Commit Graph

732 Commits

Author SHA1 Message Date
Paul Riseborough 8038efc152 AP_NavEKF2: Flow use parameter updates 2019-04-02 10:51:12 +11:00
Paul Riseborough e2148e7e2a AP_NavEKF2: Update default plane optical flow param values
Reduce time required to form estimate of terrain offset
2019-04-02 10:51:12 +11:00
Paul Riseborough aa6eee82f4 AP_NavEKF2: Rework opt flow terrain height logic 2019-04-02 10:51:12 +11:00
Paul Riseborough 67d20f3b3c AP_NavEKF2: Update parameter description 2019-04-02 10:51:12 +11:00
Paul Riseborough 1862512c2b AP_NavEKF2: Use flow sensor for navigation with unknown platform type
This is the more common use case.
2019-04-02 10:51:12 +11:00
Paul Riseborough 921205f61c AP_NavEKF2: Minor amendments from review 2019-04-02 10:51:12 +11:00
Paul Riseborough a40208ebd4 AP_NavEKF2: Improve optical flow height estimation
Updated derivation using sequential fusion of Y and X axis data.
2019-04-02 10:51:12 +11:00
Paul Riseborough 2b8b53d6b2 AP_NavEKF2: Add parameter to control how optical flow flow data is used 2019-04-02 10:51:12 +11:00
Mark Whitehorn 6b70181837 AP_NavEKF2: add getQuaternionBodyToNED 2019-03-29 10:58:00 +11:00
Tom Pittenger 8506ae9c32 AP_NavEKF2: rename dataflash to logger 2019-03-28 16:40:57 +11:00
Dr.-Ing. Amilcar do Carmo Lucas 79ee52917f AP_NavEKF2: replace location_offset() and get_distance() function calls with Location object member function calls
This allows removing duplicated code
2019-02-28 11:44:09 +11:00
Arjun Vinod 78b165e36f AP_NavEKF2: fixed typos 2019-02-26 08:33:39 +11:00
Arjun Vinod a0e7c37f8c AP_NavEKF2: fixed typos 2019-02-22 10:21:35 +11:00
Tom Pittenger b32e8a4424 AP_NavEKF2: remove HAL_CPU_CLASS_150 check, 150 is already a minimum requirement 2019-02-17 12:59:52 -08:00
Tom Pittenger 8a6a39b590 AP_NavEKF3: unify singleton naming to _singleton and get_singleton() 2019-02-10 19:09:58 -07:00
Andrew Tridgell ccc1f906f8 AP_NavEKF2: fixed EKF compass switching
when we had 3 compasses the lack of the 'break' meant when we switched
compass in flight we would always switch back instantly to the one
that we had just rejected.
2019-02-09 13:04:52 +11:00
chobits 3766ee1b60 AP_NavEKF2: add external navigation data lag 2019-01-31 08:30:22 +09:00
Peter Barker 6fc76a32af GLOBAL: use AP::logger() and strip redundant Log_ from methods 2019-01-18 18:08:20 +11:00
Peter Barker b47733142f GLOBAL: rename DataFlash_Class to AP_Logger 2019-01-18 18:08:20 +11:00
Peter Barker ebd12b30e8 AP_NavEKF2: adjust for Location_Class and Location unification 2019-01-16 11:45:29 +11:00
Peter Barker 9be604e3ce AP_NavEKF2: adjust for location flags being moved out of union 2019-01-16 11:45:29 +11:00
Randy Mackay c616587b86 AP_NavEKF: increase ABIAS_P_NSE param doc range to 0.005 2018-12-27 14:09:53 +09:00
Pierre Kancir 49d20364cb AP_NavEKF2: pass quaternion by const reference 2018-12-20 09:05:01 +09:00
Andrew Tridgell 8ea7df3efe AP_NavEKF2: added filter reset if unhealthy for 5s and disarmed 2018-11-30 11:02:30 +11:00
Michael du Breuil 29db069c75 AP_NavEKF2: Suppress clearing non-trival type warning 2018-10-30 16:17:03 -07:00
chobitsfan 1e56ad4837 AP_NavEKF2: add external nav system to POSNE_M_NSE description 2018-10-24 19:14:54 +09:00
chobits 08b9bf4a89 AP_NavEKF2: fix extNav position noise 2018-10-24 19:14:54 +09:00
Andrew Tridgell 805647df85 AP_NavEKF2: enable use of in-flight compass learning 2018-10-24 07:25:42 +10:00
Peter Barker 1c1d651979 AP_NavEKF2: add space for null-termination
This is simply to preserve existing behaviour when snprintf starts to
null-terminate strings
2018-10-21 07:54:30 +11:00
Peter Barker 3a79ae4eca AP_NavEKF2: use union to alias array and struct access to states
This avoids creating two pointers of different types to the same memory.

