Commit Graph

100 Commits

Author SHA1 Message Date
priseborough
3772fd68da AP_NavEKF3: Fix bug in wheel odometry timestamp correction 2017-08-02 12:49:09 +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
cbe8f97489 AP_NavEKF3: rename struct used for velocity odometry observations
Do this so we can add other odometry observation types.
2017-07-27 16:52:26 +09:00
priseborough
08a3f55c90 AP_NavEKF3: Fix error in scaling of observation error 2017-07-27 16:52:25 +09:00
priseborough
593437ca95 AP_NavEKF3: Add tuning of visual odometry observation error
Also adjust default values based on replay analysis.
2017-07-27 16:52:25 +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
priseborough
0827b13feb AP_NavEKF3: Fix default behaviour for height origin corrections
Previous default was to apply in-flight height origin changes to local position instead of to reported origin height. This caused problems with copters that took off before getting GPS lock.
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
Randy Mackay
d64b2fcbf0 AP_NavEKF3: final mag reset at 2.5m 2017-07-08 08:39:43 +09:00
priseborough
9d0fa09d39 AP_NavEKF3: Fix calculation of predicted LOS rate in terrain estimator 2017-06-26 14:58:06 +01:00
priseborough
a4d18696a7 AP_NavEKF3: Improve variable names and documentation
Also remove unnecessary calculation of innov * gain
2017-06-23 00:43:58 +01:00
priseborough
368983ed5a AP_NavEKF3: Clean up aiding mode logic using switch statements 2017-06-23 00:43:58 +01:00
priseborough
2a9eceaf10 AP_NavEKF3: Fix bugs causing height drift when using range beacons 2017-06-23 00:43:58 +01:00
priseborough
7659e9c31f AP_NavEKF3: Improve checking of time delay validity when setting buffers
This change means that provided the GPS_DELAY_MS parameters are set for each GPS receiver attached, the EKF will not have to wait for the configuration of each receiver to be determined before it can start.
This significantly reduces start-up times when the delay parameters are set.
2017-06-21 11:44:45 +01:00
priseborough
7d63286088 AP_NavEKF3: update to match AP_GPS interface change 2017-06-21 11:44:45 +01:00
priseborough
06d40a7901 AP_NavEKF3: Fix terrain estimator innovation consistency check 2017-06-20 02:08:56 +01:00
priseborough
284fc0f3c5 AP_NavEKF3: Fix bug in flow fusion for terrain estimation
Also remove unused class variables
2017-06-20 02:08:56 +01:00
Andrew Tridgell
a1508b58c1 AP_NavEKF3: use AHRS likely flying state
this sets inFlight when AHRS has indicated flying for 5s
2017-06-20 09:44:44 +10:00
priseborough
edee8396ba AP_NavEKF3: Improve in-flight check for non fly forward vehicles
This will enable the EK3_MAG_TYPE 0 option to be used for multirotors
2017-06-19 06:09:07 +10:00
Dr.-Ing. Amilcar Do Carmo Lucas
6a01c65197 AP_NavEKF3: Fix long description of EK3_OGN_HGT_MASK parameter (NFC) 2017-06-16 12:05:20 +01:00
priseborough
49ec2b4032 AP_NavEKF3: Change default value of EK3_OGN_HGT_MASK
Turn off by default.
Update parameter description.
2017-06-14 12:44:41 +01:00
priseborough
6d14cf0ab8 AP_NavEKF3: Ensure reported local height = global height - origin height 2017-06-14 12:44:41 +01:00
priseborough
3ae7998f51 AP_NavEKF3: Allow reporting of origin height for specified instance 2017-06-14 12:44:41 +01:00
priseborough
e58ba8044d AP_NavEKF3: Improve protection for badly conditioned dVel bias covariances
If variance falls below desired minimum, set state noise to a larger value.
If variance drops below safe value, set to desired minimum and reset off-diagonals to zero.
2017-06-14 12:44:41 +01:00
priseborough
bf963f8b65 AP_NavEKF3: Raise lower limit on del vel bias state variances
This is required to prevent co-variance matrix errors due to long periods without movement causing height divergence.
2017-06-14 12:44:41 +01:00
priseborough
628d140319 AP_NavEKF3: Make target covariance time step larger
The target covariance time step has been increased from 10 to 12 msec to improve conditioning of the covariance prediction calculation.
2017-06-14 12:44:41 +01:00
priseborough
2b97d0f5c9 AP_NavEKF3: Add public accessor for state variances 2017-06-14 12:44:41 +01:00
priseborough
9f97cbfc3b AP_NavEKF3: Revert auto-code to original form and remove micro optimisations
To eliminate the possibility of editing errors, revert the covariance prediction auto-code to the original auto-code without the replacement fo the /2 and /4 operations. The compiler optimisations are able to correctly handle the /2 and /4 operations.

