Commit Graph

38 Commits

Author SHA1 Message Date
Daniel Magree b3ff81648b Nav_EKF3: varInnovBodyVel assigned the innovation covariance, rather than inverse 2020-03-25 21:52:49 +11:00
Andrew Tridgell 772438f3ed AP_NavEKF3: fixed use of antenna position when switching GPS primary
when GPS primary switches we were using a position which had not been
corrected for antenna offset. This was used for calculating the reset
for sensor change.

This fixes that (trivial fix) and also fixes a similar issue on
position reset
2020-02-19 18:12:54 +11:00
Peter Barker 4431d01230 AP_NavEKF3: stop relying on the presence of a RangeFinder 2019-12-11 08:09:01 +11:00
Peter Barker fe8599d6d7 AP_NavEKF3: adjust for renaming of RangeFinder files 2019-11-12 07:14:37 +08:00
Paul Riseborough 5b1d9ed868 AP_NavEKF3: Add missing vertical position derivative calculation 2019-10-18 11:15:25 +09:00
Randy Mackay 0e1a2efb7c EKF3: RNG_USE_HGT param only used when ALT_SOURCE = rangefinder 2019-09-10 18:44:52 +10:00
Andrew Tridgell fc65e04ef2 AP_NavEKF3: fixed baro innovation gate when on ground with AIDING_NONE
when on the ground without a position source we would disable the
innovation gate for the barometer. This meant that a single (or small
number of) really bad baro readings would be fused into the EKF,
causing it to destabilise

Fixes #11903
2019-07-30 08:23:21 +10:00
Andrew Tridgell 634db441f8 AP_NavEKF3: origin handling fixes from Francisco 2019-07-11 06:40:55 +10:00
Andrew Tridgell 92783bccfa AP_NavEKF3: don't allow height datum reset when not on ground 2019-07-07 19:20:32 +10:00
Andrew Tridgell 3f9e48951b AP_NavEKF3: set terrainState to zero on height datum reset 2019-07-07 19:20:32 +10:00
Andrew Tridgell f3fc910abe AP_NavEKF3: continuously update gpsGoodToAlign
use it to determine how to handle a height datum reset
2019-07-07 19:20:32 +10:00
Andrew Tridgell b9a5794671 AP_NavEKF3: ensure that both AMSL and relative alt are correct after a reset
this forces the EKF origin to the GPS alt on a height datum reset if
we have GPS lock. If we don't do this then the reported AMSL alt will
drift over time away from the GPS alt when we reset while on the
ground
2019-07-07 19:20:32 +10:00
Michael du Breuil b624f6f008 AP_NavEKF3: Reduce scope of AP_Baro.h 2019-06-27 14:56:21 +10:00
Michael du Breuil be74b631fe AP_NavEKF3: Fix AP_GPS.h include 2019-06-18 10:02:05 +10:00
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 7b1a906c4e AP_NavEKF3: use baro singleton 2018-03-08 21:20:05 -08:00
Peter Barker 5dc714bf5f AP_NavEKF3: use GPS singleton 2017-12-27 00:58:02 +00:00
priseborough c96bc54254 AP_NavEKF3: correctly use wheel odometry speed for pitched rovers 2017-10-31 08:11:05 +09:00
priseborough ee6b43aabf AP_NavEKF3: Fix bugs in use of wheel encoder data
Found by pavloblindnology
2017-10-28 10:58:01 +09:00
Peter Barker 63440800fc AP_NavEKF3: use rangefinder backend accessors 2017-08-15 18:30:45 +01:00
priseborough 2310cb6d19 AP_NavEKF3: Enable external control over use of GPS vertical velocity 2017-08-10 19:49:45 +10:00
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 08a3f55c90 AP_NavEKF3: Fix error in scaling of observation error 2017-07-27 16:52:25 +09:00
Peter Barker 93e09c51d3 AP_NavEKF3: eliminate GCS_MAVLINK::send_statustext_all 2017-07-11 23:53:53 +01:00
priseborough a1c117360c AP_NavEKF3: Ensure Kalman gain calculatons respect deactivated states
All Kalman gain calculations now explicity set gains for deactivated states to zero.
Previous use of loops to set gains to zero have been replaced with more efficient memset operations.
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
priseborough fb7104f4e3 AP_NavEKF3: add fusion method for body frame odometry data 2017-04-19 11:04:40 +09:00
Jonathan Challinger c7a73e84d6 AP_NavEKF3: apply height innovation floor only when barometer is in use 2017-03-24 14:42:36 -07:00
priseborough 01551a4423 AP_NavEKF3: handle position jump caused by change in GPS receiver
If the GPS receiver selection changes and we are using GPS for height, the vertical position will be reset to the new GPS height measurement.
correct output observer history when doing a GPS height reset
2017-03-13 11:31:51 +11:00
Randy Mackay 3f6a734a71 AP_NavEKF3: only use downward facing rangefinder 2017-02-27 15:18:11 +09:00
priseborough 2e5ac40ef6 AP_NavEKF3: remove unnecessary stdio includes 2017-01-27 16:57:42 +09:00
priseborough 8688d1ddac AP_NavEKF3: Improve range finder selection logic
Fixes bug that could leave it locked out of range finder use.
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
Dr.-Ing. Amilcar Do Carmo Lucas d408d25f92 More spelling stuff 2017-01-06 10:57:39 -08:00
priseborough cd6fd0ea45 AP_NavEKF3: Improvements to range finder selection logic
Enables the horizontal speed at which we switch from range finder to alternate to be adjusted.
Does not switch from range finder to alternate based on speed when speed estimate is invalid.
2016-12-19 08:07:14 +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