Commit Graph

41 Commits

Author SHA1 Message Date
Peter Hall 47e3fda8e9 AP_NavEKF3: add initalized flag and change to uint32_t 2020-02-19 06:45:07 +11:00
Andrew Tridgell 04944fa6ce AP_NavEKF3: review fixes
thanks Paul!
2019-07-29 10:08:22 +10:00
Andrew Tridgell 451fe840ee AP_NavEKF3: ensure that EKF origin stays in sync on all cores
this prevents the EKF origin on different cores from being initialised
to different values. A common value is stored in the frontend and used
by a core if it doesn't have an origin
2019-07-29 10:08:22 +10:00
Andrew Tridgell 0fcb2037e1 AP_NavEKF3: use origin lat for earth rates
home may not yet be set when this code is run, so using home may be
invalid
2019-07-29 10:08:22 +10:00
priseborough 122f214416 AP_NavEKF3: Don't allow mag to interfere with use of external yaw sensor 2019-07-13 11:05:57 +10:00
priseborough 0c4f92d4c1 AP_NavEKF3: Add control logic to use external yaw sensor 2019-07-13 11:05:57 +10:00
Michael du Breuil be74b631fe AP_NavEKF3: Fix AP_GPS.h include 2019-06-18 10:02:05 +10:00
Paul Riseborough 0d3e1a7d23 AP_NavEKF3: flow use parameter improvements 2019-04-02 10:51:12 +11:00
Paul Riseborough b848e231c7 AP_NavEKF3: Add parameter to control how optical flow data is used 2019-04-02 10:51:12 +11:00
Arjun Vinod f382a657bd AP_NavEKF3: fixed typos 2019-02-26 08:33:39 +11:00
Tom Pittenger 55377b234f AP_NavEKF3: remove HAL_CPU_CLASS_150 check, 150 is already a minimum requirement 2019-02-17 13:00:00 -08:00
Peter Barker b68a91d171 AP_NavEKF3: remove default clause in setAidingMode
All aiding modes should be covered in the switch statement; adding the
default clause squelches a potentially useful compiler warning
2018-10-03 17:49:43 +01:00
Andrew Tridgell ac40a20c02 AP_NavEKF3: fill in gps_quality_good flag 2018-07-14 17:49:52 +10:00
Pierre Kancir 2b2c1e2d78 AP_NavEKF3: only use bcn EKF is the alignement as been completed 2018-04-03 09:55:13 +09:00
Pierre Kancir 4d2f2a2aad AP_NavEKF3: correct flag in case of GPS disable 2018-04-03 09:54:41 +09:00
priseborough 5785523a0d AP_NavEKF3: Clarify definition for gps_glitching flag 2018-03-27 20:28:56 +09:00
Tatsuya Yamaguchi aef9fa4a63 AP_NavEKF3: delete \n from the log using gcs().send_text 2018-02-02 09:13:54 +09:00
murata 6a87840c7a AP_NavEKF3: Change the if statement to a switch statement. 2018-01-28 22:20:08 +00:00
Peter Barker 5dc714bf5f AP_NavEKF3: use GPS singleton 2017-12-27 00:58:02 +00:00
priseborough c7f6d52065 AP_NavEKF3: Add wheel encoder odometry
Uses the existing body frame odometry observation model.
Handles each sensored wheel as a separate sensor.
2017-07-27 16:52:27 +09:00
priseborough 58d58b4eac AP_NavEKF3: Initialise EKF origin height to field elevation
Enables copters to set bit position 2 in the EK3_OGN_HGT_MASK parameter without having a large jump in reported local position height.
2017-07-17 02:22:02 +01:00
Peter Barker 93e09c51d3 AP_NavEKF3: eliminate GCS_MAVLINK::send_statustext_all 2017-07-11 23:53:53 +01:00
priseborough 368983ed5a AP_NavEKF3: Clean up aiding mode logic using switch statements 2017-06-23 00:43:58 +01:00
priseborough f38fccd57c AP_NavEKF3: Prevent possible race condition re-zeroing state variances 2017-06-14 12:44:41 +01:00
priseborough 5058405f8c AP_NavEKF3: add gyro bias state inhibit and rework index limit calculation
Inhibiting gyro bias estimation during the initial tilt alignment speeds alignment.
The calculation of the maxmum state index required has been modified so that it can handle all combinations of inhibited states.
Limiting the maximum state index accessed by all EKF operations result in significant processing reductions when higher index states are not being used.
2017-06-14 12:44:41 +01:00
priseborough 9da3caca47 AP_NavEKF3: Improve GPS reference height estimator
Fix rounding error bug preventing state from updating after initial convergence.
Decouple GPS reference height from published EKf origin height.
Add bitmask parameter to control update and publishing of GPS reference height.
2017-06-14 12:44:41 +01:00
murata 46cba2c970 libraries: Delete the setting value for specific editor. 2017-05-11 13:18:41 -07:00
Randy Mackay b255c7b370 AP_NavEKF: add setOrigin 2017-04-22 10:37:31 +09:00
priseborough fb7104f4e3 AP_NavEKF3: add fusion method for body frame odometry data 2017-04-19 11:04:40 +09:00
priseborough 06c073e448 AP_NavEKF3: Update tilt alignment check 2017-04-05 20:16:16 +10:00
priseborough 7a8783f35e AP_NavEKF3: Fix bug preventing reset to GPS
This fixes a bug that prevented the reset to the GPS position occurring if GPS velocity observations were still passing innovation consistency checks.
2017-03-06 17:11:39 +11:00
priseborough de7a679534 AP_NavEKF3: Enable simple heading fusion to be set for specific cores 2017-02-15 19:09:45 +00:00
priseborough ccb952ba31 AP_NavEKF3: Use the same mag fusion method for all cores
The original reason for using a different method for the second core is no longer valid.
2017-02-15 19:01:10 +00:00
priseborough a133d55b6d AP_NavEKF3: Allow copters to fly with magnetometers disabled
Copter operation without a magnetometer is limited to constant position and relative position modes only (no GPS or range beacon fusion permitted)
Copter optical flow operation without a magnetometer is permitted.
The ability of planes to takeoff/launch without a magnetometer and align the yaw using the GPS velocity is retained.
2017-01-27 16:57:42 +09:00
priseborough 2e5ac40ef6 AP_NavEKF3: remove unnecessary stdio includes 2017-01-27 16:57:42 +09:00
priseborough 7c53573a0c AP_NavEKF3: Allow range beacon use with intermittent GPS 2017-01-27 16:57:42 +09:00
priseborough e5e4883c72 AP_NavEKF3: Fix GPS use inhibit interface documentation 2017-01-27 16:57:42 +09:00
priseborough c7e1828238 AP_NavEKF3: improve variable name 2017-01-27 16:57:42 +09:00
priseborough 71eb46dd04 AP_NavEKF3: Fix bug in loss of aiding fallback
Fixes a bug introduced by the introduction of range beacon fusion to the fallback test.
2016-12-21 18:08:39 +11:00
priseborough f1c05ee320 AP_NavEKF3: Allow accel switch on bias uncertainty to be adjusted 2016-12-19 08:07:15 +11:00
priseborough 39969e7d8e AP_NavEKF3: added EKF3 for EKF experimentation
AP_NavEKF3: Implement same maths as PX4/ecl EKF