Having two pointers to the same memory can lead to the compiler
optimising code such that a write to one pointer is rearranged to be
either before or after a read from the other pointer depending on which
is deemed faster - not a good outcome.
2018-10-19 08:46:43 +11:00
Peter Barker fb176b544f AP_NavEKF2: correct compilation when running MATH_CHECK_INDEXES 2018-10-19 08:46:43 +11:00
Peter Barker 889190d46e AP_NavEKF2: always set EKF control limits, even with no cores 2018-10-09 10:47:38 +11:00
Peter Barker 3774aa6619 AP_NavEKF2: remove default clause in setAidingMode
All values from the enumeration should be handled in this switch; adding
a default will hide a compiler warning which may be useful.
2018-10-03 17:49:43 +01:00
Michael du Breuil 66e9286cf6 AP_NavEKF2: Fix roundoff, and missing offset handling of getLLH 2018-09-21 00:18:49 +01:00
Peter Barker d8aa8d2b71 AP_NavEKF2: fix writeOptFlowMeas signature
const some of the vectors, stop taking references to scalars that aren't
being changed
2018-09-11 09:03:22 +10:00
Michael du Breuil ee9cc28fda AP_NavEKF2: Utilize the GPS drivers estimate for lag 2018-08-07 09:55:26 +10:00
Randy Mackay 3d72022f6e EKF: modify ALT_SOURCE param description
We regularly find users changing the ALT_SOURCE to 1 (range finder) when trying to implement terrain following which is not the correct way to do it
2018-07-18 08:31:09 +09:00
Andrew Tridgell 3d31773fb4 AP_NavEKF2: fill in gps_quality_good flag 2018-07-14 17:49:52 +10:00
Dr.-Ing. Amilcar do Carmo Lucas 59e087214f AP_NavEKF2: spell in comments (NFC) 2018-07-10 08:17:57 +09:00
Peter Barker baa818a812 AP_NavEKF2: use compass singleton for logging 2018-07-04 20:11:27 +01:00
murata a9b2b9dddf AP_NavEKF2: Delete unused definitions 2018-06-11 09:11:44 +09:00
murata 1e011c0c15 AP_NavEKF2: Clarify the message 2018-06-04 11:32:15 +09:00
Andrew Tridgell fb0deba3aa AP_NavEKF2: send airspeed variance over mavlink 2018-04-30 15:41:31 +10:00
Peter Barker 578facc9ad AP_NavEKF2: do not pass GPS into Log_Write_GPS; it uses singleton 2018-04-18 13:50:55 +09:00
Peter Barker 81044760c7 AP_NavEKF2: const accessors 2018-04-04 12:20:36 +01:00
priseborough 12fd19ea26 AP_NavEKF2: Clarify definition for gps_glitching flag 2018-03-27 20:28:57 +09:00
Paul Riseborough c680b931dc AP_NavEKF2: Enable fusion of external nav position data 2018-03-27 20:28:42 +09:00
Peter Barker 40957ec430 AP_NavEKF2: use ins singleton 2018-03-16 00:37:35 -07:00
Peter Barker 5ab89324b2 AP_NavEKF2: use baro singleton 2018-03-08 21:20:05 -08:00
Peter Barker 5b7d5a9757 AP_NavEKF2: mark getEulerAngles as const 2018-03-07 12:34:39 +00:00
Peter Barker dbe860152d AP_NavEKF2: tight types on constants
This saves ~200 bytes on at stm32 build, at the expense of people having
to watch the type carefully when increasing the values
2018-03-01 20:27:19 +09:00
Peter Barker 3a99b2bce1 AP_NavEKF: move initialisation of EKF constants into header file
Various comments where getting out of sync with one-another, and
having everything in one place lets you match values against types.