Also use local variables for intermediate covariance calculations. The use of class variables for these small arrays was unnecessary.
2017-06-14 12:44:41 +01:00
priseborough
f38fccd57c AP_NavEKF3: Prevent possible race condition re-zeroing state variances 2017-06-14 12:44:41 +01:00
priseborough
7adaea6019 AP_NavEKF3: Improve partitioning and efficiency of the covariance prediction
This patch ensures that covariance matrix entries for inactive states are always set to zero.
It also halves the number of copy operations from the updated to stored matrix.
2017-06-14 12:44:41 +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
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
0cba133a1e AP_NavEKF3: Fix initialisation of state inhibit flags 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
Dr.-Ing. Amilcar Do Carmo Lucas
c1eb9fb9c3 AP_NavEKF3: Spell in comments 2017-05-18 09:29:55 +09:00
Dr.-Ing. Amilcar Do Carmo Lucas
d3a57b5965 AP_NavEKF3: Use SI units conventions in parameter units
Follow the rules from:
http://physics.nist.gov/cuu/Units/units.html
http://physics.nist.gov/cuu/Units/outside.html
and
http://physics.nist.gov/cuu/Units/checklist.html
one further constrain is that only printable (7bit) ASCII characters are allowed
2017-05-17 18:07:25 +10:00
Dr.-Ing. Amilcar Do Carmo Lucas
9cb068d3f4 AP_NavEKF3: Spell in coments 2017-05-16 20:29:16 +09:00
murata
46cba2c970 libraries: Delete the setting value for specific editor. 2017-05-11 13:18:41 -07:00
Dr.-Ing. Amilcar Do Carmo Lucas
23b7f1e645 AP_NavEKF3: Improve comments, typos 2017-05-03 08:45:01 +09:00
priseborough
4a898037e9 AP_NavEKF3: documentation update 2017-05-01 14:24:55 +10:00
Andrew Tridgell
a04aff7a7d AP_NavEKF3: added inter-EKF scheduling cooperation
this changes the stragegy for load levelling between EKF cores so it
works between EK2 and EK3, and with future estimators as well.

It allows us to run EK3 and EK2 at the same time with good scheduling
performance
2017-05-01 14:24:55 +10:00
priseborough
0bf50fd56f AP_NavEKF3: Add monitoring of average EKF time step 2017-04-29 11:03:44 +10:00
priseborough
3ce81967ae AP_NavEKF3: Improve calculation and use of average EKF time step 2017-04-29 11:03:44 +10:00
priseborough
7abf9997e6 AP_NavEKF3: Correctly initialise dtIMUavg time step and apply LPF 2017-04-29 11:03:44 +10:00
priseborough
1301b9797a AP_NavEKF3: Fix solution validity reporting bug
Fixes bug that causes relative position status to report as false when using optical flow and using range finder as the primary height sensor.
2017-04-28 17:19:23 +01:00
Andrew Tridgell
adb281cd4e AP_NavEKF3: added timing statistics logging 2017-04-28 17:19:39 +10:00
priseborough
f208986d43 AP_NavEKF3: Reset covariance if bad mag fusion update 2017-04-27 20:14:21 +10:00
Andrew Tridgell
18b66f9eed AP_NavEKF3: fixed reset of coviariance matrix 2017-04-27 18:33:25 +10:00
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