G);
_px4_accel.set_scale(CONSTANTS_ONE_G / 8192.f);
_px4_gyro.set_range(math::radians(2000.f));
_px4_gyro.set_scale(math::radians(1.f / 131.f));
}
return success;
}
static bool interrupt_debug = false;
static uint32_t interrupt_debug_count = 0;
static const uint32_t interrupt_debug_trigger = 800;
static hrt_abstime last_interrupt_time = 0;
static hrt_abstime avg_interrupt_delta = 0;
static hrt_abstime max_interrupt_delta = 0;
static hrt_abstime min_interrupt_delta = 60 * 1000 * 1000;
static hrt_abstime cumulative_interrupt_delta = 0;
int ICM42688P::DataReadyInterruptCallback(int irq, void *context, void *arg)
{
hrt_abstime current_interrupt_time = hrt_absolute_time();
if (interrupt_debug) {
if (last_interrupt_time) {
hrt_abstime interrupt_delta_time = current_interrupt_time - last_interrupt_time;
if (interrupt_delta_time > max_interrupt_delta) { max_interrupt_delta = interrupt_delta_time; }
if (interrupt_delta_time < min_interrupt_delta) { min_interrupt_delta = interrupt_delta_time; }
cumulative_interrupt_delta += interrupt_delta_time;
}
last_interrupt_time = current_interrupt_time;
interrupt_debug_count++;
if (interrupt_debug_count == interrupt_debug_trigger) {
avg_interrupt_delta = cumulative_interrupt_delta / interrupt_debug_trigger;
PX4_INFO(">>> Max: %llu, Min: %llu, Avg: %llu", max_interrupt_delta,
min_interrupt_delta, avg_interrupt_delta);
interrupt_debug_count = 0;
cumulative_interrupt_delta = 0;
}
}
static_cast<ICM42688P *>(arg)->DataReady();
return 0;
}
void ICM42688P::DataReady()
{
#ifndef __PX4_QURT
uint32_t expected = 0;
if (_drdy_fifo_read_samples.compare_exchange(&expected, _fifo_gyro_samples)) {
ScheduleNow();
}
#else
uint16_t fifo_byte_count = FIFOReadCount();
FIFORead(hrt_absolute_time(), fifo_byte_count / sizeof(FIFO::DATA));
#endif
}
bool ICM42688P::DataReadyInterruptConfigure()
{
if (_drdy_gpio == 0) {
return false;
}
// Setup data ready on falling edge
return px4_arch_gpiosetevent(_drdy_gpio, false, true, true, &DataReadyInterruptCallback, this) == 0;
}
bool ICM42688P::DataReadyInterruptDisable()
{
if (_drdy_gpio == 0) {
return false;
}
return px4_arch_gpiosetevent(_drdy_gpio, false, false, false, nullptr, nullptr) == 0;
}
template <typename T>
bool ICM42688P::RegisterCheck(const T &reg_cfg)
{
bool success = true;
const uint8_t reg_value = RegisterRead(reg_cfg.reg);
if (reg_cfg.set_bits && ((reg_value & reg_cfg.set_bits) != reg_cfg.set_bits)) {
PX4_DEBUG("0x%02hhX: 0x%02hhX (0x%02hhX not set)", (uint8_t)reg_cfg.reg, reg_value, reg_cfg.set_bits);
success = false;
}
if (reg_cfg.clear_bits && ((reg_value & reg_cfg.clear_bits) != 0)) {
PX4_DEBUG("0x%02hhX: 0x%02hhX (0x%02hhX not cleared)", (uint8_t)reg_cfg.reg, reg_value, reg_cfg.clear_bits);
success = false;
}
return success;
}
template <typename T>
uint8_t ICM42688P::RegisterRead(T reg)
{
uint8_t cmd[2] {};
cmd[0] = static_cast<uint8_t>(reg) | DIR_READ;
SelectRegisterBank(reg);
transfer(cmd, cmd, sizeof(cmd));
return cmd[1];
}
template <typename T>
void ICM42688P::RegisterWrite(T reg, uint8_t value)
{
uint8_t cmd[2] { (uint8_t)reg, value };
SelectRegisterBank(reg);
transfer(cmd, cmd, sizeof(cmd));
}
template <typename T>
void ICM42688P::RegisterSetAndClearBits(T reg, uint8_t setbits, uint8_t clearbits)
{
const uint8_t orig_val = RegisterRead(reg);
uint8_t val = (orig_val & ~clearbits) | setbits;
if (orig_val != val) {
RegisterWrite(reg, val);
}
}
uint16_t ICM42688P::FIFOReadCount()
{
// read FIFO count
uint8_t fifo_count_buf[3] {};
fifo_count_buf[0] = static_cast<uint8_t>(Register::BANK_0::FIFO_COUNTH) | DIR_READ;
SelectRegisterBank(REG_BANK_SEL_BIT::USER_BANK_0);
if (transfer(fifo_count_buf, fifo_count_buf, sizeof(fifo_count_buf)) != PX4_OK) {
perf_count(_bad_transfer_perf);
return 0;
}
return combine(fifo_count_buf[1], fifo_count_buf[2]);
}
// static uint32_t debug_decimator = 0;
// static hrt_abstime last_sample_time = 0;
// static bool imu_debug = true;
bool ICM42688P::FIFORead(const hrt_abstime &timestamp_sample, uint16_t samples)
{
FIFOTransferBuffer buffer{};
const size_t max_transfer_size = 10 * sizeof(FIFO::DATA) + 4;
const size_t transfer_size = math::min(samples * sizeof(FIFO::DATA) + 4, max_transfer_size);
SelectRegisterBank(REG_BANK_SEL_BIT::USER_BANK_0);
if (transfer((uint8_t *)&buffer, (uint8_t *)&buffer, transfer_size) != PX4_OK) {
perf_count(_bad_transfer_perf);
return false;
}
if (buffer.INT_STATUS & INT_STATUS_BIT::FIFO_FULL_INT) {
perf_count(_fifo_overflow_perf);
FIFOReset();
return false;
}
const uint16_t fifo_count_bytes = combine(buffer.FIFO_COUNTH, buffer.FIFO_COUNTL);
if (fifo_count_bytes >= FIFO::SIZE) {
perf_count(_fifo_overflow_perf);
FIFOReset();
return false;
}
const uint16_t fifo_count_samples = fifo_count_bytes / sizeof(FIFO::DATA);
if (fifo_count_samples == 0) {
perf_count(_fifo_empty_perf);
return false;
}
// check FIFO header in every sample
uint16_t valid_samples = 0;
// for (int i = 0; i < math::min(samples, fifo_count_samples); i++) {
for (int i = 0; i < math::min(samples, (uint16_t) 10); i++) {
bool valid = true;
// With FIFO_ACCEL_EN and FIFO_GYRO_EN header should be 8b_0110_10xx
const uint8_t FIFO_HEADER = buffer.f[i].FIFO_Header;
if (FIFO_HEADER & FIFO::FIFO_HEADER_BIT::HEADER_MSG) {
// FIFO sample empty if HEADER_MSG set
valid = false;
} else if (!(FIFO_HEADER & FIFO::FIFO_HEADER_BIT::HEADER_ACCEL)) {
// accel bit not set
valid = false;
} else if (!(FIFO_HEADER & FIFO::FIFO_HEADER_BIT::HEADER_GYRO)) {
// gyro bit not set
valid = false;
} else if (!(FIFO_HEADER & FIFO::FIFO_HEADER_BIT::HEADER_20)) {
// Packet does not contain a new and valid extended 20-bit data
valid = false;
} else if (FIFO_HEADER & FIFO::FIFO_HEADER_BIT::HEADER_ODR_ACCEL) {
// accel ODR changed
valid = false;
} else if (FIFO_HEADER & FIFO::FIFO_HEADER_BIT::HEADER_ODR_GYRO) {
// gyro ODR changed
valid = false;
}
if (valid) {
valid_samples++;
} else {
perf_count(_bad_transfer_perf);
break;
}
}
// if (imu_debug) {
// debug_decimator++;
// if (debug_decimator == 801) {
// debug_decimator = 0;
// PX4_INFO("Initial: %u Next: %u Valid: %u Delta: %llu", samples, fifo_count_samples, valid_samples, timestamp_sample - last_sample_time);
// }
// last_sample_time = timestamp_sample;
// }
if (valid_samples > 0) {
if (ProcessTemperature(buffer.f, valid_samples)) {
ProcessGyro(timestamp_sample, buffer.f, valid_samples);
ProcessAccel(timestamp_sample, buffer.f, valid_samples);
ProcessIMU(timestamp_sample, buffer.f, valid_samples);
return true;
}
}
return false;
}
void ICM42688P::FIFOReset()
{
perf_count(_fifo_reset_perf);
// SIGNAL_PATH_RESET: FIFO flush
RegisterSetBits(Register::BANK_0::SIGNAL_PATH_RESET, SIGNAL_PATH_RESET_BIT::FIFO_FLUSH);
// reset while FIFO is disabled
_drdy_fifo_read_samples.store(0);
}
static constexpr int32_t reassemble_20bit(const uint32_t a, const uint32_t b, const uint32_t c)
{
// 0xXXXAABBC
uint32_t high = ((a << 12) & 0x000FF000);
uint32_t low = ((b << 4) & 0x00000FF0);
uint32_t lowest = (c & 0x0000000F);
uint32_t x = high | low | lowest;
if (a & Bit7) {
// sign extend
x |= 0xFFF00000u;
}
return static_cast<int32_t>(x);
}
void ICM42688P::ProcessIMU(const hrt_abstime &timestamp_sample, const FIFO::DATA fifo[], const uint8_t samples)
{
float accel_x = 0.0, accel_y = 0.0, accel_z = 0.0;
float gyro_x = 0.0, gyro_y = 0.0, gyro_z = 0.0;
for (int i = 0; i < samples; i++) {
_imu_server_decimator++;
if (_imu_server_decimator == 8) {
_imu_server_decimator = 0;
// 20 bit hires mode
// Sign extension + Accel [19:12] + Accel [11:4] + Accel [3:2] (20 bit extension byte)
// Accel data is 18 bit
int32_t temp_accel_x = reassemble_20bit(fifo[i].ACCEL_DATA_X1, fifo[i].ACCEL_DATA_X0,
fifo[i].Ext_Accel_X_Gyro_X & 0xF0 >> 4);
int32_t temp_accel_y = reassemble_20bit(fifo[i].ACCEL_DATA_Y1, fifo[i].ACCEL_DATA_Y0,
fifo[i].Ext_Accel_Y_Gyro_Y & 0xF0 >> 4);
int32_t temp_accel_z = reassemble_20bit(fifo[i].ACCEL_DATA_Z1, fifo[i].ACCEL_DATA_Z0,
fifo[i].Ext_Accel_Z_Gyro_Z & 0xF0 >> 4);
// Gyro [19:12] + Gyro [11:4] + Gyro [3:0] (bottom 4 bits of 20 bit extension byte)
int32_t temp_gyro_x = reassemble_20bit(fifo[i].GYRO_DATA_X1, fifo[i].GYRO_DATA_X0,
fifo[i].Ext_Accel_X_Gyro_X & 0x0F);
int32_t temp_gyro_y = reassemble_20bit(fifo[i].GYRO_DATA_Y1, fifo[i].GYRO_DATA_Y0,
fifo[i].Ext_Accel_Y_Gyro_Y & 0x0F);
int32_t temp_gyro_z = reassemble_20bit(fifo[i].GYRO_DATA_Z1, fifo[i].GYRO_DATA_Z0,
fifo[i].Ext_Accel_Z_Gyro_Z & 0x0F);
// accel samples invalid if -524288
if (temp_accel_x != -524288 && temp_accel_y != -524288 && temp_accel_z != -524288) {
// shift accel by 2 (2 least significant bits are always 0)
accel_x = (float) temp_accel_x / 4.f;
accel_y = (float) temp_accel_y / 4.f;
accel_z = (float) temp_accel_z / 4.f;
// shift gyro by 1 (least significant bit is always 0)
gyro_x = (float) temp_gyro_x / 2.f;
gyro_y = (float) temp_gyro_y / 2.f;
gyro_z = (float) temp_gyro_z / 2.f;
// correct frame for publication
// sensor's frame is +x forward, +y left, +z up
// flip y & z to publish right handed with z down (x forward, y right, z down)
accel_y = -accel_y;
accel_z = -accel_z;
gyro_y = -gyro_y;
gyro_z = -gyro_z;
// Scale everything appropriately
float accel_scale_factor = (CONSTANTS_ONE_G / 8192.f);
accel_x *= accel_scale_factor;
accel_y *= accel_scale_factor;
accel_z *= accel_scale_factor;
float gyro_scale_factor = math::radians(1.f / 131.f);
gyro_x *= gyro_scale_factor;
gyro_y *= gyro_scale_factor;
gyro_z *= gyro_scale_factor;
// Store the data in our array
_imu_server_data.accel_x[_imu_server_index] = accel_x;
_imu_server_data.accel_y[_imu_server_index] = accel_y;
_imu_server_data.accel_z[_imu_server_index] = accel_z;
_imu_server_data.gyro_x[_imu_server_index] = gyro_x;
_imu_server_data.gyro_y[_imu_server_index] = gyro_y;
_imu_server_data.gyro_z[_imu_server_index] = gyro_z;
_imu_server_data.ts[_imu_server_index] = timestamp_sample - (125 * (samples - 1 - i));
_imu_server_index++;
// If array is full, publish the data
if (_imu_server_index == 10) {
_imu_server_index = 0;
_imu_server_data.timestamp = hrt_absolute_time();
_imu_server_data.temperature = 0; // Not used right now
_imu_server_pub.publish(_imu_server_data);
}
}
}
}
}
void ICM42688P::ProcessAccel(const hrt_abstime &timestamp_sample, const FIFO::DATA fifo[], const uint8_t samples)
{
sensor_accel_fifo_s accel{};
accel.timestamp_sample = timestamp_sample;
accel.samples = 0;
accel.dt = FIFO_SAMPLE_DT;
// 18-bits of accelerometer data
bool scale_20bit = false;
// first pass
for (int i = 0; i < samples; i++) {
// 20 bit hires mode
// Sign extension + Accel [19:12] + Accel [11:4] + Accel [3:2] (20 bit extension byte)
// Accel data is 18 bit ()
int32_t accel_x = reassemble_20bit(fifo[i].ACCEL_DATA_X1, fifo[i].ACCEL_DATA_X0,
fifo[i].Ext_Accel_X_Gyro_X & 0xF0 >> 4);
int32_t accel_y = reassemble_20bit(fifo[i].ACCEL_DATA_Y1, fifo[i].ACCEL_DATA_Y0,
fifo[i].Ext_Accel_Y_Gyro_Y & 0xF0 >> 4);
int32_t accel_z = reassemble_20bit(fifo[i].ACCEL_DATA_Z1, fifo[i].ACCEL_DATA_Z0,
fifo[i].Ext_Accel_Z_Gyro_Z & 0xF0 >> 4);
// sample invalid if -524288
if (accel_x != -524288 && accel_y != -524288 && accel_z != -524288) {
// check if any values are going to exceed int16 limits
static constexpr int16_t max_accel = INT16_MAX;
static constexpr int16_t min_accel = INT16_MIN;
if (accel_x >= max_accel || accel_x <= min_accel) {
scale_20bit = true;
}
if (accel_y >= max_accel || accel_y <= min_accel) {
scale_20bit = true;
}
if (accel_z >= max_accel || accel_z <= min_accel) {
scale_20bit = true;
}
// shift by 2 (2 least significant bits are always 0)
accel.x[accel.samples] = accel_x / 4;
accel.y[accel.samples] = accel_y / 4;
accel.z[accel.samples] = accel_z / 4;
accel.samples++;
}
}
if (!scale_20bit) {
// if highres enabled accel data is always 8192 LSB/g
if (!hitl_mode) {
_px4_accel.set_scale(CONSTANTS_ONE_G / 8192.f);
}
} else {
// 20 bit data scaled to 16 bit (2^4)
for (int i = 0; i < samples; i++) {
// 20 bit hires mode
// Sign extension + Accel [19:12] + Accel [11:4] + Accel [3:2] (20 bit extension byte)
// Accel data is 18 bit ()
int16_t accel_x = combine(fifo[i].ACCEL_DATA_X1, fifo[i].ACCEL_DATA_X0);
int16_t accel_y = combine(fifo[i].ACCEL_DATA_Y1, fifo[i].ACCEL_DATA_Y0);
int16_t accel_z = combine(fifo[i].ACCEL_DATA_Z1, fifo[i].ACCEL_DATA_Z0);
accel.x[i] = accel_x;
accel.y[i] = accel_y;
accel.z[i] = accel_z;
}
if (!hitl_mode) {
_px4_accel.set_scale(CONSTANTS_ONE_G / 2048.f);
}
}
// correct frame for publication
for (int i = 0; i < accel.samples; i++) {
// sensor's frame is +x forward, +y left, +z up
// flip y & z to publish right handed with z down (x forward, y right, z down)
accel.x[i] = accel.x[i];
accel.y[i] = (accel.y[i] == INT16_MIN) ? INT16_MAX : -accel.y[i];
accel.z[i] = (accel.z[i] == INT16_MIN) ? INT16_MAX : -accel.z[i];
}
if (!hitl_mode) {
_px4_accel.set_error_count(perf_event_count(_bad_register_perf) + perf_event_count(_bad_transfer_perf) +
perf_event_count(_fifo_empty_perf) + perf_event_count(_fifo_overflow_perf));
}
if (accel.samples > 0) {
if (!hitl_mode) {
_px4_accel.updateFIFO(accel);
}
}
}
void ICM42688P::ProcessGyro(const hrt_abstime &timestamp_sample, const FIFO::DATA fifo[], const uint8_t samples)
{
sensor_gyro_fifo_s gyro{};
gyro.timestamp_sample = timestamp_sample;
gyro.samples = 0;
gyro.dt = FIFO_SAMPLE_DT;
// 20-bits of gyroscope data
bool scale_20bit = false;
// first pass
for (int i = 0; i < samples; i++) {
// 20 bit hires mode
// Gyro [19:12] + Gyro [11:4] + Gyro [3:0] (bottom 4 bits of 20 bit extension byte)
int32_t gyro_x = reassemble_20bit(fifo[i].GYRO_DATA_X1, fifo[i].GYRO_DATA_X0, fifo[i].Ext_Accel_X_Gyro_X & 0x0F);
int32_t gyro_y = reassemble_20bit(fifo[i].GYRO_DATA_Y1, fifo[i].GYRO_DATA_Y0, fifo[i].Ext_Accel_Y_Gyro_Y & 0x0F);
int32_t gyro_z = reassemble_20bit(fifo[i].GYRO_DATA_Z1, fifo[i].GYRO_DATA_Z0, fifo[i].Ext_Accel_Z_Gyro_Z & 0x0F);
// check if any values are going to exceed int16 limits
static constexpr int16_t max_gyro = INT16_MAX;
static constexpr int16_t min_gyro = INT16_MIN;
if (gyro_x >= max_gyro || gyro_x <= min_gyro) {
scale_20bit = true;
}
if (gyro_y >= max_gyro || gyro_y <= min_gyro) {
scale_20bit = true;
}
if (gyro_z >= max_gyro || gyro_z <= min_gyro) {
scale_20bit = true;
}
gyro.x[gyro.samples] = gyro_x / 2;
gyro.y[gyro.samples] = gyro_y / 2;
gyro.z[gyro.samples] = gyro_z / 2;
gyro.samples++;
}
if (!scale_20bit) {
// if highres enabled gyro data is always 131 LSB/dps
if (!hitl_mode) {
_px4_gyro.set_scale(math::radians(1.f / 131.f));
}
} else {
// 20 bit data scaled to 16 bit (2^4)
for (int i = 0; i < samples; i++) {
gyro.x[i] = combine(fifo[i].GYRO_DATA_X1, fifo[i].GYRO_DATA_X0);
gyro.y[i] = combine(fifo[i].GYRO_DATA_Y1, fifo[i].GYRO_DATA_Y0);
gyro.z[i] = combine(fifo[i].GYRO_DATA_Z1, fifo[i].GYRO_DATA_Z0);
}
if (!hitl_mode) {
_px4_gyro.set_scale(math::radians(2000.f / 32768.f));
}
}
// correct frame for publication
for (int i = 0; i < gyro.samples; i++) {
// sensor's frame is +x forward, +y left, +z up
// flip y & z to publish right handed with z down (x forward, y right, z down)
gyro.x[i] = gyro.x[i];
gyro.y[i] = (gyro.y[i] == INT16_MIN) ? INT16_MAX : -gyro.y[i];
gyro.z[i] = (gyro.z[i] == INT16_MIN) ? INT16_MAX : -gyro.z[i];
}
if (!hitl_mode) {
_px4_gyro.set_error_count(perf_event_count(_bad_register_perf) + perf_event_count(_bad_transfer_perf) +
perf_event_count(_fifo_empty_perf) + perf_event_count(_fifo_overflow_perf));
}
if (gyro.samples > 0) {
if (!hitl_mode) {
_px4_gyro.updateFIFO(gyro);
}
}
}
bool ICM42688P::ProcessTemperature(const FIFO::DATA fifo[], const uint8_t samples)
{
int16_t temperature[FIFO_MAX_SAMPLES];
float temperature_sum{0};
int valid_samples = 0;
for (int i = 0; i < samples; i++) {
const int16_t t = combine(fifo[i].TEMP_DATA1, fifo[i].TEMP_DATA0);
// sample invalid if -32768
if (t != -32768) {
temperature_sum += t;
temperature[valid_samples] = t;
valid_samples++;
}
}
if (valid_samples > 0) {
const float temperature_avg = temperature_sum / valid_samples;
for (int i = 0; i < valid_samples; i++) {
// temperature changing wildly is an indication of a transfer error
if (fabsf(temperature[i] - temperature_avg) > 1000) {
perf_count(_bad_transfer_perf);
return false;
}
}
// use average temperature reading
const float TEMP_degC = (temperature_avg / TEMPERATURE_SENSITIVITY) + TEMPERATURE_OFFSET;
if (PX4_ISFINITE(TEMP_degC)) {
if (!hitl_mode) {
_px4_accel.set_temperature(TEMP_degC);
_px4_gyro.set_temperature(TEMP_degC);
return true;
}
} else {
perf_count(_bad_transfer_perf);
}
}
return false;
}
@@ -1,235 +0,0 @@
/****************************************************************************
*
* Copyright (c) 2020 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file ICM42688P.hpp
*
* Driver for the Invensense ICM42688P connected via SPI.
