Commit Graph

1782 Commits

Author SHA1 Message Date
bresch a4fe2b1e72 yaw_align: let the mag control logic do the alignement and resets 2021-05-12 08:33:07 +10:00
bresch 2cc023038b mag control: select mag mode before doing the reset 2021-05-12 08:33:07 +10:00
bresch fe943cf104 mag reset: force align in MC custom mode (aka. indoor mode)
Checking the parameter is enough to decide if we want to force the yaw
alignment or not
2021-05-12 08:33:07 +10:00
bresch cadcc58415 mag reset: do not stop the fusion from inside the reset function
The start/stop is already handled in the dedicated mag control logic
The early return is not required as this case is handled just below
2021-05-12 08:33:07 +10:00
bresch 6248646bff EV yaw: move EV yaw reset out of resetMagHeading function
Also remove the unnecessary 2nd "manual reset" done in the start function
2021-05-12 08:33:07 +10:00
bresch 48722a2a92 control: inhibit EV yaw from restarting when GPS aid wants to start 2021-05-12 08:33:07 +10:00
bresch a685987082 GNSS yaw: unset yaw_align if fusion stops before takeoff
We do not want to rely on a potentially badly initialized heading as it
could lead to a flyaway directly after takeoff

Also remove the resetMagHeading() call from the GPS fusion control logic
as this is properly handled in mag_control.
2021-05-12 08:33:07 +10:00
bresch 7ee69706e8 GNSS yaw: add test case when measurement jumps 2021-05-12 08:33:07 +10:00
bresch 7a11871566 GNSS yaw tests: adjust timing
the starting condition needs more than 1 sample to determine if the data
comes regularly

the timeout on "no data" is defined by the fusion reset timeout
parameter (7 seconds)
2021-05-12 08:33:07 +10:00
bresch 51197a5d82 GNSS yaw selection logic refactor 2021-05-12 08:33:07 +10:00
bresch 29243ac5cb yaw_reset: reduce minimum vector length to compute yaw error
A value of 1m/s was too conservative and the EKF takes too much time to
trigger a yaw reset. The value can be safely reduced because the
threshold is computed using the accuracy of the measurement and estimate
before being limited by this value.
2021-05-06 19:13:54 +10:00
Kabir Mohammed aad48407c2 EKF: increase allowed difference between flow and gyro ODRs
In the normal and lowlight mode for the PAW3902/3 sensor, the ODR is 66Hz, while in super lowlight mode it is 50Hz.

