Commit Graph
1354 Commits
Author SHA1 Message Date
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 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
EikeandDaniel Agar 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
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
Paul Riseborough b3c1bd6d40 EKF: Remove un-used code 2021-03-09 21:23:38 +11:00
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 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 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
Paul Riseborough 9c89fa3b29 EKF: Use IMU clipping to adjudicate bad accel data check 2021-02-09 19:55:32 +11:00
bresch cd38621dd6 flow terrain: use dedicated variable for last fusion time
This avoids confusion with the flow "for velocity" fusion in the main
EKF
2021-02-08 23:26:33 -05:00
bresch 5aaa6c6dde lpos accuracy: bump variance if deadreckon time exceeded 2021-02-08 09:01:51 -05:00
Paul Riseborough b919f3ddf4 EKF: Restore protection from extreme innovation values 2021-01-21 20:55:42 +11:00
Paul Riseborough efb78deef9 EKF: Set position fusion gate option false by default 2021-01-21 20:55:42 +11:00
Paul Riseborough 556a195320 EKF: Improve handling of non position mode large position innovations
These changes fix a bug that allowed IMU gyro errors that cause large tilt errors prior to start of aiding not resulting in large innovation test ratios.
2021-01-21 20:55:42 +11:00
Paul Riseborough 99575d73e1 EKF: Add bad accel bias checking for EV and range finder height use cases 2021-01-09 11:03:31 -05:00
Paul Riseborough ff3c0a6136 EKF: Fix bug preventing recovery from bad delta velocity bias estimates 2021-01-09 11:03:31 -05:00
Paul Riseborough dd259a288f EKF: Don't modify accel bias states and variances when inhibited 2021-01-09 11:03:31 -05:00
Paul Riseborough 3e1f2d8674 EKF: Set dvel bias variance to stored value when state is inactive 2021-01-09 11:03:31 -05:00
bresch c212975abe rng height: reset to baro using common logic
The failsafe from rng height to baro height should occur after a reset
to baro triggered by the controlHeightSensorTimeouts function and not in
the fusion selector.

Until now, the EKF was fusing baro measurements between rng updates if
the range finder ODR was slower than the EKF update rate. This is not
the case anymore as the height reset occurs after 5 seconds.

The unit test has been extended to show this behavior.
2021-01-07 10:07:57 +01:00
Paul Riseborough 03fed323ab EKF: Fix formatting 2021-01-05 21:08:28 +11:00
Paul Riseborough 31fca9c31d EKF: Update GPS loss message 2021-01-05 21:08:28 +11:00
Paul Riseborough c65cf13bb8 EKF; Treat combined sideslip and airspeed as a horizontal aiding source 2021-01-05 21:08:28 +11:00