*
*/
#pragma once
#include "InvenSense_ICM42688P_registers.hpp"
#include <drivers/drv_hrt.h>
#include <lib/drivers/accelerometer/PX4Accelerometer.hpp>
#include <lib/drivers/device/spi.h>
#include <lib/drivers/gyroscope/PX4Gyroscope.hpp>
#include <lib/geo/geo.h>
#include <lib/perf/perf_counter.h>
#include <px4_platform_common/atomic.h>
#include <px4_platform_common/i2c_spi_buses.h>
#include <uORB/topics/imu_server.h>
#include <uORB/topics/sensor_accel_fifo.h>
#include <uORB/topics/sensor_gyro_fifo.h>
#include <memory>
using namespace InvenSense_ICM42688P;
extern bool hitl_mode;
class ICM42688P : public device::SPI, public I2CSPIDriver<ICM42688P>
{
public:
// ICM42688P(I2CSPIBusOption bus_option, int bus, uint32_t device, enum Rotation rotation, int bus_frequency,
// spi_mode_e spi_mode, spi_drdy_gpio_t drdy_gpio);
ICM42688P(const I2CSPIDriverConfig &config);
~ICM42688P() override;
// static I2CSPIDriverBase *instantiate(const BusCLIArguments &cli, const BusInstanceIterator &iterator,
// int runtime_instance);
static void print_usage();
void RunImpl();
int init() override;
void print_status() override;
private:
void exit_and_cleanup() override;
// Sensor Configuration
static constexpr float IMU_ODR{8000.f}; // 8kHz accel & gyro ODR configured
static constexpr float FIFO_SAMPLE_DT{1e6f / IMU_ODR};
static constexpr float GYRO_RATE{1e6f / FIFO_SAMPLE_DT};
static constexpr float ACCEL_RATE{1e6f / FIFO_SAMPLE_DT};
// maximum FIFO samples per transfer is limited to the size of sensor_accel_fifo/sensor_gyro_fifo
// static constexpr uint32_t FIFO_MAX_SAMPLES{math::min(math::min(FIFO::SIZE / sizeof(FIFO::DATA), sizeof(sensor_gyro_fifo_s::x) / sizeof(sensor_gyro_fifo_s::x[0])), sizeof(sensor_accel_fifo_s::x) / sizeof(sensor_accel_fifo_s::x[0]) * (int)(GYRO_RATE / ACCEL_RATE))};
static constexpr uint32_t FIFO_MAX_SAMPLES{10};
// Transfer data
struct FIFOTransferBuffer {
uint8_t cmd{static_cast<uint8_t>(Register::BANK_0::INT_STATUS) | DIR_READ};
uint8_t INT_STATUS{0};
uint8_t FIFO_COUNTH{0};
uint8_t FIFO_COUNTL{0};
FIFO::DATA f[FIFO_MAX_SAMPLES] {};
};
// ensure no struct padding
static_assert(sizeof(FIFOTransferBuffer) == (4 + FIFO_MAX_SAMPLES *sizeof(FIFO::DATA)),
"Invalid FIFOTransferBuffer size");
struct register_bank0_config_t {
Register::BANK_0 reg;
uint8_t set_bits{0};
uint8_t clear_bits{0};
};
struct register_bank1_config_t {
Register::BANK_1 reg;
uint8_t set_bits{0};
uint8_t clear_bits{0};
};
struct register_bank2_config_t {
Register::BANK_2 reg;
uint8_t set_bits{0};
uint8_t clear_bits{0};
};
int probe() override;
bool Reset();
bool Configure();
void ConfigureSampleRate(int sample_rate);
void ConfigureFIFOWatermark(uint8_t samples);
void SelectRegisterBank(enum REG_BANK_SEL_BIT bank, bool force = false);
void SelectRegisterBank(Register::BANK_0 reg) { SelectRegisterBank(REG_BANK_SEL_BIT::USER_BANK_0); }
void SelectRegisterBank(Register::BANK_1 reg) { SelectRegisterBank(REG_BANK_SEL_BIT::USER_BANK_1); }
void SelectRegisterBank(Register::BANK_2 reg) { SelectRegisterBank(REG_BANK_SEL_BIT::USER_BANK_2); }
static int DataReadyInterruptCallback(int irq, void *context, void *arg);
void DataReady();
bool DataReadyInterruptConfigure();
bool DataReadyInterruptDisable();
template <typename T> bool RegisterCheck(const T &reg_cfg);
template <typename T> uint8_t RegisterRead(T reg);
template <typename T> void RegisterWrite(T reg, uint8_t value);
template <typename T> void RegisterSetAndClearBits(T reg, uint8_t setbits, uint8_t clearbits);
template <typename T> void RegisterSetBits(T reg, uint8_t setbits) { RegisterSetAndClearBits(reg, setbits, 0); }
template <typename T> void RegisterClearBits(T reg, uint8_t clearbits) { RegisterSetAndClearBits(reg, 0, clearbits); }
uint16_t FIFOReadCount();
bool FIFORead(const hrt_abstime &timestamp_sample, uint16_t samples);
void FIFOReset();
void ProcessIMU(const hrt_abstime &timestamp_sample, const FIFO::DATA fifo[], const uint8_t samples);
void ProcessAccel(const hrt_abstime &timestamp_sample, const FIFO::DATA fifo[], const uint8_t samples);
void ProcessGyro(const hrt_abstime &timestamp_sample, const FIFO::DATA fifo[], const uint8_t samples);
bool ProcessTemperature(const FIFO::DATA fifo[], const uint8_t samples);
const spi_drdy_gpio_t _drdy_gpio;
// std::shared_ptr<PX4Accelerometer> _px4_accel;
// std::shared_ptr<PX4Gyroscope> _px4_gyro;
PX4Accelerometer _px4_accel;
PX4Gyroscope _px4_gyro;
perf_counter_t _bad_register_perf{perf_alloc(PC_COUNT, MODULE_NAME": bad register")};
perf_counter_t _bad_transfer_perf{perf_alloc(PC_COUNT, MODULE_NAME": bad transfer")};
perf_counter_t _fifo_empty_perf{perf_alloc(PC_COUNT, MODULE_NAME": FIFO empty")};
perf_counter_t _fifo_overflow_perf{perf_alloc(PC_COUNT, MODULE_NAME": FIFO overflow")};
perf_counter_t _fifo_reset_perf{perf_alloc(PC_COUNT, MODULE_NAME": FIFO reset")};
perf_counter_t _drdy_missed_perf{nullptr};
hrt_abstime _reset_timestamp{0};
hrt_abstime _last_config_check_timestamp{0};
hrt_abstime _temperature_update_timestamp{0};
int _failure_count{0};
enum REG_BANK_SEL_BIT _last_register_bank {REG_BANK_SEL_BIT::USER_BANK_0};
px4::atomic<uint32_t> _drdy_fifo_read_samples{0};
bool _data_ready_interrupt_enabled{false};
enum class STATE : uint8_t {
RESET,
WAIT_FOR_RESET,
CONFIGURE,
FIFO_READ,
} _state{STATE::RESET};
uint16_t _fifo_empty_interval_us{1250}; // default 1250 us / 800 Hz transfer interval
uint32_t _fifo_gyro_samples{static_cast<uint32_t>(_fifo_empty_interval_us / (1000000 / GYRO_RATE))};
uint8_t _checked_register_bank0{0};
static constexpr uint8_t size_register_bank0_cfg{12};
register_bank0_config_t _register_bank0_cfg[size_register_bank0_cfg] {
// Register | Set bits, Clear bits
{ Register::BANK_0::INT_CONFIG, INT_CONFIG_BIT::INT1_MODE | INT_CONFIG_BIT::INT1_DRIVE_CIRCUIT, INT_CONFIG_BIT::INT1_POLARITY },
{ Register::BANK_0::FIFO_CONFIG, FIFO_CONFIG_BIT::FIFO_MODE_STOP_ON_FULL, 0 },
{ Register::BANK_0::GYRO_CONFIG0, GYRO_CONFIG0_BIT::GYRO_FS_SEL_2000_DPS | GYRO_CONFIG0_BIT::GYRO_ODR_8KHZ_SET, GYRO_CONFIG0_BIT::GYRO_ODR_8KHZ_CLEAR },
{ Register::BANK_0::ACCEL_CONFIG0, ACCEL_CONFIG0_BIT::ACCEL_FS_SEL_16G | ACCEL_CONFIG0_BIT::ACCEL_ODR_8KHZ_SET, ACCEL_CONFIG0_BIT::ACCEL_ODR_8KHZ_CLEAR },
{ Register::BANK_0::GYRO_CONFIG1, 0, GYRO_CONFIG1_BIT::GYRO_UI_FILT_ORD },
{ Register::BANK_0::GYRO_ACCEL_CONFIG0, 0, GYRO_ACCEL_CONFIG0_BIT::ACCEL_UI_FILT_BW | GYRO_ACCEL_CONFIG0_BIT::GYRO_UI_FILT_BW },
{ Register::BANK_0::ACCEL_CONFIG1, 0, ACCEL_CONFIG1_BIT::ACCEL_UI_FILT_ORD },
{ Register::BANK_0::FIFO_CONFIG1, FIFO_CONFIG1_BIT::FIFO_WM_GT_TH | FIFO_CONFIG1_BIT::FIFO_HIRES_EN | FIFO_CONFIG1_BIT::FIFO_TEMP_EN | FIFO_CONFIG1_BIT::FIFO_GYRO_EN | FIFO_CONFIG1_BIT::FIFO_ACCEL_EN, 0 },
{ Register::BANK_0::FIFO_CONFIG2, 0, 0 }, // FIFO_WM[7:0] set at runtime
{ Register::BANK_0::FIFO_CONFIG3, 0, 0 }, // FIFO_WM[11:8] set at runtime
{ Register::BANK_0::INT_CONFIG0, INT_CONFIG0_BIT::CLEAR_ON_FIFO_READ, 0 },
{ Register::BANK_0::INT_SOURCE0, INT_SOURCE0_BIT::FIFO_THS_INT1_EN, 0 },
};
uint8_t _checked_register_bank1{0};
static constexpr uint8_t size_register_bank1_cfg{4};
register_bank1_config_t _register_bank1_cfg[size_register_bank1_cfg] {
// Register | Set bits, Clear bits
{ Register::BANK_1::GYRO_CONFIG_STATIC2, 0, GYRO_CONFIG_STATIC2_BIT::GYRO_NF_DIS | GYRO_CONFIG_STATIC2_BIT::GYRO_AAF_DIS },
{ Register::BANK_1::GYRO_CONFIG_STATIC3, GYRO_CONFIG_STATIC3_BIT::GYRO_AAF_DELT_SET, GYRO_CONFIG_STATIC3_BIT::GYRO_AAF_DELT_CLEAR},
{ Register::BANK_1::GYRO_CONFIG_STATIC4, GYRO_CONFIG_STATIC4_BIT::GYRO_AAF_DELTSQR_LOW_SET, GYRO_CONFIG_STATIC4_BIT::GYRO_AAF_DELTSQR_LOW_CLEAR},
{ Register::BANK_1::GYRO_CONFIG_STATIC5, GYRO_CONFIG_STATIC5_BIT::GYRO_AAF_BITSHIFT_SET | GYRO_CONFIG_STATIC5_BIT::GYRO_AAF_DELTSQR_HIGH_SET, GYRO_CONFIG_STATIC5_BIT::GYRO_AAF_BITSHIFT_CLEAR | GYRO_CONFIG_STATIC5_BIT::GYRO_AAF_DELTSQR_HIGH_CLEAR},
};
uint8_t _checked_register_bank2{0};
static constexpr uint8_t size_register_bank2_cfg{3};
register_bank2_config_t _register_bank2_cfg[size_register_bank2_cfg] {
// Register | Set bits, Clear bits
{ Register::BANK_2::ACCEL_CONFIG_STATIC2, ACCEL_CONFIG_STATIC2_BIT::ACCEL_AAF_DELT_SET, ACCEL_CONFIG_STATIC2_BIT::ACCEL_AAF_DELT_CLEAR | ACCEL_CONFIG_STATIC2_BIT::ACCEL_AAF_DIS },
{ Register::BANK_2::ACCEL_CONFIG_STATIC3, ACCEL_CONFIG_STATIC3_BIT::ACCEL_AAF_DELTSQR_LOW_SET, ACCEL_CONFIG_STATIC3_BIT::ACCEL_AAF_DELTSQR_LOW_CLEAR },
{ Register::BANK_2::ACCEL_CONFIG_STATIC4, ACCEL_CONFIG_STATIC4_BIT::ACCEL_AAF_BITSHIFT_SET | ACCEL_CONFIG_STATIC4_BIT::ACCEL_AAF_DELTSQR_HIGH_SET, ACCEL_CONFIG_STATIC4_BIT::ACCEL_AAF_BITSHIFT_CLEAR | ACCEL_CONFIG_STATIC4_BIT::ACCEL_AAF_DELTSQR_HIGH_CLEAR },
};
uint32_t _temperature_samples{0};
// Support for the IMU server
uint32_t _imu_server_index{0};
uint32_t _imu_server_decimator{0};
imu_server_s _imu_server_data;
uORB::Publication<imu_server_s> _imu_server_pub{ORB_ID(imu_server)};
};
@@ -1,430 +0,0 @@
/****************************************************************************
*
* Copyright (c) 2020 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file InvenSense_ICM42688P_registers.hpp
*
* Invensense ICM-42688-P registers.