Replace attitude vector states with quaternions
Remove gyro scale factor states
Add XY accel delta velocity bias estimation
Initial tuning
Add GPS body frame offset compensation

AP_NavEKF3: Fix bugs and consolidate aiding switch logic

Switching in and out of aiding modes was being performed in more than one place and was using two variables.
The reversion out of GPS mode due to prolonged loss of GPS was not working.
This consolidates the logic and ensures that PV_AidingMode is only changed by the setAidingMode function.

AP_NavEKF3: prevent multiple fusion mode changes per filter update

AP_NavEKF3: Update tuning defaults

AP_NavEKF3: Fix bug causing switching in and out of aiding
If the GPS receiver was disconnected and no data received, then then the gpsGoodToAlign check did not get a chance to run and becasue it was previously true the EKF would switch back into aiding.
This prevents this by ensuring that gpsGoodToAlign defaults to false when the check is not being performed.
An additional check has also been dded to ensure that there is GPS data to fuse before we declare ready to use GPS.

AP_NavEKF3: Fix bug preventing planes recovering from bad magnetometers
This bug created a race condition whereby if the EKF had to reset the yaw to the GPS ground course to recover from a bad magnetometer, the new heading could be over-written by the bad magnetic heading when the plane reached the height for the scheduled reset.

AP_NavEKF3: Improve switch-over to backup magnetometer
When switching over to a back up magnetometer, ensure that the earth field estimate are reset. Otherwise mag earth field estimates due to the previous failed mag could cause data from the new mag to be rejected.

AP_NavEKF3: enable automatic use of range finder height

AP_NavEKF3: Fix bug in handling of invalid range data

AP_NavEKF3: Fix height drift on ground using range finder without GPSAP_NavEKF3:

AP_NavEKF3: Handle yaw jumps due to core switches

AP_NavEKF3: Enable simultaneous GPS and optical flow use

AP_NavEKF3: fix console status reporting

AP_NavEKF3: send messages to mavlink instead of console

This allows the GCS to better handle the display of messages to the user.

AP_NavEKF3: replace deprecated function call

AP_NavEKF3: Compensate for sensor body frame offsets

AP_NavEKF3: Fix bug in median filter code

AP_NavEKF3: save some memory in the position offsets in EKF3

We don't need to copy that vector3f for every sample. A uint8_t does the job

AP_NavEKF3: Add fusion of range beacon data

AP_NavEKF3: Bring up to date with EKF2

AP_NavEKF3: Misc range beacon updates

AP_NavEKF3: Add mising accessors

AP_NavEKF3: remove duplicate include

AP_NavEKF3: Prevent NaN's when accessing range beacon debug data

AP_NavEKF3: Update range beacon naming

AP_NavEKF3: updates

AP_NavEKF3: miscellaneous changes

AP_NavEKF3: misc updates

AP_NavEKF3: misc range beacons updates

AP_NavEKF3: add missing rover default param
2016-12-19 08:06:47 +11:00