The IMU ODR vs flow ODR mismatch threshold was too conservative for the 66Hz ODR, since https://github.com/PX4/PX4-ECL/pull/928. The EKF would keep waiting for the data to line up and never fuse measurements.
2021-05-03 11:08:16 +02:00
Eike a7b8afe420 Allow rangefinder fusion in vision height mode (Fix for #994) (#999)
Co-authored-by: Daniel Agar <daniel@agar.ca>
2021-04-30 14:17:39 -04:00
Daniel Agar 4ac57d3bde EKF: increase fault flags value size to fit current flag bits (> 16) 2021-04-25 17:05:09 -04:00
Eike 5d34d7a24e Height source vision: Fallback to rangefinder if available (#994) 2021-03-31 14:24:38 +02:00
PX4BuildBot da06f25216 [AUTO COMMIT] update change indication 2021-03-28 21:22:25 -04:00
PX4 BuildBot 85fcf9393d Update geo_lookup WMM to latest Sun Mar 28 11:48:06 UTC 2021 2021-03-28 21:22:25 -04:00
bresch 6f2dec726a gps sacc: apply same minimum for EKF2 and yaw estimator 2021-03-25 09:54:30 +01:00
Daniel Agar e3d1ade660 EKF: use flow for vel test ratio if only active source of horizontal aiding 2021-03-23 15:56:22 +01:00
Morten Fyhn Amundsen bb950a1550 Expose terrain vpos reset counter 2021-03-18 14:25:07 +01:00
Morten Fyhn Amundsen ab69681744 Add parameter for terrain timeout 2021-03-18 14:25:07 +01:00
Daniel Agar 4df0054873 geo: purge old globallocal_converter 2021-03-15 14:43:53 -04:00
Paul Riseborough b3c1bd6d40 EKF: Remove un-used code 2021-03-09 21:23:38 +11:00
Paul Riseborough 4bad2a272c EKF: Use debug prints for NuttX builds 2021-03-05 19:06:59 -05:00
Daniel Agar 0f47cae1e1 remove ECL_{INFO,WARN,ERN}_TIMESTAMPED macros
- we already have mechanisms to print these messages timestamped
2021-03-05 19:06:59 -05:00
Paul Riseborough c1f1415696 EKF: Add usage warning comment 2021-03-05 19:06:59 -05:00
Paul Riseborough c2b86cdb20 EKF: Provide external reset of event records 2021-03-05 19:06:59 -05:00
Paul Riseborough 9d51ab079a EKF: Remove duplicated event recording 2021-03-05 19:06:59 -05:00
Paul Riseborough 140ca3f48f EKF: Add external monitoring of warning and information events 2021-03-05 19:06:59 -05:00
Paul Riseborough 90a445ddbc EKF: upgrade some events from into to warning status 2021-03-05 19:06:59 -05:00
bresch cb8367026c [AUTO COMMIT] update change indication 2021-03-04 19:43:01 +11:00
bresch 93dd4e5754 fix unit tests 2021-03-04 19:43:01 +11:00
bresch 5d441d65e1 Accelerate tilt fine alignment by reducing obs noise when at rest
Fine tilt alignment is accomplished by fusing fake position data after
a coarse tilt leveling. The observation noise can be reduced if the
vehicle is at rest to speed up the process.
2021-03-04 19:43:01 +11:00
Daniel Agar 098d5ce5c0 EKF allow range aid without horizontal aiding
- skip range aid velocity check when horizontal aiding isn't active
2021-02-22 11:55:56 -05:00
Nicolas MARTIN 29943a2c09 EKF test ratio status return current height source test ratio 2021-02-22 09:22:45 -05:00
mcsauder 164e53bad3 Add unit tests and update ekf_helper setEkfGlobalOrigin() method to allow for condition when current position is unitialized. 2021-02-19 08:59:47 -05:00
Daniel Agar 63f64b57c1 EKF: set global origin method
EKF: add convergence after global origin reset test
2021-02-19 08:59:47 -05:00
bresch 81937370ac [AUTO COMMIT] update change indication 2021-02-18 10:11:51 +01:00
bresch 04844a04ed ekf control: move time_last_in_air/on_ground out of GPS control logic 2021-02-18 10:11:51 +01:00
bresch b00d4a9237 mag fusion: improve on ground forced mag fusion logic
While a yaw test ration > 1 rejects the mag data in air, the fusion is
forced with a limited innovation on ground to fix gyro bias and local
magnetic effects problems pre-takeoff. However, the same logic is
applied after landing and immediately after the land detector detects
landing. In some cases, this can disturb the other EKF states which can
lead to a state change of the land detector.
To avoid such a loop, the start of this forced yaw fusion is delayed by
5 seconds after landing.
2021-02-18 10:11:51 +01:00
Daniel Agar 310f415175 EKF add const state reset status access 2021-02-16 10:33:43 -05:00
isidroas 0c5291d194 Heading reset to magnetometer from GPS or EV (#969) 2021-02-16 14:37:34 +01:00
Mathieu Bresciani d4258cc66d yaw emergency: check angle between vel observation and estimate (#975)
use thresholds based on state and obs variance

* [AUTO COMMIT] update change indication
2021-02-15 10:31:16 +01:00
Loic Dubois ffab483504 Waiting for the filter to be initialized to set global origin 2021-02-11 12:55:25 -05:00
Paul Riseborough 602e65146c EKF: Remove unnecessary initialisation 2021-02-09 19:55:32 +11:00
Paul Riseborough 6f664abc4a EKF: Non functional changes arising from review 2021-02-09 19:55:32 +11:00
Paul Riseborough b87778e61d EKF: Make clip detection logic easier to follow 2021-02-09 19:55:32 +11:00
Paul Riseborough 9aa8d93efc EKF: Use isRecent function 2021-02-09 19:55:32 +11:00
Paul Riseborough e948b3505f EKF: Don't reject vertical aiding data if inertial solution is bad
Also reduce clipping count threshold
2021-02-09 19:55:32 +11:00
Paul Riseborough c566318db5 EKF: misc improvements to handling of accel clipping 2021-02-09 19:55:32 +11:00