*
*/
#pragma once
#include <cstdint>
namespace InvenSense_ICM42688P
{
// TODO: move to a central header
static constexpr uint8_t Bit0 = (1 << 0);
static constexpr uint8_t Bit1 = (1 << 1);
static constexpr uint8_t Bit2 = (1 << 2);
static constexpr uint8_t Bit3 = (1 << 3);
static constexpr uint8_t Bit4 = (1 << 4);
static constexpr uint8_t Bit5 = (1 << 5);
static constexpr uint8_t Bit6 = (1 << 6);
static constexpr uint8_t Bit7 = (1 << 7);
static constexpr uint32_t SPI_SPEED = 24 * 1000 * 1000; // 24 MHz SPI
static constexpr uint8_t DIR_READ = 0x80;
static constexpr uint8_t WHOAMI = 0x47;
static constexpr float TEMPERATURE_SENSITIVITY = 132.48f; // LSB/C
static constexpr float TEMPERATURE_OFFSET = 25.f; // C
namespace Register
{
enum class BANK_0 : uint8_t {
DEVICE_CONFIG = 0x11,
INT_CONFIG = 0x14,
FIFO_CONFIG = 0x16,
TEMP_DATA1 = 0x1D,
TEMP_DATA0 = 0x1E,
INT_STATUS = 0x2D,
FIFO_COUNTH = 0x2E,
FIFO_COUNTL = 0x2F,
FIFO_DATA = 0x30,
SIGNAL_PATH_RESET = 0x4B,
INTF_CONFIG0 = 0x4C,
INTF_CONFIG1 = 0x4D,
PWR_MGMT0 = 0x4E,
GYRO_CONFIG0 = 0x4F,
ACCEL_CONFIG0 = 0x50,
GYRO_CONFIG1 = 0x51,
GYRO_ACCEL_CONFIG0 = 0x52,
ACCEL_CONFIG1 = 0x53,
FIFO_CONFIG1 = 0x5F,
FIFO_CONFIG2 = 0x60,
FIFO_CONFIG3 = 0x61,
INT_CONFIG0 = 0x63,
INT_SOURCE0 = 0x65,
SELF_TEST_CONFIG = 0x70,
WHO_AM_I = 0x75,
REG_BANK_SEL = 0x76,
};
enum class BANK_1 : uint8_t {
GYRO_CONFIG_STATIC2 = 0x0B,
GYRO_CONFIG_STATIC3 = 0x0C,
GYRO_CONFIG_STATIC4 = 0x0D,
GYRO_CONFIG_STATIC5 = 0x0E,
INTF_CONFIG5 = 0x7B,
};
enum class BANK_2 : uint8_t {
ACCEL_CONFIG_STATIC2 = 0x03,
ACCEL_CONFIG_STATIC3 = 0x04,
ACCEL_CONFIG_STATIC4 = 0x05,
};
};
//---------------- BANK0 Register bits
// DEVICE_CONFIG
enum DEVICE_CONFIG_BIT : uint8_t {
SOFT_RESET_CONFIG = Bit0, //
};
// INT_CONFIG
enum INT_CONFIG_BIT : uint8_t {
INT1_MODE = Bit2,
INT1_DRIVE_CIRCUIT = Bit1,
INT1_POLARITY = Bit0,
};
// FIFO_CONFIG
enum FIFO_CONFIG_BIT : uint8_t {
// 7:6 FIFO_MODE
FIFO_MODE_STOP_ON_FULL = Bit7 | Bit6, // 11: STOP-on-FULL Mode
};
// INT_STATUS
enum INT_STATUS_BIT : uint8_t {
RESET_DONE_INT = Bit4,
DATA_RDY_INT = Bit3,
FIFO_THS_INT = Bit2,
FIFO_FULL_INT = Bit1,
};
// SIGNAL_PATH_RESET
enum SIGNAL_PATH_RESET_BIT : uint8_t {
ABORT_AND_RESET = Bit3,
FIFO_FLUSH = Bit1,
};
// PWR_MGMT0
enum PWR_MGMT0_BIT : uint8_t {
GYRO_MODE_LOW_NOISE = Bit3 | Bit2, // 11: Places gyroscope in Low Noise (LN) Mode
ACCEL_MODE_LOW_NOISE = Bit1 | Bit0, // 11: Places accelerometer in Low Noise (LN) Mode
};
// GYRO_CONFIG0
enum GYRO_CONFIG0_BIT : uint8_t {
// 7:5 GYRO_FS_SEL
GYRO_FS_SEL_2000_DPS = 0, // 0b000 = ±2000dps (default)
GYRO_FS_SEL_1000_DPS = Bit5,
GYRO_FS_SEL_500_DPS = Bit6,
GYRO_FS_SEL_250_DPS = Bit6 | Bit5,
GYRO_FS_SEL_125_DPS = Bit7,
// 3:0 GYRO_ODR
// 0001: 32kHz
GYRO_ODR_32KHZ_SET = Bit0,
GYRO_ODR_32KHZ_CLEAR = Bit3 | Bit2 | Bit0,
// 0010: 16kHz
GYRO_ODR_16KHZ_SET = Bit1,
GYRO_ODR_16KHZ_CLEAR = Bit3 | Bit2 | Bit0,
// 0011: 8kHz
GYRO_ODR_8KHZ_SET = Bit1 | Bit0,
GYRO_ODR_8KHZ_CLEAR = Bit3 | Bit2,
// 0110: 1kHz (default)
GYRO_ODR_1KHZ_SET = Bit2 | Bit1,
GYRO_ODR_1KHZ_CLEAR = Bit3 | Bit0,
};
// ACCEL_CONFIG0
enum ACCEL_CONFIG0_BIT : uint8_t {
// 7:5 ACCEL_FS_SEL
ACCEL_FS_SEL_16G = 0, // 000: ±16g (default)
ACCEL_FS_SEL_8G = Bit5,
ACCEL_FS_SEL_4G = Bit6,
ACCEL_FS_SEL_2G = Bit6 | Bit5,
// 3:0 ACCEL_ODR
// 0001: 32kHz
ACCEL_ODR_32KHZ_SET = Bit0,
ACCEL_ODR_32KHZ_CLEAR = Bit3 | Bit2 | Bit0,
// 0010: 16kHz
ACCEL_ODR_16KHZ_SET = Bit1,
ACCEL_ODR_16KHZ_CLEAR = Bit3 | Bit2 | Bit0,
// 0011: 8kHz
ACCEL_ODR_8KHZ_SET = Bit1 | Bit0,
ACCEL_ODR_8KHZ_CLEAR = Bit3 | Bit2,
// 0110: 1kHz (default)
ACCEL_ODR_1KHZ_SET = Bit2 | Bit1,
ACCEL_ODR_1KHZ_CLEAR = Bit3 | Bit0,
};
// GYRO_CONFIG1
enum GYRO_CONFIG1_BIT : uint8_t {
GYRO_UI_FILT_ORD = Bit3 | Bit2, // 00: 1st Order
};
// GYRO_ACCEL_CONFIG0
enum GYRO_ACCEL_CONFIG0_BIT : uint8_t {
// 7:4 ACCEL_UI_FILT_BW
ACCEL_UI_FILT_BW = Bit7 | Bit6 | Bit5 | Bit4, // 0: BW=ODR/2
// 3:0 GYRO_UI_FILT_BW
GYRO_UI_FILT_BW = Bit3 | Bit2 | Bit1 | Bit0, // 0: BW=ODR/2
};
// ACCEL_CONFIG1
enum ACCEL_CONFIG1_BIT : uint8_t {
ACCEL_UI_FILT_ORD = Bit4 | Bit3, // 00: 1st Order
};
// FIFO_CONFIG1
enum FIFO_CONFIG1_BIT : uint8_t {
FIFO_RESUME_PARTIAL_RD = Bit6,
FIFO_WM_GT_TH = Bit5,
FIFO_HIRES_EN = Bit4,
FIFO_TEMP_EN = Bit2,
FIFO_GYRO_EN = Bit1,
FIFO_ACCEL_EN = Bit0,
};
// INT_CONFIG0
enum INT_CONFIG0_BIT : uint8_t {
// 3:2 FIFO_THS_INT_CLEAR
CLEAR_ON_FIFO_READ = Bit3,
};
// INT_SOURCE0
enum INT_SOURCE0_BIT : uint8_t {
UI_FSYNC_INT1_EN = Bit6,
PLL_RDY_INT1_EN = Bit5,
RESET_DONE_INT1_EN = Bit4,
UI_DRDY_INT1_EN = Bit3,
FIFO_THS_INT1_EN = Bit2, // FIFO threshold interrupt routed to INT1
FIFO_FULL_INT1_EN = Bit1,
UI_AGC_RDY_INT1_EN = Bit0,
};
// REG_BANK_SEL
enum REG_BANK_SEL_BIT : uint8_t {
USER_BANK_0 = 0, // 0: Select USER BANK 0.
USER_BANK_1 = Bit0, // 1: Select USER BANK 1.
USER_BANK_2 = Bit1, // 2: Select USER BANK 2.
USER_BANK_3 = Bit1 | Bit0, // 3: Select USER BANK 3.
};
//---------------- BANK1 Register bits
// GYRO_CONFIG_STATIC2
enum GYRO_CONFIG_STATIC2_BIT : uint8_t {
GYRO_AAF_DIS = Bit1,
GYRO_NF_DIS = Bit0,
};
// GYRO_CONFIG_STATIC3
enum GYRO_CONFIG_STATIC3_BIT : uint8_t {
// 585 Hz
GYRO_AAF_DELT_SET = Bit3 | Bit2 | Bit0, //13
GYRO_AAF_DELT_CLEAR = Bit5 | Bit4 | Bit1,
// 213 Hz
// GYRO_AAF_DELT_SET = Bit2 | Bit0, //5
// GYRO_AAF_DELT_CLEAR = Bit5 | Bit4 | Bit3 | Bit1,
// 126 Hz
//GYRO_AAF_DELT_SET = Bit1 | Bit0, //3
//GYRO_AAF_DELT_CLEAR = Bit5 | Bit4 | Bit3 | Bit2,
// 42 Hz
// GYRO_AAF_DELT_SET = Bit0, //1
// GYRO_AAF_DELT_CLEAR = Bit5 | Bit4 | Bit3 | Bit2 | Bit1,
};
// GYRO_CONFIG_STATIC4
enum GYRO_CONFIG_STATIC4_BIT : uint8_t {
// 585 Hz
GYRO_AAF_DELTSQR_LOW_SET = Bit7 | Bit5 | Bit3 | Bit1, //170
GYRO_AAF_DELTSQR_LOW_CLEAR = Bit6 | Bit4 | Bit2 | Bit0,
// 213 Hz
// GYRO_AAF_DELTSQR_LOW_SET = Bit4 | Bit3 | Bit0, //25
// GYRO_AAF_DELTSQR_LOW_CLEAR = Bit7 | Bit6 | Bit5 | Bit2 | Bit1,
// 126 Hz
//GYRO_AAF_DELTSQR_LOW_SET = Bit3 | Bit0, //9
//GYRO_AAF_DELTSQR_LOW_CLEAR = Bit7 | Bit6 | Bit5 | Bit4 | Bit2 | Bit1,
// 42 Hz
// GYRO_AAF_DELTSQR_LOW_SET = Bit0, //1
// GYRO_AAF_DELTSQR_LOW_CLEAR = Bit7 | Bit6 | Bit5 | Bit4 | Bit3 | Bit2 | Bit1,
};
// GYRO_CONFIG_STATIC5
enum GYRO_CONFIG_STATIC5_BIT : uint8_t {
// 585 Hz
GYRO_AAF_DELTSQR_HIGH_SET = 0,
GYRO_AAF_DELTSQR_HIGH_CLEAR = Bit3 | Bit2 | Bit1 | Bit0,
GYRO_AAF_BITSHIFT_SET = Bit7, // 8 << 4
GYRO_AAF_BITSHIFT_CLEAR = Bit6 | Bit5 | Bit4,
// 213 Hz
// GYRO_AAF_DELTSQR_HIGH_SET = 0,
// GYRO_AAF_DELTSQR_HIGH_CLEAR = Bit3 | Bit2 | Bit1 | Bit0,
// GYRO_AAF_BITSHIFT_SET = Bit7 | Bit5, //10
// GYRO_AAF_BITSHIFT_CLEAR = Bit6 | Bit4,
// 126 Hz
// GYRO_AAF_BITSHIFT_SET = Bit7 | Bit6, //12
// GYRO_AAF_BITSHIFT_CLEAR = Bit5 | Bit4,
// 42 Hz
// GYRO_AAF_BITSHIFT_SET = Bit7 | Bit6 | Bit5 | Bit4, //15
// GYRO_AAF_BITSHIFT_CLEAR = 0,
};
//---------------- BANK2 Register bits
// ACCEL_CONFIG_STATIC2
enum ACCEL_CONFIG_STATIC2_BIT : uint8_t {
ACCEL_AAF_DIS = Bit0,
ACCEL_AAF_DELT = Bit3 | Bit1,
// 213 Hz
ACCEL_AAF_DELT_SET = Bit3 | Bit1, //5
ACCEL_AAF_DELT_CLEAR = Bit6 | Bit5 | Bit4 | Bit2,
// 42 Hz
// ACCEL_AAF_DELT_SET = Bit1, //1
// ACCEL_AAF_DELT_CLEAR = Bit6 | Bit5 | Bit4 | Bit3 | Bit2,
};
// ACCEL_CONFIG_STATIC3
enum ACCEL_CONFIG_STATIC3_BIT : uint8_t {
ACCEL_AAF_DELTSQR_LOW = Bit4 | Bit3 | Bit0,
// 213 Hz
ACCEL_AAF_DELTSQR_LOW_SET = Bit4 | Bit3 | Bit0, //25
ACCEL_AAF_DELTSQR_LOW_CLEAR = Bit7 | Bit6 | Bit5 | Bit2 | Bit1,
// 42 Hz
// ACCEL_AAF_DELTSQR_LOW_SET = Bit0, //1
// ACCEL_AAF_DELTSQR_LOW_CLEAR = Bit7 | Bit6 | Bit5 | Bit4 | Bit3 | Bit2 | Bit1,
};
// ACCEL_CONFIG_STATIC4
enum ACCEL_CONFIG_STATIC4_BIT : uint8_t {
ACCEL_AAF_BITSHIFT = Bit7 | Bit5,
ACCEL_AAF_DELTSQR_HIGH = 0,
// 213 Hz
ACCEL_AAF_BITSHIFT_SET = Bit7 | Bit5, //10
ACCEL_AAF_BITSHIFT_CLEAR = Bit6 | Bit4,
// 42 Hz
// ACCEL_AAF_BITSHIFT_SET = Bit7 | Bit6 | Bit5 | Bit4, //15
// ACCEL_AAF_BITSHIFT_CLEAR = 0,
ACCEL_AAF_DELTSQR_HIGH_SET = 0,
ACCEL_AAF_DELTSQR_HIGH_CLEAR = Bit3 | Bit2 | Bit1 | Bit0,
};
namespace FIFO
{
static constexpr size_t SIZE = 2048;
// FIFO_DATA layout when FIFO_CONFIG1 has FIFO_GYRO_EN and FIFO_ACCEL_EN set
// Packet 4
struct DATA {
uint8_t FIFO_Header;
uint8_t ACCEL_DATA_X1; // Accel X [19:12]
uint8_t ACCEL_DATA_X0; // Accel X [11:4]
uint8_t ACCEL_DATA_Y1; // Accel Y [19:12]
uint8_t ACCEL_DATA_Y0; // Accel Y [11:4]
uint8_t ACCEL_DATA_Z1; // Accel Z [19:12]
uint8_t ACCEL_DATA_Z0; // Accel Z [11:4]
uint8_t GYRO_DATA_X1; // Gyro X [19:12]
uint8_t GYRO_DATA_X0; // Gyro X [11:4]
uint8_t GYRO_DATA_Y1; // Gyro Y [19:12]
uint8_t GYRO_DATA_Y0; // Gyro Y [11:4]
uint8_t GYRO_DATA_Z1; // Gyro Z [19:12]
uint8_t GYRO_DATA_Z0; // Gyro Z [11:4]
uint8_t TEMP_DATA1; // Temperature[15:8]
uint8_t TEMP_DATA0; // Temperature[7:0]
uint8_t TimeStamp_h; // TimeStamp[15:8]
uint8_t TimeStamp_l; // TimeStamp[7:0]
uint8_t Ext_Accel_X_Gyro_X; // Accel X [3:0] Gyro X [3:0]
uint8_t Ext_Accel_Y_Gyro_Y; // Accel Y [3:0] Gyro Y [3:0]
uint8_t Ext_Accel_Z_Gyro_Z; // Accel Z [3:0] Gyro Z [3:0]
};
// With FIFO_ACCEL_EN and FIFO_GYRO_EN header should be 8b_0110_10xx
enum FIFO_HEADER_BIT : uint8_t {
HEADER_MSG = Bit7, // 1: FIFO is empty
HEADER_ACCEL = Bit6, // 1: Packet is sized so that accel data have location in the packet, FIFO_ACCEL_EN must be 1
HEADER_GYRO = Bit5, // 1: Packet is sized so that gyro data have location in the packet, FIFO_GYRO_EN must be1
HEADER_20 = Bit4, // 1: Packet has a new and valid sample of extended 20-bit data for gyro and/or accel
HEADER_TIMESTAMP_FSYNC = Bit3 | Bit2,
HEADER_ODR_ACCEL = Bit1, // 1: The ODR for accel is different for this accel data packet compared to the previous accel packet
HEADER_ODR_GYRO = Bit0, // 1: The ODR for gyro is different for this gyro data packet compared to the previous gyro packet
};
}
} // namespace InvenSense_ICM42688P
@@ -1,116 +0,0 @@
/****************************************************************************
*
* Copyright (c) 2020 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include "ICM42688P.hpp"
#include <px4_platform_common/getopt.h>
#include <px4_platform_common/module.h>
#include <string>
void ICM42688P::print_usage()
{
PRINT_MODULE_USAGE_NAME("icm42688p", "driver");
PRINT_MODULE_USAGE_SUBCATEGORY("imu");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_PARAMS_I2C_SPI_DRIVER(false, true);
PRINT_MODULE_USAGE_PARAM_INT('R', 0, 0, 35, "Rotation", true);
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
}
// I2CSPIDriverBase *ICM42688P::instantiate(const BusCLIArguments &cli, const BusInstanceIterator &iterator,
// int runtime_instance)
// {
// ICM42688P *instance = new ICM42688P(iterator.configuredBusOption(), iterator.bus(), iterator.devid(), cli.rotation,
// cli.bus_frequency, cli.spi_mode, iterator.DRDYGPIO());
//
// if (!instance) {
// PX4_ERR("alloc failed");
// return nullptr;
// }
//
// if (OK != instance->init()) {
// delete instance;
// return nullptr;
// }
//
// return instance;
// }
extern "C" int icm42688p_main(int argc, char *argv[])
{
for (int i = 0; i <= argc - 1; i++) {
if (std::string(argv[i]) == "-h") {
argv[i] = 0;
hitl_mode = true;
break;
}
}
int ch;
using ThisDriver = ICM42688P;
BusCLIArguments cli{false, true};
cli.default_spi_frequency = SPI_SPEED;
while ((ch = cli.getOpt(argc, argv, "R:")) != EOF) {
switch (ch) {
case 'R':
cli.rotation = (enum Rotation)atoi(cli.optArg());
break;
}
}
const char *verb = cli.optArg();
if (!verb) {
ThisDriver::print_usage();
return -1;
}
BusInstanceIterator iterator(MODULE_NAME, cli, DRV_IMU_DEVTYPE_ICM42688P);
if (!strcmp(verb, "start")) {
return ThisDriver::module_start(cli, iterator);
}
if (!strcmp(verb, "stop")) {
return ThisDriver::module_stop(iterator);
}
if (!strcmp(verb, "status")) {
return ThisDriver::module_status(iterator);
}
ThisDriver::print_usage();
return -1;
}
+1 -1
View File
@@ -18,4 +18,4 @@ CONFIG_MODULES_UUV_POS_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -53,7 +53,7 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