2018-03-01 20:27:19 +09:00
bugobliterator b1213a522d AP_NavEKF2: allocate NavEKF core from MEM_FAST region 2018-01-15 11:46:02 +11:00
Peter Barker 9c8466dc03 AP_NavEKF2: use GPS singleton 2017-12-27 00:58:02 +00:00
Pierre Kancir 171e80d8dc AP_NavEKF2: only report terrain estimator innovations with valid rng value 2017-12-18 22:51:46 +00:00
Andrew Tridgell 4d4e66d825 AP_NavEKF2: removed create() method for objects
See discussion here:

  https://github.com/ArduPilot/ardupilot/issues/7331

we were getting some uninitialised variables. While it only showed up in
AP_SbusOut, it means we can't be sure it won't happen on other objects,
so safest to remove the approach

Thanks to assistance from Lucas, Peter and Francisco
2017-12-14 08:12:28 +11:00
priseborough 3b32d583a9 AP_NavEKF2: Fix delta time use error 2017-12-12 11:39:38 +11:00
priseborough 440d361aff AP_NavEKF2: Limit range of delta times 2017-12-12 11:39:38 +11:00
Andrew Tridgell 97729a12f0 AP_NavEKF2: don't run IMU updates until buffer fills
this prevents us using bad initial data multiple times. It fixes a bug
where the IMU may pause during EK2 initialisation
2017-12-12 11:39:38 +11:00
Andrew Tridgell 4019a167a9 AP_NavEKF2: fixed inverted function setInhibitGpsVertVelUse() 2017-11-29 09:47:14 +09:00
Samuel Tabor 1b4705242c AP_NavEKF2: print reason for EKF2 arming failure when no GPS is available 2017-11-20 13:53:31 +09:00
priseborough efdc651d1a AP_NavEKF2: Require reboot after changing ALT_SOURCE parameter
Toggling between alt sources in flight using the parameter can have unpredictable effects due to the various height offsets and the possibility that the data source may be unavailable.
2017-10-04 00:24:15 +01:00
Lucas De Marchi 3c04f4e4d1 AP_NavEKF2: add static create method 2017-09-26 03:01:21 +01:00
Peter Barker 1e83ef3c44 AP_NavEKF2: use rangefinder backend accessors 2017-08-15 18:30:45 +01:00
priseborough f2f3067326 AP_NavEKF2: Add interface to control GPS vertical velocity use 2017-08-10 19:49:45 +10:00
Michael du Breuil dffa3d3b40 AP_NavEKF2: Fix possible compass nullptr dereference 2017-08-01 15:25:05 +01:00
priseborough ac568bae53 AP_NavEKF2: Initialise EKF origin height to field elevation
Enables copters to set bit position 2 in the EK2_OGN_HGT_MASK parameter without having a large jump in reported local position height.
2017-07-17 02:22:02 +01:00
priseborough 027552ef44 AP_NavEKF2: 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 5da3759ff4 AP_NavEKF2: eliminate GCS_MAVLINK::send_statustext_all 2017-07-11 23:53:53 +01:00
Randy Mackay 7e7f78d4b5 AP_NavEKF2: final mag reset at 2.5m 2017-07-08 08:39:43 +09:00
priseborough c69c5440a0 AP_NavEKF2: Fix calculation of predicted LOS rate in terrain estimator 2017-06-26 14:58:06 +01:00
priseborough ce8e935896 AP_NavEKF2: Fix terrain estimator innovation consistency check 2017-06-20 02:08:56 +01:00
priseborough b7e6e6f95f AP_NavEKF2: Fix bug in flow fusion for terrain estimation
Also remove unused class variables
2017-06-20 02:08:56 +01:00
Andrew Tridgell cbffc29f0b AP_NavEKF2: use AHRS likely flying state
this sets inFlight when AHRS has indicated flying for 5s
2017-06-20 09:44:44 +10:00
priseborough 647db728ce AP_NavEKF2: Improve is flying check for non fly forward vehicles
Will enable use of EK3_MAG_TYPE = 0 for coptersAP_NavEKF2:
2017-06-19 06:09:07 +10:00
Dr.-Ing. Amilcar Do Carmo Lucas 7426bdb9b7 AP_NavEKF2: Fix long description of EK2_OGN_HGT_MASK parameter 2017-06-16 12:05:20 +01:00
priseborough b42fb31d7d AP_NavEKF2: Change default value of EK2_OGN_HGT_MASK
Turn off by default.