+1 -1
View File
@@ -16,7 +16,7 @@ param set-default SENS_EN_INA238 0
param set-default SENS_EN_INA228 0
param set-default SENS_EN_INA226 1
if ver hwbasecmp 008 009 00a 010
if ver hwbasecmp 008 009 00a 010 011
then
# Skynode: use the "custom participant" config for uxrce_dds_client
param set-default UXRCE_DDS_PTCFG 2
+1 -1
View File
@@ -3,7 +3,7 @@
# board specific MAVLink startup script.
#------------------------------------------------------------------------------
if ver hwbasecmp 008 009 00a 010
if ver hwbasecmp 008 009 00a 010 011
then
# Start MAVLink on the UART connected to the mission computer
mavlink start -d /dev/ttyS4 -b 3000000 -r 290000 -m onboard_low_bandwidth -x -z
+1 -1
View File
@@ -49,7 +49,7 @@ then
fi
fi
if ver hwbasecmp 008 009 00a 010
if ver hwbasecmp 008 009 00a 010 011
then
#SKYNODE base fmu board orientation
+1 -1
View File
@@ -13,4 +13,4 @@ CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -13,4 +13,4 @@ CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -18,7 +18,7 @@ param set-default SENS_EN_INA238 0
param set-default SENS_EN_INA228 0
param set-default SENS_EN_INA226 0
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
# Skynode: use the "custom participant" config for uxrce_dds_client
param set-default UXRCE_DDS_PTCFG 2
+1 -1
View File
@@ -4,7 +4,7 @@
#------------------------------------------------------------------------------
# if skynode base board is detected start Mavlink on Telem2
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
mavlink start -d /dev/ttyS4 -b 3000000 -r 290000 -m onboard_low_bandwidth -x -z
+4 -4
View File
@@ -56,7 +56,7 @@ then
fi
#Start Auterion Power Module selector for Skynode boards
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
pm_selector_auterion start
else
@@ -93,7 +93,7 @@ else
icm20649 -s -R 6 start
else
# Internal SPI BMI088
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
bmi088 -A -R 6 -s start
bmi088 -G -R 6 -s start
@@ -110,7 +110,7 @@ else
fi
# Internal SPI bus ICM42688p
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
icm42688p -R 12 -s start
else
@@ -127,7 +127,7 @@ else
# Internal SPI bus ICM-42670-P (hard-mounted)
icm42670p -R 10 -s start
else
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
icm20602 -R 6 -s start
else
+1 -1
View File
@@ -13,4 +13,4 @@ CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+23 -4
View File
@@ -6,21 +6,30 @@ CONFIG_BOARD_SERIAL_GPS2="/dev/ttyS3"
CONFIG_BOARD_SERIAL_TEL1="/dev/ttyS2"
CONFIG_BOARD_SERIAL_TEL2="/dev/ttyS5"
CONFIG_BOARD_SERIAL_TEL3="/dev/ttyS6"
CONFIG_DRIVERS_ADC_ADS1115=y
CONFIG_DRIVERS_ADC_BOARD_ADC=y
CONFIG_DRIVERS_BAROMETER_BMP388=y
CONFIG_DRIVERS_BAROMETER_INVENSENSE_ICP201XX=y
CONFIG_DRIVERS_BAROMETER_MS5611=y
CONFIG_DRIVERS_CAMERA_CAPTURE=y
CONFIG_DRIVERS_CAMERA_TRIGGER=y
CONFIG_DRIVERS_DISTANCE_SENSOR_LIGHTWARE_LASER_I2C=y
CONFIG_COMMON_DIFFERENTIAL_PRESSURE=y
CONFIG_COMMON_DISTANCE_SENSOR=y
CONFIG_DRIVERS_DSHOT=y
CONFIG_DRIVERS_GPS=y
CONFIG_DRIVERS_IMU_ANALOG_DEVICES_ADIS16470=y
CONFIG_DRIVERS_IMU_BOSCH_BMI088=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM20602=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM20649=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM20948=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM42670P=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM42688P=y
CONFIG_DRIVERS_IMU_INVENSENSE_ICM45686=y
CONFIG_DRIVERS_IMU_INVENSENSE_IIM42652=y
CONFIG_COMMON_INS=y
CONFIG_COMMON_LIGHT=y
CONFIG_DRIVERS_MAGNETOMETER_BOSCH_BMM150=y
CONFIG_DRIVERS_MAGNETOMETER_HMC5883=y
CONFIG_DRIVERS_MAGNETOMETER_ISENTEK_IST8310=y
CONFIG_COMMON_MAGNETOMETER=y
CONFIG_DRIVERS_OSD_MSP_OSD=y
CONFIG_DRIVERS_POWER_MONITOR_INA226=y
CONFIG_DRIVERS_POWER_MONITOR_INA228=y
CONFIG_DRIVERS_POWER_MONITOR_INA238=y
@@ -32,14 +41,20 @@ CONFIG_COMMON_TELEMETRY=y
CONFIG_DRIVERS_TONE_ALARM=y
CONFIG_DRIVERS_UAVCAN=y
CONFIG_COMMON_UWB=y
CONFIG_MODULES_AIRSPEED_SELECTOR=y
CONFIG_MODULES_BATTERY_STATUS=y
CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_EKF2=y
CONFIG_MODULES_ESC_BATTERY=y
CONFIG_MODULES_EVENTS=y
CONFIG_MODULES_FLIGHT_MODE_MANAGER=y
CONFIG_MODULES_FW_ATT_CONTROL=y
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=y
CONFIG_MODULES_FW_POS_CONTROL=y
CONFIG_MODULES_FW_RATE_CONTROL=y
CONFIG_MODULES_GIMBAL=y
CONFIG_MODULES_GYRO_CALIBRATION=y
CONFIG_MODULES_GYRO_FFT=y
@@ -57,11 +72,15 @@ CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=y
CONFIG_MODULES_MC_POS_CONTROL=y
CONFIG_MODULES_MC_RATE_CONTROL=y
CONFIG_MODULES_NAVIGATOR=y
CONFIG_MODE_NAVIGATOR_VTOL_TAKEOFF=y
CONFIG_MODULES_RC_UPDATE=y
CONFIG_MODULES_ROVER_POS_CONTROL=y
CONFIG_MODULES_SENSORS=y
CONFIG_MODULES_TEMPERATURE_COMPENSATION=y
CONFIG_MODULES_UXRCE_DDS_CLIENT=y
CONFIG_MODULES_VTOL_ATT_CONTROL=y
CONFIG_SYSTEMCMDS_ACTUATOR_TEST=y
CONFIG_SYSTEMCMDS_BSONDUMP=y
CONFIG_SYSTEMCMDS_DMESG=y
CONFIG_SYSTEMCMDS_DUMPFILE=y
CONFIG_SYSTEMCMDS_HARDFAULT_LOG=y
+1 -1
View File
@@ -4,7 +4,7 @@
#------------------------------------------------------------------------------
# if skynode base board is detected start Mavlink on Telem2
if ver hwbasecmp 009 010
if ver hwbasecmp 009 010 011
then
mavlink start -d /dev/ttyS5 -b 3000000 -r 290000 -m onboard_low_bandwidth -x -z
@@ -257,7 +257,7 @@ CONFIG_SCHED_INSTRUMENTATION_EXTERNAL=y
CONFIG_SCHED_INSTRUMENTATION_SWITCH=y
CONFIG_SCHED_LPWORK=y
CONFIG_SCHED_LPWORKPRIORITY=50
CONFIG_SCHED_LPWORKSTACKSIZE=1632
CONFIG_SCHED_LPWORKSTACKSIZE=2032
CONFIG_SCHED_WAITPID=y
CONFIG_SDIO_BLOCKSETUP=y
CONFIG_SEM_PREALLOCHOLDERS=32
+7 -1
View File
@@ -1,4 +1,9 @@
CONFIG_MODULES_AIRSPEED_SELECTOR=n
CONFIG_MODULES_FLIGHT_MODE_MANAGER=n
CONFIG_MODULES_FW_ATT_CONTROL=n
CONFIG_MODULES_FW_AUTOTUNE_ATTITUDE_CONTROL=n
CONFIG_MODULES_FW_POS_CONTROL=n
CONFIG_MODULES_FW_RATE_CONTROL=n
CONFIG_MODULES_LANDING_TARGET_ESTIMATOR=n
CONFIG_MODULES_LOCAL_POSITION_ESTIMATOR=n
CONFIG_MODULES_MC_ATT_CONTROL=n
@@ -6,6 +11,7 @@ CONFIG_MODULES_MC_AUTOTUNE_ATTITUDE_CONTROL=n
CONFIG_MODULES_MC_HOVER_THRUST_ESTIMATOR=n
CONFIG_MODULES_MC_POS_CONTROL=n
CONFIG_MODULES_MC_RATE_CONTROL=n
CONFIG_MODULES_VTOL_ATT_CONTROL=n
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
# CONFIG_EKF2_WIND is not set
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
+1 -1
View File
@@ -12,7 +12,7 @@ CONFIG_MODULES_CAMERA_FEEDBACK=y
CONFIG_MODULES_COMMANDER=y
CONFIG_MODULES_CONTROL_ALLOCATOR=y
CONFIG_MODULES_DATAMAN=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE_CONTROL=y
CONFIG_MODULES_DIFFERENTIAL_DRIVE=y
CONFIG_MODULES_EKF2=y
CONFIG_EKF2_VERBOSE_STATUS=y
CONFIG_EKF2_AUX_GLOBAL_POSITION=y
+1
View File
@@ -173,6 +173,7 @@ set(msg_files
RegisterExtComponentReply.msg
RegisterExtComponentRequest.msg
Rpm.msg
RtlStatus.msg
RtlTimeEstimate.msg
SatelliteInfo.msg
SensorAccel.msg
+4
View File
@@ -1,4 +1,8 @@
uint64 timestamp # time since system start (microseconds)
float32 speed # [m/s] collective roll-off speed in body x-axis
bool closed_loop_speed_control # true if speed is controlled using estimator feedback, false if direct feed-forward
float32 yaw_rate # [rad/s] yaw rate
bool closed_loop_yaw_rate_control # true if yaw rate is controlled using gyroscope feedback, false if direct feed-forward
# TOPICS differential_drive_setpoint differential_drive_control_output
+3 -9
View File
@@ -55,15 +55,9 @@ bool fs_bad_airspeed # 5 - true if fusion of the airspeed has encounte
bool fs_bad_sideslip # 6 - true if fusion of the synthetic sideslip constraint has encountered a numerical error
bool fs_bad_optflow_x # 7 - true if fusion of the optical flow X axis has encountered a numerical error
bool fs_bad_optflow_y # 8 - true if fusion of the optical flow Y axis has encountered a numerical error
bool fs_bad_vel_n # 9 - true if fusion of the North velocity has encountered a numerical error
bool fs_bad_vel_e # 10 - true if fusion of the East velocity has encountered a numerical error
bool fs_bad_vel_d # 11 - true if fusion of the Down velocity has encountered a numerical error
bool fs_bad_pos_n # 12 - true if fusion of the North position has encountered a numerical error
bool fs_bad_pos_e # 13 - true if fusion of the East position has encountered a numerical error
bool fs_bad_pos_d # 14 - true if fusion of the Down position has encountered a numerical error
bool fs_bad_acc_bias # 15 - true if bad delta velocity bias estimates have been detected
bool fs_bad_acc_vertical # 16 - true if bad vertical accelerometer data has been detected
bool fs_bad_acc_clipping # 17 - true if delta velocity data contains clipping (asymmetric railing)
bool fs_bad_acc_bias # 9 - true if bad delta velocity bias estimates have been detected
bool fs_bad_acc_vertical # 10 - true if bad vertical accelerometer data has been detected
bool fs_bad_acc_clipping # 11 - true if delta velocity data contains clipping (asymmetric railing)
# innovation test failures
+2
View File
@@ -4,4 +4,6 @@ int32 val
uint8[64] junk
uint8 ORB_QUEUE_LENGTH = 16
# TOPICS orb_test_medium orb_test_medium_multi orb_test_medium_wrap_around orb_test_medium_queue orb_test_medium_queue_poll
+15
View File
@@ -0,0 +1,15 @@
uint64 timestamp # time since system start (microseconds)
uint32 safe_points_id # unique ID of active set of safe_point_items
bool is_evaluation_pending # flag if the RTL point needs reevaluation (e.g. new safe points available, but need loading).
bool has_vtol_approach # flag if approaches are defined for current RTL_TYPE parameter setting
uint8 rtl_type # Type of RTL chosen
uint8 safe_point_index # index of the chosen safe point, if in RTL_STATUS_TYPE_DIRECT_SAFE_POINT mode
uint8 RTL_STATUS_TYPE_NONE=0 # RTL type is pending if evaluation can't pe performed currently e.g. when it is still loading the safe points
uint8 RTL_STATUS_TYPE_DIRECT_SAFE_POINT=1 # RTL type is chosen to directly go to a safe point or home position
uint8 RTL_STATUS_TYPE_DIRECT_MISSION_LAND=2 # RTL type is going straight to the beginning of the mission landing
uint8 RTL_STATUS_TYPE_FOLLOW_MISSION=3 # RTL type is following the mission from closest point to mission landing
uint8 RTL_STATUS_TYPE_FOLLOW_MISSION_REVERSE=4 # RTL type is following the mission in reverse to the start position
+49 -7
View File
@@ -48,6 +48,8 @@
#include <board_config.h>
#if defined(BOARD_HAS_HW_SPLIT_VERSIONING)
#include <inttypes.h>
#include <stdbool.h>
#include <syslog.h>
@@ -57,7 +59,6 @@
/****************************************************************************
* Pre-Processor Definitions
****************************************************************************/
#if defined(BOARD_HAS_HW_SPLIT_VERSIONING)
typedef struct {
hw_base_id_t hw_base_id; /* The ID of the Base */
@@ -292,12 +293,6 @@ static const px4_hw_mft_item_t base_configuration_9[] = {
.mandatory = 1,
.connection = px4_hw_con_onboard,
},
{
.id = PX4_MFT_PM2,
.present = 1,
.mandatory = 1,
.connection = px4_hw_con_onboard,
},
{
.id = PX4_MFT_ETHERNET,
.present = 1,
@@ -315,6 +310,52 @@ static const px4_hw_mft_item_t base_configuration_9[] = {
// BASE ID 10 Skynode QS no USB Alaised to ID 9
// BASE ID 16 Auterion Skynode RC10, RC11, RC12, RC13 Alaised to ID 0
// BASE ID 17 Auterion Skynode RC13 with many parts removed
static const px4_hw_mft_item_t base_configuration_17[] = {
{
.id = PX4_MFT_PX4IO,
.present = 0,
.mandatory = 0,
.connection = px4_hw_con_onboard,
},
{
.id = PX4_MFT_USB,
.present = 1,
.mandatory = 1,
.connection = px4_hw_con_unknown,
},
{
.id = PX4_MFT_CAN2,
.present = 0,
.mandatory = 0,
.connection = px4_hw_con_onboard,
},
{
.id = PX4_MFT_CAN3,
.present = 0,
.mandatory = 0,
.connection = px4_hw_con_unknown,
},
{
.id = PX4_MFT_PM2,
.present = 0,
.mandatory = 0,
.connection = px4_hw_con_onboard,
},
{
.id = PX4_MFT_ETHERNET,
.present = 1,
.mandatory = 1,
.connection = px4_hw_con_connector,
},
{
.id = PX4_MFT_T100_ETH,
.present = 1,
.mandatory = 1,
.connection = px4_hw_con_onboard,
},
};
static px4_hw_mft_list_entry_t mft_lists[] = {
// ver_rev
@@ -328,6 +369,7 @@ static px4_hw_mft_list_entry_t mft_lists[] = {
{HW_BASE_ID(9), base_configuration_9, arraySize(base_configuration_9)}, // Auterion Skynode ver 9
{HW_BASE_ID(10), base_configuration_9, arraySize(base_configuration_9)}, // Auterion Skynode ver 10
{HW_BASE_ID(16), base_configuration_0, arraySize(base_configuration_0)}, // Auterion Skynode ver 16
{HW_BASE_ID(17), base_configuration_17, arraySize(base_configuration_17)}, // Auterion Skynode ver 17
};
/************************************************************************************
+1 -1
View File
@@ -74,7 +74,7 @@ void px4_log_initialize(void)
log_message.severity = 6; // info
strcpy((char *)log_message.text, "initialized uORB logging");
log_message.timestamp = hrt_absolute_time();
orb_log_message_pub = orb_advertise_queue(ORB_ID(log_message), &log_message, log_message_s::ORB_QUEUE_LENGTH);
orb_log_message_pub = orb_advertise(ORB_ID(log_message), &log_message);
}
__EXPORT void px4_log_modulename(int level, const char *module_name, const char *fmt, ...)
+2 -20
View File
@@ -48,24 +48,6 @@
namespace uORB
{
template <typename U> class DefaultQueueSize
{
private:
template <typename T>
static constexpr uint8_t get_queue_size(decltype(T::ORB_QUEUE_LENGTH) *)
{
return T::ORB_QUEUE_LENGTH;
}
template <typename T> static constexpr uint8_t get_queue_size(...)
{
return 1;
}
public:
static constexpr unsigned value = get_queue_size<U>(nullptr);
};
class PublicationBase
{
public:
@@ -97,7 +79,7 @@ protected:
/**
* uORB publication wrapper class
*/
template<typename T, uint8_t ORB_QSIZE = DefaultQueueSize<T>::value>
template<typename T>
class Publication : public PublicationBase
{
public:
@@ -113,7 +95,7 @@ public:
bool advertise()
{
if (!advertised()) {
_handle = orb_advertise_queue(get_topic(), nullptr, ORB_QSIZE);
_handle = orb_advertise(get_topic(), nullptr);
}
return advertised();
+2 -2
View File
@@ -51,7 +51,7 @@ namespace uORB
/**
* Base publication multi wrapper class
*/
template<typename T, uint8_t QSIZE = DefaultQueueSize<T>::value>
template<typename T>
class PublicationMulti : public PublicationBase
{
public:
@@ -73,7 +73,7 @@ public:
{
if (!advertised()) {
int instance = 0;
_handle = orb_advertise_multi_queue(get_topic(), nullptr, &instance, QSIZE);
_handle = orb_advertise_multi(get_topic(), nullptr, &instance);
}
return advertised();
+8 -11
View File
@@ -118,22 +118,11 @@ orb_advert_t orb_advertise(const struct orb_metadata *meta, const void *data)
return uORB::Manager::get_instance()->orb_advertise(meta, data);
}
orb_advert_t orb_advertise_queue(const struct orb_metadata *meta, const void *data, unsigned int queue_size)
{
return uORB::Manager::get_instance()->orb_advertise(meta, data, queue_size);
}
orb_advert_t orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance)
{
return uORB::Manager::get_instance()->orb_advertise_multi(meta, data, instance);
}
orb_advert_t orb_advertise_multi_queue(const struct orb_metadata *meta, const void *data, int *instance,
unsigned int queue_size)
{
return uORB::Manager::get_instance()->orb_advertise_multi(meta, data, instance, queue_size);
}
int orb_unadvertise(orb_advert_t handle)
{
return uORB::Manager::get_instance()->orb_unadvertise(handle);
@@ -227,6 +216,14 @@ const char *orb_get_c_type(unsigned char short_type)
return nullptr;
}
uint8_t orb_get_queue_depth(const struct orb_metadata *meta)
{
if (meta) {
return meta->o_queue;
}
return 0;
}
void orb_print_message_internal(const orb_metadata *meta, const void *data, bool print_topic_name)
{
+18 -20
View File
@@ -53,6 +53,8 @@ struct orb_metadata {
const uint16_t o_size_no_padding; /**< object size w/o padding at the end (for logger) */
uint32_t message_hash; /**< Hash over all fields for message compatibility checks */
orb_id_size_t o_id; /**< ORB_ID enum */
uint8_t o_queue; /**< queue size */
};
typedef const struct orb_metadata *orb_id_t;
@@ -102,14 +104,16 @@ typedef const struct orb_metadata *orb_id_t;
* @param _size_no_padding Struct size w/o padding at the end
* @param _message_hash 32 bit message hash over all fields
* @param _orb_id_enum ORB ID enum e.g.: ORB_ID::vehicle_status
* @param _queue_size Queue size from topic definition
*/
#define ORB_DEFINE(_name, _struct, _size_no_padding, _message_hash, _orb_id_enum) \
const struct orb_metadata __orb_##_name = { \
#_name, \
sizeof(_struct), \
_size_no_padding, \
_message_hash, \
_orb_id_enum \
#define ORB_DEFINE(_name, _struct, _size_no_padding, _message_hash, _orb_id_enum, _queue_size) \
const struct orb_metadata __orb_##_name = { \
#_name, \
sizeof(_struct), \
_size_no_padding, \
_message_hash, \
_orb_id_enum, \
_queue_size \
}; struct hack
__BEGIN_DECLS
@@ -135,23 +139,11 @@ typedef void *orb_advert_t;
*/
extern orb_advert_t orb_advertise(const struct orb_metadata *meta, const void *data) __EXPORT;
/**
* @see uORB::Manager::orb_advertise()
*/
extern orb_advert_t orb_advertise_queue(const struct orb_metadata *meta, const void *data,
unsigned int queue_size) __EXPORT;
/**
* @see uORB::Manager::orb_advertise_multi()
*/
extern orb_advert_t orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance) __EXPORT;
/**
* @see uORB::Manager::orb_advertise_multi()
*/
extern orb_advert_t orb_advertise_multi_queue(const struct orb_metadata *meta, const void *data, int *instance,
unsigned int queue_size) __EXPORT;
/**
* @see uORB::Manager::orb_unadvertise()
*/
@@ -160,7 +152,7 @@ extern int orb_unadvertise(orb_advert_t handle) __EXPORT;
/**
* @see uORB::Manager::orb_publish()
*/
extern int orb_publish(const struct orb_metadata *meta, orb_advert_t handle, const void *data) __EXPORT;
extern int orb_publish(const struct orb_metadata *meta, orb_advert_t handle, const void *data) __EXPORT;
/**
* Advertise as the publisher of a topic.
@@ -241,6 +233,12 @@ extern int orb_get_interval(int handle, unsigned *interval) __EXPORT;
*/
const char *orb_get_c_type(unsigned char short_type);
/**
* Returns the queue depth of a topic
* @param meta orb topic metadata
*/
extern uint8_t orb_get_queue_depth(const struct orb_metadata *meta);
/**
* Print a topic to console. Do not call this directly, use print_message() instead.
* @param meta orb topic metadata
+5 -30
View File
@@ -73,12 +73,10 @@ static inline uint8_t round_pow_of_two_8(uint8_t n)
return value + 1;
}
uORB::DeviceNode::DeviceNode(const struct orb_metadata *meta, const uint8_t instance, const char *path,
uint8_t queue_size) :
uORB::DeviceNode::DeviceNode(const struct orb_metadata *meta, const uint8_t instance, const char *path) :
CDev(strdup(path)), // success is checked in CDev::init
_meta(meta),
_instance(instance),
_queue_size(round_pow_of_two_8(queue_size))
_instance(instance)
{
}
@@ -186,7 +184,7 @@ uORB::DeviceNode::write(cdev::file_t *filp, const char *buffer, size_t buflen)
/* re-check size */
if (nullptr == _data) {
const size_t data_size = _meta->o_size * _queue_size;
const size_t data_size = _meta->o_size * _meta->o_queue;
_data = (uint8_t *) px4_cache_aligned_alloc(data_size);
if (_data) {
@@ -217,7 +215,7 @@ uORB::DeviceNode::write(cdev::file_t *filp, const char *buffer, size_t buflen)
/* wrap-around happens after ~49 days, assuming a publisher rate of 1 kHz */
unsigned generation = _generation.fetch_add(1);
memcpy(_data + (_meta->o_size * (generation % _queue_size)), buffer, _meta->o_size);
memcpy(_data + (_meta->o_size * (generation % _meta->o_queue)), buffer, _meta->o_size);
// callbacks
for (auto item : _callbacks) {
@@ -254,13 +252,6 @@ uORB::DeviceNode::ioctl(cdev::file_t *filp, int cmd, unsigned long arg)
*(uintptr_t *)arg = (uintptr_t)this;
return PX4_OK;
case ORBIOCSETQUEUESIZE: {
lock();
int ret = update_queue_size(arg);
unlock();
return ret;
}
case ORBIOCGETINTERVAL:
*(unsigned *)arg = filp_to_subscription(filp)->get_interval_us();
return PX4_OK;
@@ -389,12 +380,11 @@ uORB::DeviceNode::print_statistics(int max_topic_length)
const uint8_t instance = get_instance();
const int8_t sub_count = subscriber_count();
const uint8_t queue_size = get_queue_size();
unlock();
PX4_INFO_RAW("%-*s %2i %4i %2i %4i %s\n", max_topic_length, get_meta()->o_name, (int)instance, (int)sub_count,
queue_size, get_meta()->o_size, get_devname());
get_meta()->o_queue, get_meta()->o_size, get_devname());
return true;
}
@@ -483,21 +473,6 @@ int16_t uORB::DeviceNode::process_received_message(int32_t length, uint8_t *data
}
#endif /* CONFIG_ORB_COMMUNICATOR */
int uORB::DeviceNode::update_queue_size(unsigned int queue_size)
{
if (_queue_size == queue_size) {
return PX4_OK;
}
//queue size is limited to 255 for the single reason that we use uint8 to store it
if (_data || _queue_size > queue_size || queue_size > 255) {
return PX4_ERROR;
}
_queue_size = round_pow_of_two_8(queue_size);
return PX4_OK;
}
unsigned uORB::DeviceNode::get_initial_generation()
{
ATOMIC_ENTER;
+7 -16
View File
@@ -62,7 +62,7 @@ class UnitTest;
class uORB::DeviceNode : public cdev::CDev, public IntrusiveSortedListNode<uORB::DeviceNode *>
{
public:
DeviceNode(const struct orb_metadata *meta, const uint8_t instance, const char *path, uint8_t queue_size = 1);
DeviceNode(const struct orb_metadata *meta, const uint8_t instance, const char *path);
virtual ~DeviceNode();
// no copy, assignment, move, move assignment
@@ -179,15 +179,6 @@ public:
void mark_as_advertised() { _advertised = true; }
/**
* Try to change the size of the queue. This can only be done as long as nobody published yet.
* This is the case, for example when orb_subscribe was called before an orb_advertise.
* The queue size can only be increased.
* @param queue_size new size of the queue
* @return PX4_OK if queue size successfully set
*/
int update_queue_size(unsigned int queue_size);
/**
* Print statistics
* @param max_topic_length max topic name length for printing
@@ -195,7 +186,7 @@ public:
*/
bool print_statistics(int max_topic_length);
uint8_t get_queue_size() const { return _queue_size; }
uint8_t get_queue_size() const { return _meta->o_queue; }
int8_t subscriber_count() const { return _subscriber_count; }
@@ -234,7 +225,7 @@ public:
bool copy(void *dst, unsigned &generation)
{
if ((dst != nullptr) && (_data != nullptr)) {
if (_queue_size == 1) {
if (_meta->o_queue == 1) {
ATOMIC_ENTER;
memcpy(dst, _data, _meta->o_size);
generation = _generation.load();
@@ -253,12 +244,12 @@ public:
}
// Compatible with normal and overflow conditions
if (!is_in_range(current_generation - _queue_size, generation, current_generation - 1)) {
if (!is_in_range(current_generation - _meta->o_queue, generation, current_generation - 1)) {
// Reader is too far behind: some messages are lost
generation = current_generation - _queue_size;
generation = current_generation - _meta->o_queue;
}
memcpy(dst, _data + (_meta->o_size * (generation % _queue_size)), _meta->o_size);
memcpy(dst, _data + (_meta->o_size * (generation % _meta->o_queue)), _meta->o_size);
ATOMIC_LEAVE;
++generation;
@@ -295,7 +286,7 @@ private:
const uint8_t _instance; /**< orb multi instance identifier */
bool _advertised{false}; /**< has ever been advertised (not necessarily published data yet) */
uint8_t _queue_size; /**< maximum number of elements in the queue */
int8_t _subscriber_count{0};
+27 -36
View File
@@ -265,8 +265,7 @@ int uORB::Manager::orb_exists(const struct orb_metadata *meta, int instance)
return ret;
}
orb_advert_t uORB::Manager::orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance,
unsigned int queue_size)
orb_advert_t uORB::Manager::orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance)
{
#ifdef ORB_USE_PUBLISHER_RULES
@@ -300,19 +299,10 @@ orb_advert_t uORB::Manager::orb_advertise_multi(const struct orb_metadata *meta,
return nullptr;
}
/* Set the queue size. This must be done before the first publication; thus it fails if
* this is not the first advertiser.
*/
int result = px4_ioctl(fd, ORBIOCSETQUEUESIZE, (unsigned long)queue_size);
if (result < 0 && queue_size > 1) {
PX4_WARN("orb_advertise_multi: failed to set queue size");
}
/* get the advertiser handle and close the node */
orb_advert_t advertiser;
result = px4_ioctl(fd, ORBIOCGADVERTISER, (unsigned long)&advertiser);
int result = px4_ioctl(fd, ORBIOCGADVERTISER, (unsigned long)&advertiser);
px4_close(fd);
if (result == PX4_ERROR) {
@@ -602,6 +592,22 @@ int16_t uORB::Manager::process_remote_topic(const char *topic_name)
{
PX4_DEBUG("entering process_remote_topic: name: %s", topic_name);
// First make sure this is a valid topic
const struct orb_metadata *const *topic_list = orb_get_topics();
orb_id_t topic_ptr = nullptr;
for (size_t i = 0; i < orb_topics_count(); i++) {
if (strcmp(topic_list[i]->o_name, topic_name) == 0) {
topic_ptr = topic_list[i];
break;
}
}
if (! topic_ptr) {
PX4_ERR("process_remote_topic meta not found for %s\n", topic_name);
return -1;
}
// Look to see if we already have a node for this topic
char nodepath[orb_maxpath];
int ret = uORB::Utils::node_mkpath(nodepath, topic_name);
@@ -613,7 +619,7 @@ int16_t uORB::Manager::process_remote_topic(const char *topic_name)
uORB::DeviceNode *node = device_master->getDeviceNode(nodepath);
if (node) {
PX4_INFO("Marking DeviceNode(%s) as advertised in process_remote_topic", topic_name);
PX4_DEBUG("Marking DeviceNode(%s) as advertised in process_remote_topic", topic_name);
node->mark_as_advertised();
_remote_topics.insert(topic_name);
return 0;
@@ -622,27 +628,9 @@ int16_t uORB::Manager::process_remote_topic(const char *topic_name)
}
// We didn't find a node so we need to create it via an advertisement
const struct orb_metadata *const *topic_list = orb_get_topics();
orb_id_t topic_ptr = nullptr;
for (size_t i = 0; i < orb_topics_count(); i++) {
if (strcmp(topic_list[i]->o_name, topic_name) == 0) {
topic_ptr = topic_list[i];
break;
}
}
if (topic_ptr) {
PX4_INFO("Advertising remote topic %s", topic_name);
_remote_topics.insert(topic_name);
// Add some queue depth when advertising remote topics. These
// topics may get aggregated and thus delivered in a batch that
// requires some buffering in a queue.
orb_advertise(topic_ptr, nullptr, 5);
} else {
PX4_INFO("process_remote_topic meta not found for %s\n", topic_name);
}
PX4_DEBUG("Advertising remote topic %s", topic_name);
_remote_topics.insert(topic_name);
orb_advertise(topic_ptr, nullptr, topic_ptr->o_queue);
return 0;
}
@@ -663,8 +651,11 @@ int16_t uORB::Manager::process_add_subscription(const char *messageName)
PX4_DEBUG("DeviceNode(%s) not created yet", messageName);
} else {
// node is present.
node->process_add_subscription();
// node is present. But don't send any data to it if it
// is a node advertised by the remote side
if (_remote_topics.find(messageName) == false) {
node->process_add_subscription();
}
}
} else {
+3 -8
View File
@@ -215,17 +215,15 @@ public:
* @param data A pointer to the initial data to be published.
* For topics updated by interrupt handlers, the advertisement
* must be performed from non-interrupt context.
* @param queue_size Maximum number of buffered elements. If this is 1, no queuing is
* used.
* @return nullptr on error, otherwise returns an object pointer
* that can be used to publish to the topic.
* If the topic in question is not known (due to an
* ORB_DEFINE with no corresponding ORB_DECLARE)
* this function will return nullptr and set errno to ENOENT.
*/
orb_advert_t orb_advertise(const struct orb_metadata *meta, const void *data, unsigned int queue_size = 1)
orb_advert_t orb_advertise(const struct orb_metadata *meta, const void *data = nullptr)
{
return orb_advertise_multi(meta, data, nullptr, queue_size);
return orb_advertise_multi(meta, data, nullptr);
}
/**
@@ -250,16 +248,13 @@ public:
* @param instance Pointer to an integer which will yield the instance ID (0-based)
* of the publication. This is an output parameter and will be set to the newly
* created instance, ie. 0 for the first advertiser, 1 for the next and so on.
* @param queue_size Maximum number of buffered elements. If this is 1, no queuing is
* used.
* @return nullptr on error, otherwise returns a handle
* that can be used to publish to the topic.
* If the topic in question is not known (due to an
* ORB_DEFINE with no corresponding ORB_DECLARE)
* this function will return nullptr and set errno to ENOENT.
*/
orb_advert_t orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance,
unsigned int queue_size = 1);
orb_advert_t orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance);
/**
* Unadvertise a topic.
+2 -12
View File
@@ -89,8 +89,7 @@ int uORB::Manager::orb_exists(const struct orb_metadata *meta, int instance)
return data.ret;
}
orb_advert_t uORB::Manager::orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance,
unsigned int queue_size)
orb_advert_t uORB::Manager::orb_advertise_multi(const struct orb_metadata *meta, const void *data, int *instance)
{
/* open the node as an advertiser */
int fd = node_open(meta, true, instance);
@@ -100,19 +99,10 @@ orb_advert_t uORB::Manager::orb_advertise_multi(const struct orb_metadata *meta,
return nullptr;
}
/* Set the queue size. This must be done before the first publication; thus it fails if
* this is not the first advertiser.
*/
int result = px4_ioctl(fd, ORBIOCSETQUEUESIZE, (unsigned long)queue_size);
if (result < 0 && queue_size > 1) {
PX4_WARN("orb_advertise_multi: failed to set queue size");
}
/* get the advertiser handle and close the node */
orb_advert_t advertiser;
result = px4_ioctl(fd, ORBIOCGADVERTISER, (unsigned long)&advertiser);
int result = px4_ioctl(fd, ORBIOCGADVERTISER, (unsigned long)&advertiser);
px4_close(fd);
if (result == PX4_ERROR) {
@@ -574,8 +574,8 @@ int uORBTest::UnitTest::test_wrap_around()
bool updated{false};
// Advertise but not publish topics, only generate device_node, which is convenient for modifying DeviceNode::_generation
const int queue_size = 16;
ptopic = orb_advertise_queue(ORB_ID(orb_test_medium_wrap_around), nullptr, queue_size);
const int queue_size = orb_test_medium_s::ORB_QUEUE_LENGTH;
ptopic = orb_advertise(ORB_ID(orb_test_medium_wrap_around), nullptr);
if (ptopic == nullptr) {
return test_fail("advertise failed: %d", errno);
@@ -828,9 +828,9 @@ int uORBTest::UnitTest::test_queue()
return test_fail("subscribe failed: %d", errno);
}
const int queue_size = 16;
const int queue_size = orb_test_medium_s::ORB_QUEUE_LENGTH;
orb_test_medium_s t{};
ptopic = orb_advertise_queue(ORB_ID(orb_test_medium_queue), &t, queue_size);
ptopic = orb_advertise(ORB_ID(orb_test_medium_queue), &t);
if (ptopic == nullptr) {
return test_fail("advertise failed: %d", errno);
@@ -935,9 +935,9 @@ int uORBTest::UnitTest::pub_test_queue_main()
{
orb_test_medium_s t{};
orb_advert_t ptopic{nullptr};
const int queue_size = 50;
const int queue_size = orb_test_medium_s::ORB_QUEUE_LENGTH;
if ((ptopic = orb_advertise_queue(ORB_ID(orb_test_medium_queue_poll), &t, queue_size)) == nullptr) {
if ((ptopic = orb_advertise(ORB_ID(orb_test_medium_queue_poll), &t)) == nullptr) {
_thread_should_exit = true;
return test_fail("advertise failed: %d", errno);
}
@@ -40,15 +40,34 @@
#include <px4_platform_common/px4_work_queue/WorkQueueManager.hpp>
#include <uORB/uORB.h>
#if defined(CONFIG_MODULES_MUORB_APPS)
extern "C" { int muorb_init(); }
#endif
int px4_platform_init(void)
{
hrt_init();
px4::WorkQueueManagerStart();
// MUORB has slightly different startup requirements
#if defined(CONFIG_MODULES_MUORB_APPS)
//Put sleeper in here to allow wq to finish initializing before param_init is called
usleep(10000);
uorb_start();
muorb_init();
// Give muorb some time to setup the DSP
usleep(100000);
param_init();
#else
param_init();
uorb_start();
#endif
px4_log_initialize();
+1 -19
View File
@@ -45,28 +45,10 @@
namespace uORB
{
template <typename U> class DefaultQueueSize
{
private:
template <typename T>
static constexpr uint8_t get_queue_size(decltype(T::ORB_QUEUE_LENGTH) *)
{
return T::ORB_QUEUE_LENGTH;
}
template <typename T> static constexpr uint8_t get_queue_size(...)
{
return 1;
}
public:
static constexpr unsigned value = get_queue_size<U>(nullptr);
};
/**
* uORB publication wrapper class
*/
template<typename T, uint8_t ORB_QSIZE = DefaultQueueSize<T>::value>
template<typename T>
class Publication
{
public:
+1
View File
@@ -77,6 +77,7 @@ BMP388::init()
if (_chip_id == BMP390_CHIP_ID) {
_interface->set_device_type(DRV_BARO_DEVTYPE_BMP390);
this->_item_name = "bmp390";
}
_chip_rev_id = _interface->get_reg(BMP3_REV_ID_ADDR);
@@ -251,7 +251,7 @@ ICP201XX::RunImpl()
case STATE::CONFIG: {
if (configure()) {
_state = STATE::WAIT_READ;
ScheduleDelayed(30_ms);
ScheduleDelayed(50_ms);
} else {
if (hrt_elapsed_time(&_reset_timestamp) > 1000_ms) {
+6
View File
@@ -392,6 +392,12 @@ int BATT_SMBUS::get_startup_info()
uint16_t state_of_health;
ret |= _interface->read_word(BATT_SMBUS_STATE_OF_HEALTH, state_of_health);
/* ManufacturerAccess dummy command to init the ManufacturerBlockAccess routine
in the BQ40Zx0 and avoid timeout during LifetimeDataFlush.
test Sleep > 20 ms to give time to init the ManufacturerBlockAccess routine*/
ret |= _interface->write_word(BATT_SMBUS_MANUFACTURER_ACCESS, BATT_SMBUS_DEVICE_TYPE);
px4_usleep(30_ms);
if (!ret) {
_serial_number = serial_num;
_batt_startup_capacity = (uint16_t)((float)remaining_cap * _c_mult);
+1
View File
@@ -107,6 +107,7 @@ using namespace time_literals;
#define BATT_SMBUS_SECURITY_KEYS 0x0035
#define BATT_SMBUS_DEVICE_TYPE 0x0001
#define BATT_SMBUS_LIFETIME_FLUSH 0x002E
#define BATT_SMBUS_LIFETIME_BLOCK_ONE 0x0060
#define BATT_SMBUS_ENABLED_PROTECTIONS_A_ADDRESS 0x4938
@@ -314,7 +314,7 @@ CameraTrigger::CameraTrigger() :
// Advertise critical publishers here, because we cannot advertise in interrupt context
camera_trigger_s trigger{};
_trigger_pub = orb_advertise_queue(ORB_ID(camera_trigger), &trigger, camera_trigger_s::ORB_QUEUE_LENGTH);
_trigger_pub = orb_advertise(ORB_ID(camera_trigger), &trigger);
}
CameraTrigger::~CameraTrigger()
+2 -5
View File
@@ -64,13 +64,10 @@
/** Get the priority for the topic */
#define ORBIOCGPRIORITY _ORBIOC(14)
/** Set the queue size of the topic */
#define ORBIOCSETQUEUESIZE _ORBIOC(15)
/** Get the minimum interval at which the topic can be seen to be updated for this subscription */
#define ORBIOCGETINTERVAL _ORBIOC(16)
#define ORBIOCGETINTERVAL _ORBIOC(15)
/** Check whether the topic is advertised, sets *(unsigned long *)arg to 1 if advertised, 0 otherwise */
#define ORBIOCISADVERTISED _ORBIOC(17)
#define ORBIOCISADVERTISED _ORBIOC(16)
#endif /* _DRV_UORB_H */
@@ -88,7 +88,7 @@ private:
FIFO::DATA f[FIFO_MAX_SAMPLES] {};
};
// ensure no struct padding
static_assert(sizeof(FIFOTransferBuffer) == (4 + FIFO_MAX_SAMPLES *sizeof(FIFO::DATA)));
static_assert(sizeof(FIFOTransferBuffer) == (4 + FIFO_MAX_SAMPLES *sizeof(FIFO::DATA)), "Invalid transfer buffer size");
struct register_bank0_config_t {
Register::BANK_0 reg;
-2
View File
@@ -45,8 +45,6 @@ using namespace time_literals;
ToneAlarm::ToneAlarm() :
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::hp_default)
{
// ensure ORB_ID(tune_control) is advertised with correct queue depth
orb_advertise_queue(ORB_ID(tune_control), nullptr, tune_control_s::ORB_QUEUE_LENGTH);
}
ToneAlarm::~ToneAlarm()
+1
View File
@@ -45,6 +45,7 @@ px4_add_module(
voxl2_io.cpp
voxl2_io.hpp
DEPENDS
rc
px4_work_queue
mixer_module
MODULE_CONFIG
+1 -1
View File
@@ -151,7 +151,7 @@ private:
transponder_report_s tr{};
orb_advert_t fake_traffic_report_publisher = orb_advertise_queue(ORB_ID(transponder_report), &tr, (unsigned int)20);
orb_advert_t fake_traffic_report_publisher = orb_advertise(ORB_ID(transponder_report), &tr);
TRAFFIC_STATE _traffic_state_previous{TRAFFIC_STATE::NO_CONFLICT};
+1 -1
View File
@@ -61,7 +61,7 @@ void send(EventType &event)
orb_publish(ORB_ID(event), orb_event_pub, &event);
} else {
orb_event_pub = orb_advertise_queue(ORB_ID(event), &event, event_s::ORB_QUEUE_LENGTH);
orb_event_pub = orb_advertise(ORB_ID(event), &event);
}
pthread_mutex_unlock(&publish_event_mutex);
+2 -2
View File
@@ -42,7 +42,7 @@ class GeoTest : public ::testing::Test
public:
void SetUp() override
{
proj.initReference(math::radians(473566094 / 1e7), math::radians(85190237 / 1e7), 0);
proj.initReference(473566094 / 1e7, 85190237 / 1e7, 0);
}
protected:
@@ -73,7 +73,7 @@ TEST_F(GeoTest, reprojectProject)
TEST_F(GeoTest, projectReproject)
{
// GIVEN: x and y coordinates in the local cartesian frame
// GIVEN: lat and lon coordinates in the geographic coordinate system
double lat = 47.356616973876953;
double lon = 8.5190505981445313;
float x;
+18 -12
View File
@@ -162,6 +162,24 @@ public:
return res;
}
// Using this function reduces the number of temporary variables needed to compute A * B.T
template<size_t P>
Matrix<Type, M, M> multiplyByTranspose(const Matrix<Type, P, N> &other) const
{
Matrix<Type, M, P> res;
const Matrix<Type, M, N> &self = *this;
for (size_t i = 0; i < M; i++) {
for (size_t k = 0; k < P; k++) {
for (size_t j = 0; j < N; j++) {
res(i, k) += self(i, j) * other(k, j);
}
}
}
return res;
}
// Element-wise multiplication
Matrix<Type, M, N> emult(const Matrix<Type, M, N> &other) const
{
@@ -391,12 +409,6 @@ public:
for (unsigned j = 0; j < N; j++) {
double d = static_cast<double>(self(i, j));
// Matrix diagonal elements
if (N > 1 && M > 1 && i == j) {
// make diagonal elements bold (ANSI CSI n 1)
printf("\033[1m");
}
// if symmetric don't print upper triangular elements
if ((M == N) && (j > i) && (i < N) && (j < M)
&& (fabs(d - static_cast<double>(self(j, i))) < (double)eps)
@@ -417,12 +429,6 @@ public:
printf("% 6.5f ", d);
}
}
// Matrix diagonal elements
if (N > 1 && M > 1 && i == j) {
// reset any formatting (ANSI CSI n 0)
printf("\033[0m");
}
}
printf("\n");
@@ -14,7 +14,7 @@ class XMLInject():
def __init__(self, injected_xml_filename):
self.groups=[]
valid_parameter_attributes = set(["category", "default", "name", "type", "volatile"])
valid_parameter_attributes = set(["category", "default", "name", "type", "volatile", "boolean"])
valid_field_tags = set(["board","short_desc", "long_desc", "min", "max", "unit", "decimal", "increment", "reboot_required"])
valid_other_top_level_tags = set(["group","values"])
@@ -42,7 +42,8 @@ class XMLInject():
new_param.default = iparam.get('default')
elif param_attrib == 'volatile':
new_param.SetVolatile()
elif param_attrib == "boolean":
new_param.SetBoolean()
#get param info stored as child tags
for child in iparam:
+1 -1
View File
@@ -73,6 +73,6 @@ __EXPORT void mavlink_vasprintf(int severity, orb_advert_t *mavlink_log_pub, con
orb_publish(ORB_ID(mavlink_log), *mavlink_log_pub, &log_msg);
} else {
*mavlink_log_pub = orb_advertise_queue(ORB_ID(mavlink_log), &log_msg, mavlink_log_s::ORB_QUEUE_LENGTH);
*mavlink_log_pub = orb_advertise(ORB_ID(mavlink_log), &log_msg);
}
}
@@ -55,7 +55,7 @@ public:
void SetUp() override
{
// ensure topic exists, otherwise we might lose first queued events
orb_advertise_queue(ORB_ID(event), nullptr, event_s::ORB_QUEUE_LENGTH);
orb_advertise(ORB_ID(event), nullptr);
}
};
+2 -2
View File
@@ -153,7 +153,7 @@ int buzzer_init()
tune_durations[tune_control_s::TUNE_ID_BATTERY_WARNING_SLOW] = 800000;
tune_durations[tune_control_s::TUNE_ID_SINGLE_BEEP] = 300000;
tune_control_pub = orb_advertise_queue(ORB_ID(tune_control), &tune_control, tune_control_s::ORB_QUEUE_LENGTH);
tune_control_pub = orb_advertise(ORB_ID(tune_control), &tune_control);
return PX4_OK;
}
@@ -330,7 +330,7 @@ int led_init()
led_control.mode = led_control_s::MODE_OFF;
led_control.priority = 0;
led_control.timestamp = hrt_absolute_time();
led_control_pub = orb_advertise_queue(ORB_ID(led_control), &led_control, led_control_s::ORB_QUEUE_LENGTH);
led_control_pub = orb_advertise(ORB_ID(led_control), &led_control);
/* first open normal LEDs */
fd_leds = px4_open(LED0_DEVICE_PATH, O_RDWR);
+2 -2
View File
@@ -1006,8 +1006,8 @@ int do_mag_calibration_quick(orb_advert_t *mavlink_log_pub, float heading_radian
return PX4_ERROR;
}
calibration_log_critical(mavlink_log_pub, "Assuming vehicle is facing heading %.1f degrees",
(double)math::radians(heading_radians));
calibration_log_info(mavlink_log_pub, "Assuming vehicle is facing heading %.1f degrees",
(double)math::degrees(heading_radians));
matrix::Eulerf euler{matrix::Quatf{attitude.q}};
euler(2) = heading_radians;
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2023 PX4 Development Team. All rights reserved.
# Copyright (c) 2023-2024 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
@@ -31,17 +31,22 @@
#
############################################################################
add_subdirectory(DifferentialDriveControl)
add_subdirectory(DifferentialDriveGuidance)
add_subdirectory(DifferentialDriveKinematics)
px4_add_module(
MODULE modules__differential_drive_control
MAIN differential_drive_control
MODULE modules__differential_drive
MAIN differential_drive
SRCS
DifferentialDriveControl.cpp
DifferentialDriveControl.hpp
DifferentialDrive.cpp
DifferentialDrive.hpp
DEPENDS
DifferentialDriveControl
DifferentialDriveGuidance
DifferentialDriveKinematics
px4_work_queue
modules__control_allocator # for parameter CA_R_REV
MODULE_CONFIG
module.yaml
)
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (c) 2023-2024 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
@@ -31,38 +31,37 @@
*
****************************************************************************/
#include "DifferentialDriveControl.hpp"
#include "DifferentialDrive.hpp"
using namespace time_literals;
using namespace matrix;
namespace differential_drive_control
{
DifferentialDriveControl::DifferentialDriveControl() :
DifferentialDrive::DifferentialDrive() :
ModuleParams(nullptr),
ScheduledWorkItem(MODULE_NAME, px4::wq_configurations::rate_ctrl)
{
updateParams();
}
bool DifferentialDriveControl::init()
bool DifferentialDrive::init()
{
ScheduleOnInterval(10_ms); // 100 Hz
return true;
}
void DifferentialDriveControl::updateParams()
void DifferentialDrive::updateParams()
{
ModuleParams::updateParams();
_max_speed = _param_rdd_max_wheel_speed.get() * _param_rdd_wheel_radius.get();
_max_angular_velocity = _max_speed / (_param_rdd_wheel_base.get() / 2.f);
_differential_drive_kinematics.setWheelBase(_param_rdd_wheel_base.get());
_max_speed = _param_rdd_wheel_speed.get() * _param_rdd_wheel_radius.get();
_differential_drive_guidance.setMaxSpeed(_max_speed);
_differential_drive_kinematics.setMaxSpeed(_max_speed);
_max_angular_velocity = _max_speed / (_param_rdd_wheel_base.get() / 2.f);
_differential_drive_guidance.setMaxAngularVelocity(_max_angular_velocity);
_differential_drive_kinematics.setMaxAngularVelocity(_max_angular_velocity);
}
void DifferentialDriveControl::Run()
void DifferentialDrive::Run()
{
if (should_exit()) {
ScheduleClear();
@@ -70,20 +69,32 @@ void DifferentialDriveControl::Run()
}
hrt_abstime now = hrt_absolute_time();
const float dt = math::min((now - _time_stamp_last), 5000_ms) / 1e6f;
_time_stamp_last = now;
if (_parameter_update_sub.updated()) {
parameter_update_s pupdate;
_parameter_update_sub.copy(&pupdate);
parameter_update_s parameter_update;
_parameter_update_sub.copy(&parameter_update);
updateParams();
}
if (_vehicle_control_mode_sub.updated()) {
vehicle_control_mode_s vehicle_control_mode;
vehicle_control_mode_s vehicle_control_mode{};
if (_vehicle_control_mode_sub.copy(&vehicle_control_mode)) {
_armed = vehicle_control_mode.flag_armed;
_manual_driving = vehicle_control_mode.flag_control_manual_enabled; // change this when more modes are supported
_manual_driving = vehicle_control_mode.flag_control_manual_enabled;
_mission_driving = vehicle_control_mode.flag_control_auto_enabled;
}
}
if (_vehicle_status_sub.updated()) {
vehicle_status_s vehicle_status{};
if (_vehicle_status_sub.copy(&vehicle_status)) {
const bool armed = (vehicle_status.arming_state == vehicle_status_s::ARMING_STATE_ARMED);
const bool spooled_up = armed && (hrt_elapsed_time(&vehicle_status.armed_time) > _param_com_spoolup_time.get() * 1_s);
_differential_drive_kinematics.setArmed(spooled_up);
_acro_driving = (vehicle_status.nav_state == vehicle_status_s::NAVIGATION_STATE_ACRO);
}
}
@@ -94,43 +105,42 @@ void DifferentialDriveControl::Run()
manual_control_setpoint_s manual_control_setpoint{};
if (_manual_control_setpoint_sub.copy(&manual_control_setpoint)) {
_differential_drive_setpoint.timestamp = now;
_differential_drive_setpoint.speed = manual_control_setpoint.throttle * _param_rdd_speed_scale.get() * _max_speed;
_differential_drive_setpoint.yaw_rate = manual_control_setpoint.roll * _param_rdd_ang_velocity_scale.get() *
_max_angular_velocity;
_differential_drive_setpoint_pub.publish(_differential_drive_setpoint);
differential_drive_setpoint_s setpoint{};
setpoint.speed = manual_control_setpoint.throttle * math::max(0.f, _param_rdd_speed_scale.get()) * _max_speed;
setpoint.yaw_rate = manual_control_setpoint.roll * _param_rdd_ang_velocity_scale.get() * _max_angular_velocity;
// if acro mode, we activate the yaw rate control
if (_acro_driving) {
setpoint.closed_loop_speed_control = false;
setpoint.closed_loop_yaw_rate_control = true;
} else {
setpoint.closed_loop_speed_control = false;
setpoint.closed_loop_yaw_rate_control = false;
}
setpoint.timestamp = now;
_differential_drive_setpoint_pub.publish(setpoint);
}
}
} else if (_mission_driving) {
// Mission mode
// directly receive setpoints from the guidance library
_differential_drive_guidance.computeGuidance(
_differential_drive_control.getVehicleYaw(),
_differential_drive_control.getVehicleBodyYawRate(),
dt
);
}
_differential_drive_setpoint_sub.update(&_differential_drive_setpoint);
// publish data to actuator_motors (output module)
// get the wheel speeds from the inverse kinematics class (DifferentialDriveKinematics)
Vector2f wheel_speeds = _differential_drive_kinematics.computeInverseKinematics(
_differential_drive_setpoint.speed,
_differential_drive_setpoint.yaw_rate);
// Check if max_angular_wheel_speed is zero
const bool setpoint_timeout = (_differential_drive_setpoint.timestamp + 100_ms) < now;
const bool valid_max_speed = _param_rdd_speed_scale.get() > FLT_EPSILON;
if (!_armed || setpoint_timeout || !valid_max_speed) {
wheel_speeds = {}; // stop
}
wheel_speeds = matrix::constrain(wheel_speeds, -1.f, 1.f);
actuator_motors_s actuator_motors{};
actuator_motors.reversible_flags = _param_r_rev.get(); // should be 3 see rc.rover_differential_defaults
wheel_speeds.copyTo(actuator_motors.control);
actuator_motors.timestamp = now;
_actuator_motors_pub.publish(actuator_motors);
_differential_drive_control.control(dt);
_differential_drive_kinematics.allocate();
}
int DifferentialDriveControl::task_spawn(int argc, char *argv[])
int DifferentialDrive::task_spawn(int argc, char *argv[])
{
DifferentialDriveControl *instance = new DifferentialDriveControl();
DifferentialDrive *instance = new DifferentialDrive();
if (instance) {
_object.store(instance);
@@ -151,12 +161,12 @@ int DifferentialDriveControl::task_spawn(int argc, char *argv[])
return PX4_ERROR;
}
int DifferentialDriveControl::custom_command(int argc, char *argv[])
int DifferentialDrive::custom_command(int argc, char *argv[])
{
return print_usage("unknown command");
}
int DifferentialDriveControl::print_usage(const char *reason)
int DifferentialDrive::print_usage(const char *reason)
{
if (reason) {
PX4_ERR("%s\n", reason);
@@ -168,15 +178,13 @@ int DifferentialDriveControl::print_usage(const char *reason)
Rover Differential Drive controller.
)DESCR_STR");
PRINT_MODULE_USAGE_NAME("differential_drive_control", "controller");
PRINT_MODULE_USAGE_NAME("differential_drive", "controller");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
return 0;
}
extern "C" __EXPORT int differential_drive_control_main(int argc, char *argv[])
extern "C" __EXPORT int differential_drive_main(int argc, char *argv[])
{
return DifferentialDriveControl::main(argc, argv);
return DifferentialDrive::main(argc, argv);
}
} // namespace differential_drive_control
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (c) 2023-2024 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
@@ -33,41 +33,31 @@
#pragma once
// PX4 includes
#include <px4_platform_common/px4_config.h>
#include <px4_platform_common/defines.h>
#include <px4_platform_common/module.h>
#include <px4_platform_common/module_params.h>
#include <px4_platform_common/px4_work_queue/ScheduledWorkItem.hpp>
// uORB includes
#include <uORB/topics/actuator_outputs.h>
#include <uORB/topics/actuator_motors.h>
#include <uORB/PublicationMulti.hpp>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/SubscriptionMultiArray.hpp>
#include <uORB/topics/differential_drive_setpoint.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/vehicle_control_mode.h>
#include <uORB/topics/vehicle_status.h>
// Standard library includes
#include <math.h>
#include "DifferentialDriveControl/DifferentialDriveControl.hpp"
#include "DifferentialDriveGuidance/DifferentialDriveGuidance.hpp"
#include "DifferentialDriveKinematics/DifferentialDriveKinematics.hpp"
// Local includes
#include <DifferentialDriveKinematics.hpp>
using namespace time_literals;
namespace differential_drive_control
{
class DifferentialDriveControl : public ModuleBase<DifferentialDriveControl>, public ModuleParams,
class DifferentialDrive : public ModuleBase<DifferentialDrive>, public ModuleParams,
public px4::ScheduledWorkItem
{
public:
DifferentialDriveControl();
~DifferentialDriveControl() override = default;
DifferentialDrive();
~DifferentialDrive() override = default;
/** @see ModuleBase */
static int task_spawn(int argc, char *argv[]);
@@ -85,32 +75,31 @@ protected:
private:
void Run() override;
uORB::Subscription _differential_drive_setpoint_sub{ORB_ID(differential_drive_setpoint)};
uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)};
uORB::Subscription _parameter_update_sub{ORB_ID(parameter_update)};
uORB::Subscription _vehicle_control_mode_sub{ORB_ID(vehicle_control_mode)};
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
uORB::PublicationMulti<actuator_motors_s> _actuator_motors_pub{ORB_ID(actuator_motors)};
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
uORB::Publication<differential_drive_setpoint_s> _differential_drive_setpoint_pub{ORB_ID(differential_drive_setpoint)};
differential_drive_setpoint_s _differential_drive_setpoint{};
DifferentialDriveKinematics _differential_drive_kinematics{};
bool _armed = false;
bool _manual_driving = false;
bool _mission_driving = false;
bool _acro_driving = false;
hrt_abstime _time_stamp_last{0}; /**< time stamp when task was last updated */
DifferentialDriveGuidance _differential_drive_guidance{this};
DifferentialDriveControl _differential_drive_control{this};
DifferentialDriveKinematics _differential_drive_kinematics{this};
float _max_speed{0.f};
float _max_angular_velocity{0.f};
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RDD_SPEED_SCALE>) _param_rdd_speed_scale,
(ParamFloat<px4::params::RDD_ANG_SCALE>) _param_rdd_ang_velocity_scale,
(ParamFloat<px4::params::RDD_WHL_SPEED>) _param_rdd_max_wheel_speed,
(ParamFloat<px4::params::RDD_SPEED_SCALE>) _param_rdd_speed_scale,
(ParamFloat<px4::params::RDD_WHEEL_BASE>) _param_rdd_wheel_base,
(ParamFloat<px4::params::RDD_WHEEL_SPEED>) _param_rdd_wheel_speed,
(ParamFloat<px4::params::RDD_WHEEL_RADIUS>) _param_rdd_wheel_radius,
(ParamInt<px4::params::CA_R_REV>) _param_r_rev
(ParamFloat<px4::params::COM_SPOOLUP_TIME>) _param_com_spoolup_time
)
};
} // namespace differential_drive_control
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2020 PX4 Development Team. All rights reserved.
# Copyright (c) 2024 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
@@ -30,19 +30,10 @@
# POSSIBILITY OF SUCH DAMAGE.
#
############################################################################
px4_add_module(
MODULE drivers__imu__invensense__icm42688p
MAIN icm42688p
COMPILE_FLAGS
${MAX_CUSTOM_OPT_LEVEL}
SRCS
icm42688p_main.cpp
ICM42688P.cpp
ICM42688P.hpp
InvenSense_ICM42688P_registers.hpp
DEPENDS
px4_work_queue
drivers_accelerometer
drivers_gyroscope
drivers__device
)
px4_add_library(DifferentialDriveControl
DifferentialDriveControl.cpp
)
target_link_libraries(DifferentialDriveControl PUBLIC pid)
target_include_directories(DifferentialDriveControl PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
@@ -0,0 +1,109 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 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.
*
****************************************************************************/
#include "DifferentialDriveControl.hpp"
using namespace matrix;
DifferentialDriveControl::DifferentialDriveControl(ModuleParams *parent) : ModuleParams(parent)
{
pid_init(&_pid_angular_velocity, PID_MODE_DERIVATIV_NONE, 0.001f);
pid_init(&_pid_speed, PID_MODE_DERIVATIV_NONE, 0.001f);
}
void DifferentialDriveControl::updateParams()
{
ModuleParams::updateParams();
pid_set_parameters(&_pid_angular_velocity,
_param_rdd_p_gain_angular_velocity.get(), // Proportional gain
_param_rdd_i_gain_angular_velocity.get(), // Integral gain
0, // Derivative gain
20, // Integral limit
200); // Output limit
pid_set_parameters(&_pid_speed,
_param_rdd_p_gain_speed.get(), // Proportional gain
_param_rdd_i_gain_speed.get(), // Integral gain
0, // Derivative gain
2, // Integral limit
200); // Output limit
}
void DifferentialDriveControl::control(float dt)
{
if (_vehicle_angular_velocity_sub.updated()) {
vehicle_angular_velocity_s vehicle_angular_velocity{};
if (_vehicle_angular_velocity_sub.copy(&vehicle_angular_velocity)) {
_vehicle_body_yaw_rate = vehicle_angular_velocity.xyz[2];
}
}
if (_vehicle_attitude_sub.updated()) {
vehicle_attitude_s vehicle_attitude{};
if (_vehicle_attitude_sub.copy(&vehicle_attitude)) {
_vehicle_attitude_quaternion = Quatf(vehicle_attitude.q);
_vehicle_yaw = matrix::Eulerf(_vehicle_attitude_quaternion).psi();
}
}
if (_vehicle_local_position_sub.updated()) {
vehicle_local_position_s vehicle_local_position{};
if (_vehicle_local_position_sub.copy(&vehicle_local_position)) {
Vector3f velocity_in_local_frame(vehicle_local_position.vx, vehicle_local_position.vy, vehicle_local_position.vz);
Vector3f velocity_in_body_frame = _vehicle_attitude_quaternion.rotateVectorInverse(velocity_in_local_frame);
_vehicle_forward_speed = velocity_in_body_frame(0);
}
}
_differential_drive_setpoint_sub.update(&_differential_drive_setpoint);
// PID to reach setpoint using control_output
differential_drive_setpoint_s differential_drive_control_output = _differential_drive_setpoint;
if (_differential_drive_setpoint.closed_loop_speed_control) {
differential_drive_control_output.speed +=
pid_calculate(&_pid_speed, _differential_drive_setpoint.speed, _vehicle_forward_speed, 0, dt);
}
if (_differential_drive_setpoint.closed_loop_yaw_rate_control) {
differential_drive_control_output.yaw_rate +=
pid_calculate(&_pid_angular_velocity, _differential_drive_setpoint.yaw_rate, _vehicle_body_yaw_rate, 0, dt);
}
differential_drive_control_output.timestamp = hrt_absolute_time();
_differential_drive_control_output_pub.publish(differential_drive_control_output);
}
@@ -0,0 +1,91 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 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 DifferentialDriveControl.hpp
*
* Controller for heading rate and forward speed.
*/
#pragma once
#include <lib/pid/pid.h>
#include <matrix/matrix/math.hpp>
#include <px4_platform_common/module_params.h>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/topics/differential_drive_setpoint.h>
#include <uORB/topics/vehicle_angular_velocity.h>
#include <uORB/topics/vehicle_attitude.h>
#include <uORB/topics/vehicle_local_position.h>
class DifferentialDriveControl : public ModuleParams
{
public:
DifferentialDriveControl(ModuleParams *parent);
~DifferentialDriveControl() = default;
void control(float dt);
float getVehicleBodyYawRate() const { return _vehicle_body_yaw_rate; }
float getVehicleYaw() const { return _vehicle_yaw; }
protected:
void updateParams() override;
private:
uORB::Subscription _differential_drive_setpoint_sub{ORB_ID(differential_drive_setpoint)};
uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
uORB::Subscription _vehicle_attitude_sub{ORB_ID(vehicle_attitude)};
uORB::Subscription _vehicle_local_position_sub{ORB_ID(vehicle_local_position)};
uORB::Publication<differential_drive_setpoint_s> _differential_drive_control_output_pub{ORB_ID(differential_drive_control_output)};
differential_drive_setpoint_s _differential_drive_setpoint{};
matrix::Quatf _vehicle_attitude_quaternion{};
float _vehicle_yaw{0.f};
// States
float _vehicle_body_yaw_rate{0.f};
float _vehicle_forward_speed{0.f};
PID_t _pid_angular_velocity; ///< The PID controller for yaw rate.
PID_t _pid_speed; ///< The PID controller for velocity.
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RDD_P_SPEED>) _param_rdd_p_gain_speed,
(ParamFloat<px4::params::RDD_I_SPEED>) _param_rdd_i_gain_speed,
(ParamFloat<px4::params::RDD_P_ANG_VEL>) _param_rdd_p_gain_angular_velocity,
(ParamFloat<px4::params::RDD_I_ANG_VEL>) _param_rdd_i_gain_angular_velocity
)
};
@@ -0,0 +1,38 @@
############################################################################
#
# Copyright (c) 2023-2024 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.
#
############################################################################
px4_add_library(DifferentialDriveGuidance
DifferentialDriveGuidance.cpp
)
target_include_directories(DifferentialDriveGuidance PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
@@ -0,0 +1,138 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 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.
*
****************************************************************************/
#include "DifferentialDriveGuidance.hpp"
#include <mathlib/math/Limits.hpp>
using namespace matrix;
DifferentialDriveGuidance::DifferentialDriveGuidance(ModuleParams *parent) : ModuleParams(parent)
{
updateParams();
pid_init(&_heading_p_controller, PID_MODE_DERIVATIV_NONE, 0.001f);
}
void DifferentialDriveGuidance::computeGuidance(float yaw, float angular_velocity, float dt)
{
if (_position_setpoint_triplet_sub.updated()) {
_position_setpoint_triplet_sub.copy(&_position_setpoint_triplet);
}
if (_vehicle_global_position_sub.updated()) {
_vehicle_global_position_sub.copy(&_vehicle_global_position);
}
matrix::Vector2d global_position(_vehicle_global_position.lat, _vehicle_global_position.lon);
matrix::Vector2d current_waypoint(_position_setpoint_triplet.current.lat, _position_setpoint_triplet.current.lon);
matrix::Vector2d next_waypoint(_position_setpoint_triplet.next.lat, _position_setpoint_triplet.next.lon);
const float distance_to_next_wp = get_distance_to_next_waypoint(global_position(0), global_position(1),
current_waypoint(0),
current_waypoint(1));
float desired_heading = get_bearing_to_next_waypoint(global_position(0), global_position(1), current_waypoint(0),
current_waypoint(1));
float heading_error = matrix::wrap_pi(desired_heading - yaw);
if (_current_waypoint != current_waypoint) {
_currentState = GuidanceState::TURNING;
}
// Make rover stop when it arrives at the last waypoint instead of loitering and driving around weirdly.
if ((current_waypoint == next_waypoint) && distance_to_next_wp <= _param_nav_acc_rad.get()) {
_currentState = GuidanceState::GOAL_REACHED;
}
float desired_speed = 0.f;
switch (_currentState) {
case GuidanceState::TURNING:
desired_speed = 0.f;
if (fabsf(heading_error) < 0.05f) {
_currentState = GuidanceState::DRIVING;
}
break;
case GuidanceState::DRIVING: {
const float max_velocity = math::trajectory::computeMaxSpeedFromDistance(_param_rdd_max_jerk.get(),
_param_rdd_max_accel.get(), distance_to_next_wp, 0.0f);
_forwards_velocity_smoothing.updateDurations(max_velocity);
_forwards_velocity_smoothing.updateTraj(dt);
desired_speed = math::interpolate<float>(abs(heading_error), 0.1f, 0.8f,
_forwards_velocity_smoothing.getCurrentVelocity(), 0.0f);
break;
}
case GuidanceState::GOAL_REACHED:
// temporary till I find a better way to stop the vehicle
desired_speed = 0.f;
heading_error = 0.f;
angular_velocity = 0.f;
_desired_angular_velocity = 0.f;
break;
}
// Compute the desired angular velocity relative to the heading error, to steer the vehicle towards the next waypoint.
float angular_velocity_pid = pid_calculate(&_heading_p_controller, heading_error, angular_velocity, 0,
dt) + heading_error;
differential_drive_setpoint_s output{};
output.speed = math::constrain(desired_speed, -_max_speed, _max_speed);
output.yaw_rate = math::constrain(angular_velocity_pid, -_max_angular_velocity, _max_angular_velocity);
output.closed_loop_speed_control = output.closed_loop_yaw_rate_control = true;
output.timestamp = hrt_absolute_time();
_differential_drive_setpoint_pub.publish(output);
_current_waypoint = current_waypoint;
}
void DifferentialDriveGuidance::updateParams()
{
ModuleParams::updateParams();
pid_set_parameters(&_heading_p_controller,
_param_rdd_p_gain_heading.get(), // Proportional gain
0, // Integral gain
0, // Derivative gain
0, // Integral limit
200); // Output limit
_forwards_velocity_smoothing.setMaxJerk(_param_rdd_max_jerk.get());
_forwards_velocity_smoothing.setMaxAccel(_param_rdd_max_accel.get());
_forwards_velocity_smoothing.setMaxVel(_max_speed);
}
@@ -0,0 +1,140 @@
/****************************************************************************
*
* Copyright (c) 2023-2024 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#pragma once
#include <px4_platform_common/module_params.h>
#include <matrix/matrix/math.hpp>
#include <matrix/math.hpp>
#include <mathlib/mathlib.h>
#include <lib/geo/geo.h>
#include <math.h>
#include <lib/motion_planning/PositionSmoothing.hpp>
#include <lib/motion_planning/VelocitySmoothing.hpp>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/topics/differential_drive_setpoint.h>
#include <uORB/topics/position_setpoint_triplet.h>
#include <uORB/topics/vehicle_global_position.h>
#include <lib/pid/pid.h>
/**
* @brief Enum class for the different states of guidance.
*/
enum class GuidanceState {
TURNING, ///< The vehicle is currently turning.
DRIVING, ///< The vehicle is currently driving straight.
GOAL_REACHED ///< The vehicle has reached its goal.
};
/**
* @brief Class for differential drive guidance.
*/
class DifferentialDriveGuidance : public ModuleParams
{
public:
/**
* @brief Constructor for DifferentialDriveGuidance.
* @param parent The parent ModuleParams object.
*/
DifferentialDriveGuidance(ModuleParams *parent);
~DifferentialDriveGuidance() = default;
/**
* @brief Compute guidance for the vehicle.
* @param global_pos The global position of the vehicle in degrees.
* @param current_waypoint The current waypoint the vehicle is heading towards in degrees.
* @param next_waypoint The next waypoint the vehicle will head towards after reaching the current waypoint in degrees.
* @param vehicle_yaw The yaw orientation of the vehicle in radians.
* @param body_velocity The velocity of the vehicle in m/s.
* @param angular_velocity The angular velocity of the vehicle in rad/s.
* @param dt The time step in seconds.
*/
void computeGuidance(float yaw, float angular_velocity, float dt);
/**
* @brief Set the maximum speed for the vehicle.
* @param max_speed The maximum speed in m/s.
* @return The set maximum speed in m/s.
*/
float setMaxSpeed(float max_speed) { return _max_speed = max_speed; }
/**
* @brief Set the maximum angular velocity for the vehicle.
* @param max_angular_velocity The maximum angular velocity in rad/s.
* @return The set maximum angular velocity in rad/s.
*/
float setMaxAngularVelocity(float max_angular_velocity) { return _max_angular_velocity = max_angular_velocity; }
protected:
/**
* @brief Update the parameters of the module.
*/
void updateParams() override;
private:
uORB::Subscription _position_setpoint_triplet_sub{ORB_ID(position_setpoint_triplet)};
uORB::Subscription _vehicle_global_position_sub{ORB_ID(vehicle_global_position)};
uORB::Publication<differential_drive_setpoint_s> _differential_drive_setpoint_pub{ORB_ID(differential_drive_setpoint)};
position_setpoint_triplet_s _position_setpoint_triplet{};
vehicle_global_position_s _vehicle_global_position{};
GuidanceState _currentState; ///< The current state of guidance.
float _desired_angular_velocity; ///< The desired angular velocity.
float _max_speed; ///< The maximum speed.
float _max_angular_velocity; ///< The maximum angular velocity.
matrix::Vector2d _current_waypoint; ///< The current waypoint.
VelocitySmoothing _forwards_velocity_smoothing; ///< The velocity smoothing for forward motion.
PositionSmoothing _position_smoothing; ///< The position smoothing.
PID_t _heading_p_controller; ///< The PID controller for yaw rate.
DEFINE_PARAMETERS(
(ParamFloat<px4::params::RDD_P_HEADING>) _param_rdd_p_gain_heading,
(ParamFloat<px4::params::NAV_ACC_RAD>) _param_nav_acc_rad,
(ParamFloat<px4::params::RDD_MAX_JERK>) _param_rdd_max_jerk,
(ParamFloat<px4::params::RDD_MAX_ACCEL>) _param_rdd_max_accel
)
};
@@ -1,6 +1,6 @@
############################################################################
#
# Copyright (c) 2023 PX4 Development Team. All rights reserved.
# Copyright (c) 2023-2024 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
@@ -37,4 +37,4 @@ px4_add_library(DifferentialDriveKinematics
target_include_directories(DifferentialDriveKinematics PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
px4_add_unit_gtest(SRC DifferentialDriveKinematicsTest.cpp LINKLIBS DifferentialDriveKinematics)
px4_add_functional_gtest(SRC DifferentialDriveKinematicsTest.cpp LINKLIBS DifferentialDriveKinematics)
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2023 PX4 Development Team. All rights reserved.
* Copyright (C) 2023-2024 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
@@ -36,8 +36,38 @@
#include <mathlib/mathlib.h>
using namespace matrix;
using namespace time_literals;
matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float linear_velocity_x, float yaw_rate)
DifferentialDriveKinematics::DifferentialDriveKinematics(ModuleParams *parent) : ModuleParams(parent)
{}
void DifferentialDriveKinematics::allocate()
{
hrt_abstime now = hrt_absolute_time();
if (_differential_drive_control_output_sub.updated()) {
_differential_drive_control_output_sub.copy(&_differential_drive_control_output);
}
const bool setpoint_timeout = (_differential_drive_control_output.timestamp + 100_ms) < now;
Vector2f wheel_speeds =
computeInverseKinematics(_differential_drive_control_output.speed, _differential_drive_control_output.yaw_rate);
if (!_armed || setpoint_timeout) {
wheel_speeds = {}; // stop
}
wheel_speeds = matrix::constrain(wheel_speeds, -1.f, 1.f);
actuator_motors_s actuator_motors{};
actuator_motors.reversible_flags = _param_r_rev.get(); // should be 3 see rc.rover_differential_defaults
wheel_speeds.copyTo(actuator_motors.control);
actuator_motors.timestamp = now;
_actuator_motors_pub.publish(actuator_motors);
}
matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float linear_velocity_x, float yaw_rate) const
{
if (_max_speed < FLT_EPSILON) {
return Vector2f();
@@ -54,7 +84,7 @@ matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float lin
if (combined_velocity > _max_speed) {
float excess_velocity = fabsf(combined_velocity - _max_speed);
float adjusted_linear_velocity = fabsf(linear_velocity_x) - excess_velocity;
const float adjusted_linear_velocity = fabsf(linear_velocity_x) - excess_velocity;
gain = adjusted_linear_velocity / fabsf(linear_velocity_x);
}
@@ -65,4 +95,3 @@ matrix::Vector2f DifferentialDriveKinematics::computeInverseKinematics(float lin
return Vector2f(linear_velocity_x - rotational_velocity,
linear_velocity_x + rotational_velocity) / _max_speed;
}
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (c) 2023 PX4 Development Team. All rights reserved.
* Copyright (c) 2023-2024 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
@@ -34,6 +34,11 @@
#pragma once
#include <matrix/matrix/math.hpp>
#include <px4_platform_common/module_params.h>
#include <uORB/PublicationMulti.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/topics/actuator_motors.h>
#include <uORB/topics/differential_drive_setpoint.h>
/**
* @brief Differential Drive Kinematics class for computing the kinematics of a differential drive robot.
@@ -41,10 +46,10 @@
* This class provides functions to set the wheel base and radius, and to compute the inverse kinematics
* given linear velocity and yaw rate.
*/
class DifferentialDriveKinematics
class DifferentialDriveKinematics : public ModuleParams
{
public:
DifferentialDriveKinematics() = default;
DifferentialDriveKinematics(ModuleParams *parent);
~DifferentialDriveKinematics() = default;
/**
@@ -68,6 +73,10 @@ public:
*/
void setMaxAngularVelocity(const float max_angular_velocity) { _max_angular_velocity = max_angular_velocity; };
void setArmed(const bool armed) { _armed = armed; };
void allocate();
/**
* @brief Computes the inverse kinematics for differential drive.
*
@@ -75,10 +84,20 @@ public:
* @param yaw_rate Yaw rate of the robot.
* @return matrix::Vector2f Motor velocities for the right and left motors.
*/
matrix::Vector2f computeInverseKinematics(float linear_velocity_x, float yaw_rate);
matrix::Vector2f computeInverseKinematics(float linear_velocity_x, float yaw_rate) const;
private:
uORB::Subscription _differential_drive_control_output_sub{ORB_ID(differential_drive_control_output)};
uORB::PublicationMulti<actuator_motors_s> _actuator_motors_pub{ORB_ID(actuator_motors)};
differential_drive_setpoint_s _differential_drive_control_output{};
bool _armed = false;
float _wheel_base{0.f};
float _max_speed{0.f};
float _max_angular_velocity{0.f};
DEFINE_PARAMETERS(
(ParamInt<px4::params::CA_R_REV>) _param_r_rev
)
};
@@ -1,6 +1,6 @@
/****************************************************************************
*
* Copyright (C) 2023 PX4 Development Team. All rights reserved.
* Copyright (C) 2023-2024 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
@@ -37,9 +37,14 @@
using namespace matrix;
TEST(DifferentialDriveKinematicsTest, AllZeroInputCase)
class DifferentialDriveKinematicsTest : public ::testing::Test
{
public:
DifferentialDriveKinematics kinematics{nullptr};
};
TEST_F(DifferentialDriveKinematicsTest, AllZeroInputCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(10.f);
kinematics.setMaxAngularVelocity(10.f);
@@ -49,9 +54,8 @@ TEST(DifferentialDriveKinematicsTest, AllZeroInputCase)
}
TEST(DifferentialDriveKinematicsTest, InvalidParameterCase)
TEST_F(DifferentialDriveKinematicsTest, InvalidParameterCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(0.f);
kinematics.setMaxSpeed(10.f);
kinematics.setMaxAngularVelocity(10.f);
@@ -61,9 +65,8 @@ TEST(DifferentialDriveKinematicsTest, InvalidParameterCase)
}
TEST(DifferentialDriveKinematicsTest, UnitCase)
TEST_F(DifferentialDriveKinematicsTest, UnitCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(10.f);
kinematics.setMaxAngularVelocity(10.f);
@@ -73,9 +76,8 @@ TEST(DifferentialDriveKinematicsTest, UnitCase)
}
TEST(DifferentialDriveKinematicsTest, UnitSaturationCase)
TEST_F(DifferentialDriveKinematicsTest, UnitSaturationCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -85,9 +87,8 @@ TEST(DifferentialDriveKinematicsTest, UnitSaturationCase)
}
TEST(DifferentialDriveKinematicsTest, OppositeUnitSaturationCase)
TEST_F(DifferentialDriveKinematicsTest, OppositeUnitSaturationCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -96,9 +97,8 @@ TEST(DifferentialDriveKinematicsTest, OppositeUnitSaturationCase)
EXPECT_EQ(kinematics.computeInverseKinematics(-1.f, 1.f), Vector2f(-1, 0));
}
TEST(DifferentialDriveKinematicsTest, RandomCase)
TEST_F(DifferentialDriveKinematicsTest, RandomCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(2.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -107,9 +107,8 @@ TEST(DifferentialDriveKinematicsTest, RandomCase)
EXPECT_EQ(kinematics.computeInverseKinematics(0.5f, 0.7f), Vector2f(-0.4f, 1.0f));
}
TEST(DifferentialDriveKinematicsTest, RotateInPlaceCase)
TEST_F(DifferentialDriveKinematicsTest, RotateInPlaceCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -118,9 +117,8 @@ TEST(DifferentialDriveKinematicsTest, RotateInPlaceCase)
EXPECT_EQ(kinematics.computeInverseKinematics(0.f, 1.f), Vector2f(-0.5f, 0.5f));
}
TEST(DifferentialDriveKinematicsTest, StraightMovementCase)
TEST_F(DifferentialDriveKinematicsTest, StraightMovementCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -129,9 +127,8 @@ TEST(DifferentialDriveKinematicsTest, StraightMovementCase)
EXPECT_EQ(kinematics.computeInverseKinematics(1.f, 0.f), Vector2f(1.f, 1.f));
}
TEST(DifferentialDriveKinematicsTest, MinInputValuesCase)
TEST_F(DifferentialDriveKinematicsTest, MinInputValuesCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(FLT_MIN);
kinematics.setMaxSpeed(FLT_MIN);
kinematics.setMaxAngularVelocity(FLT_MIN);
@@ -140,9 +137,8 @@ TEST(DifferentialDriveKinematicsTest, MinInputValuesCase)
EXPECT_EQ(kinematics.computeInverseKinematics(FLT_MIN, FLT_MIN), Vector2f(0.f, 0.f));
}
TEST(DifferentialDriveKinematicsTest, MaxSpeedLimitCase)
TEST_F(DifferentialDriveKinematicsTest, MaxSpeedLimitCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -151,9 +147,8 @@ TEST(DifferentialDriveKinematicsTest, MaxSpeedLimitCase)
EXPECT_EQ(kinematics.computeInverseKinematics(10.f, 10.f), Vector2f(0.f, 1.f));
}
TEST(DifferentialDriveKinematicsTest, MaxSpeedForwardsCase)
TEST_F(DifferentialDriveKinematicsTest, MaxSpeedForwardsCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(1.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -162,9 +157,8 @@ TEST(DifferentialDriveKinematicsTest, MaxSpeedForwardsCase)
EXPECT_EQ(kinematics.computeInverseKinematics(10.f, 0.f), Vector2f(1.f, 1.f));
}
TEST(DifferentialDriveKinematicsTest, MaxAngularCase)
TEST_F(DifferentialDriveKinematicsTest, MaxAngularCase)
{
DifferentialDriveKinematics kinematics;
kinematics.setWheelBase(2.f);
kinematics.setMaxSpeed(1.f);
kinematics.setMaxAngularVelocity(1.f);
@@ -1,5 +1,5 @@
menuconfig MODULES_DIFFERENTIAL_DRIVE_CONTROL
bool "differential_drive_control"
menuconfig MODULES_DIFFERENTIAL_DRIVE
bool "differential_drive"
default n
depends on MODULES_CONTROL_ALLOCATOR
---help---
+122
View File
@@ -0,0 +1,122 @@
module_name: Differential Drive
parameters:
- group: Rover Differential Drive
definitions:
RDD_WHEEL_BASE:
description:
short: Wheel base
long: Distance from the center of the right wheel to the center of the left wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.5
RDD_WHEEL_RADIUS:
description:
short: Wheel radius
long: Size of the wheel, half the diameter of the wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.1
RDD_SPEED_SCALE:
description:
short: Manual speed scale
type: float
min: 0
max: 1
increment: 0.01
decimal: 2
default: 1
RDD_ANG_SCALE:
description:
short: Manual angular velocity scale
type: float
min: 0
max: 1
increment: 0.01
decimal: 2
default: 1
RDD_WHEEL_SPEED:
description:
short: Maximum wheel speed
type: float
unit: rad/s
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0.3
RDD_P_HEADING:
description:
short: Proportional gain for heading controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 1
RDD_P_SPEED:
description:
short: Proportional gain for speed controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 1
RDD_I_SPEED:
description:
short: Integral gain for ground speed controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0
RDD_P_ANG_VEL:
description:
short: Proportional gain for angular velocity controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 1
RDD_I_ANG_VEL:
description:
short: Integral gain for angular velocity controller
type: float
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0
RDD_MAX_JERK:
description:
short: Maximum jerk
long: Limit for forwards acc/deceleration change.
type: float
unit: m/s^3
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0.5
RDD_MAX_ACCEL:
description:
short: Maximum acceleration
long: Maximum acceleration is used to limit the acceleration of the rover
type: float
unit: m/s^2
min: 0
max: 100
increment: 0.01
decimal: 2
default: 0.5
@@ -1,55 +0,0 @@
module_name: Differential Drive Control
parameters:
- group: Rover Differential Drive
definitions:
RDD_WHEEL_BASE:
description:
short: Wheel base
long: Distance from the center of the right wheel to the center of the left wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.5
RDD_WHEEL_RADIUS:
description:
short: Wheel radius
long: Size of the wheel, half the diameter of the wheel
type: float
unit: m
min: 0.001
max: 100
increment: 0.001
decimal: 3
default: 0.1
RDD_SPEED_SCALE:
description:
short: Manual speed scale
type: float
min: 0
max: 1.0
increment: 0.01
decimal: 2
default: 1.0
RDD_ANG_SCALE:
description:
short: Manual angular velocity scale
type: float
min: 0
max: 1.0
increment: 0.01
decimal: 2
default: 1.0
RDD_WHL_SPEED:
description:
short: Maximum wheel speed
type: float
unit: rad/s
min: 0
max: 100
increment: 0.01
decimal: 2
default: 10
+2 -1
View File
@@ -127,7 +127,8 @@ list(APPEND EKF_SRCS
EKF/height_control.cpp
EKF/imu_down_sampler.cpp
EKF/output_predictor.cpp
EKF/vel_pos_fusion.cpp
EKF/velocity_fusion.cpp
EKF/position_fusion.cpp
EKF/yaw_fusion.cpp
EKF/zero_innovation_heading_update.cpp
+2 -1
View File
@@ -44,7 +44,8 @@ list(APPEND EKF_SRCS
height_control.cpp
imu_down_sampler.cpp
output_predictor.cpp
vel_pos_fusion.cpp
velocity_fusion.cpp
position_fusion.cpp
yaw_fusion.cpp
zero_innovation_heading_update.cpp
+2 -2
View File
@@ -67,11 +67,11 @@ public:
void setTrueAirspeed(float true_airspeed) { _true_airspeed = true_airspeed; }
void setGyroBias(const Vector3f &imu_gyro_bias)
void setGyroBias(const Vector3f &imu_gyro_bias, const bool force = false)
{
// Initialise to gyro bias estimate from main filter because there could be a large
// uncorrected rate gyro bias error about the gravity vector
if (!_ahrs_ekf_gsf_tilt_aligned || !_ekf_gsf_vel_fuse_started) {
if (!_ahrs_ekf_gsf_tilt_aligned || !_ekf_gsf_vel_fuse_started || force) {
// init gyro bias for each model
for (uint8_t model_index = 0; model_index < N_MODELS_EKFGSF; model_index++) {
_ahrs_ekf_gsf[model_index].gyro_bias = imu_gyro_bias;
@@ -60,22 +60,13 @@ bool ZeroGyroUpdate::update(Ekf &ekf, const estimator::imuSample &imu_delayed)
if (zero_gyro_update_data_ready) {
Vector3f gyro_bias = _zgup_delta_ang / _zgup_delta_ang_dt;
Vector3f innovation = ekf.state().gyro_bias - gyro_bias;
const float obs_var = sq(math::constrain(ekf.getGyroNoise(), 0.f, 1.f));
const Vector3f innov_var = ekf.getGyroBiasVariance() + obs_var;
for (int i = 0; i < 3; i++) {
Ekf::VectorState K; // Kalman gain vector for any single observation - sequential fusion is used.
const unsigned state_index = State::gyro_bias.idx + i;
// calculate kalman gain K = PHS, where S = 1/innovation variance
for (int row = 0; row < State::size; row++) {
K(row) = ekf.stateCovariance(row, state_index) / innov_var(i);
}
ekf.measurementUpdate(K, innov_var(i), innovation(i));
for (unsigned i = 0; i < 3; i++) {
const float innovation = ekf.state().gyro_bias(i) - gyro_bias(i);
const float innov_var = ekf.getGyroBiasVariance()(i) + obs_var;
ekf.fuseDirectStateMeasurement(innovation, innov_var, obs_var, State::gyro_bias.idx + i);
}
// Reset the integrators
@@ -66,7 +66,7 @@ bool ZeroVelocityUpdate::update(Ekf &ekf, const estimator::imuSample &imu_delaye
for (unsigned i = 0; i < 3; i++) {
const float innovation = ekf.state().vel(i) - vel_obs(i);
ekf.fuseVelPosHeight(innovation, innov_var(i), State::vel.idx + i);
ekf.fuseDirectStateMeasurement(innovation, innov_var(i), obs_var, State::vel.idx + i);
}
_time_last_zero_velocity_fuse = imu_delayed.time_us;
+23 -9
View File
@@ -93,7 +93,7 @@ void Ekf::controlAirDataFusion(const imuSample &imu_delayed)
const bool is_airspeed_significant = airspeed_sample.true_airspeed > _params.arsp_thr;
const bool is_airspeed_consistent = (_aid_src_airspeed.test_ratio > 0.f && _aid_src_airspeed.test_ratio < 1.f);
const bool starting_conditions_passing = continuing_conditions_passing && is_airspeed_significant
&& (is_airspeed_consistent || !_control_status.flags.wind); // if wind isn't already estimated, the states are reset when starting airspeed fusion
&& (is_airspeed_consistent || !_control_status.flags.wind || _control_status.flags.inertial_dead_reckoning);
if (_control_status.flags.fuse_aspd) {
if (continuing_conditions_passing) {
@@ -118,17 +118,16 @@ void Ekf::controlAirDataFusion(const imuSample &imu_delayed)
} else if (starting_conditions_passing) {
ECL_INFO("starting airspeed fusion");
// If starting wind state estimation, reset the wind states and covariances before fusing any data
// Also catch the case where sideslip fusion enabled wind estimation recently and didn't converge yet.
const Vector2f wind_var_xy = getWindVelocityVariance();
if (_control_status.flags.inertial_dead_reckoning && !is_airspeed_consistent) {
resetVelUsingAirspeed(airspeed_sample);
if (!_control_status.flags.wind || (wind_var_xy(0) + wind_var_xy(1) > sq(_params.initial_wind_uncertainty))) {
// activate the wind states
_control_status.flags.wind = true;
// reset the wind speed states and corresponding covariances
} else if (!_control_status.flags.wind || getWindVelocityVariance().longerThan(_params.initial_wind_uncertainty)) {
// If starting wind state estimation, reset the wind states and covariances before fusing any data
// Also catch the case where sideslip fusion enabled wind estimation recently and didn't converge yet.
resetWindUsingAirspeed(airspeed_sample);
}
_control_status.flags.wind = true;
_control_status.flags.fuse_aspd = true;
}
@@ -208,7 +207,7 @@ void Ekf::fuseAirspeed(const airspeedSample &airspeed_sample, estimator_aid_sour
K.slice<State::wind_vel.dof, 1>(State::wind_vel.idx, 0) = K_wind;
}
const bool is_fused = measurementUpdate(K, aid_src.innovation_variance, aid_src.innovation);
const bool is_fused = measurementUpdate(K, H, aid_src.observation_variance, aid_src.innovation);
aid_src.fused = is_fused;
_fault_status.flags.bad_airspeed = !is_fused;
@@ -247,3 +246,18 @@ void Ekf::resetWindUsingAirspeed(const airspeedSample &airspeed_sample)
_aid_src_airspeed.time_last_fuse = _time_delayed_us;
}
void Ekf::resetVelUsingAirspeed(const airspeedSample &airspeed_sample)
{
const float euler_yaw = getEulerYaw(_R_to_earth);
// Estimate velocity using zero sideslip assumption and airspeed measurement
Vector2f horizontal_velocity;
horizontal_velocity(0) = _state.wind_vel(0) + airspeed_sample.true_airspeed * cosf(euler_yaw);
horizontal_velocity(1) = _state.wind_vel(1) + airspeed_sample.true_airspeed * sinf(euler_yaw);
float vel_var = NAN; // Do not reset the velocity variance as wind variance estimate is most likely not correct
resetHorizontalVelocityTo(horizontal_velocity, vel_var);
_aid_src_airspeed.time_last_fuse = _time_delayed_us;
}
+2 -2
View File
@@ -42,10 +42,10 @@ void Ekf::controlAuxVelFusion()
resetEstimatorAidStatus(_aid_src_aux_vel);
updateVelocityAidSrcStatus(auxvel_sample_delayed.time_us, auxvel_sample_delayed.vel, auxvel_sample_delayed.velVar, fmaxf(_params.auxvel_gate, 1.f), _aid_src_aux_vel);
updateHorizontalVelocityAidSrcStatus(auxvel_sample_delayed.time_us, auxvel_sample_delayed.vel, auxvel_sample_delayed.velVar, fmaxf(_params.auxvel_gate, 1.f), _aid_src_aux_vel);
if (isHorizontalAidingActive()) {
fuseVelocity(_aid_src_aux_vel);
fuseHorizontalVelocity(_aid_src_aux_vel);
}
}
}

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