Update parameter description
2017-06-14 12:44:41 +01:00
priseborough fd25450632 AP_NavEKF2: Ensure reported local height = global height - origin height 2017-06-14 12:44:41 +01:00
priseborough 77d21f72d4 AP_NavEKF2: Allow reporting of origin height for specified instance 2017-06-14 12:44:41 +01:00
priseborough 36e7dfb5f6 AP_NavEKF2: 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
priseborough 1985dcd366 AP_NavEKF2: Fix bug in declination fusion 2017-06-03 15:16:25 +01:00
Dr.-Ing. Amilcar Do Carmo Lucas 3f6059397c AP_NavEKF2: Add missing @RebootRequired: True 2017-05-27 01:55:55 +01:00
Dr.-Ing. Amilcar Do Carmo Lucas 38b19b9eee AP_NavEKF2: 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 ce37517268 AP_NavEKF2: Improve comments, typos 2017-05-03 08:44:49 +09:00
priseborough 2d4eee0cce AP_NavEKF2: documentation update 2017-05-01 14:24:55 +10:00
Andrew Tridgell 2de8777669 AP_NavEKF2: 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 e48f46c98b AP_NavEKF2: Add monitoring of average EKF time step 2017-04-29 11:03:44 +10:00
priseborough 082f429da3 AP_NavEKF2: 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 ee5c032f27 AP_NavEKF2: added recording of timing statistics 2017-04-28 17:19:39 +10:00
priseborough 596b20eb07 AP_NavEKF2: close perf counter when doing early return 2017-04-27 20:14:21 +10:00
priseborough 88469ce80c AP_NavEKF2: Reset covariance if bad mag fusion update 2017-04-27 20:14:21 +10:00
Andrew Tridgell d799bacd7d AP_NavEKF2: 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
Andrew Tridgell 9f3c2cb704 AP_NavEKF2: allow access to quaternion for each instance 2017-04-16 14:01:36 +10:00
Jonathan Challinger c53125f3b5 AP_NavEKF2: apply height innovation floor only when barometer is in use 2017-03-24 14:42:36 -07:00
Jacob Walser 646d68c76d AP_NavEKF2: Fix parameter metadata 2017-03-22 16:16:26 -07:00
priseborough 44fa82d58c AP_NavEKF2: Reference correct derivation 2017-03-13 11:31:51 +11:00
priseborough 407a60e599 AP_NavEKF2: log correct GPS for replay 2017-03-13 11:31:51 +11:00
priseborough 8c46d4316b AP_NavEKF2: 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
priseborough b7c4945000 AP_NavEKF2: 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
Randy Mackay 563be389ee AP_NavEKF2: only use downward facing rangefinder 2017-02-27 15:18:10 +09:00
Michael du Breuil 8b69f1708e NavEKF2: Add optional check for GPS vertical accuracy before aligning the EKF 2017-02-22 11:53:42 -08:00
Jacob Walser e7a34b0fb3 AP_NavEKF2: Add set_baro_alt_noise method 2017-02-21 11:26:14 +11:00
priseborough 1a7b5538e5 AP_NavEKF2: Enable simple heading fusion to be set for specific cores 2017-02-15 19:17:53 +00:00
priseborough a1d41edc4e AP_NavEKF2: 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 5cd403c0b9 AP_NavEKF2: prevent NaN if RNGFND_GNDCLEAR is zero 2017-02-15 07:04:38 +09:00
priseborough a63eac8073 AP_NavEKF2: Add missing perf_end 2017-01-27 16:57:42 +09:00
priseborough 7ea37029b6 AP_NavEKF2: use standard unit descriptor for milliseconds 2017-01-27 16:57:42 +09:00
Dr.-Ing. Amilcar Do Carmo Lucas 715d094678 AP_NavEKF2: Correct display names, bitmask and units 2017-01-16 19:07:26 +00:00
Francisco Ferreira c6875e1756
AP_NavEKF2: remove editor information wrongly added in d408d25 2017-01-09 16:16:14 +00:00
Dr.-Ing. Amilcar Do Carmo Lucas 9389ec2274 AP_NavEKF2: fix parameter descriptions 2017-01-09 13:30:30 +09:00
Dr.-Ing. Amilcar Do Carmo Lucas d408d25f92 More spelling stuff 2017-01-06 10:57:39 -08:00
Dr.-Ing. Amilcar Do Carmo Lucas 8419045aea Spell in comments 2017-01-06 10:57:39 -08:00
murata 653030b038 AP_NavEKF2: Changed if statements to switch statement.
AP_NavEKF2: Change indentation.
2016-12-26 10:15:55 +09:00
priseborough 6dc7d25fde AP_NavEKF2: 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 fe69d9a0ea AP_NavEKF2: remove duplicate include 2016-12-18 10:28:04 +11:00
priseborough a8f3a374e2 AP_NavEKF2: replace sqrt function calls with sqrtf
Prevents compiler errors and un-wanted use of double precision types
2016-12-18 10:28:04 +11:00
priseborough 76106889d5 AP_NavEKF2: Prevent unwanted core switch on startup
Require primary core to be healthy for 10 seconds before starting selection logic
2016-12-13 01:18:28 +00:00
priseborough 69f3c83c20 AP_NavEKF2: Don't use speed switch criteria when speed estimate is invalid
Prevent unwanted switches from range finder to Baro height aiding due to triggering of the speed threshold
2016-12-09 21:17:28 +00:00
priseborough 14a0155f5e AP_NavEKF2: Allow threshold speed for range finder use to be adjusted 2016-12-09 21:17:28 +00:00
murata 25e47cce6b AP_NavEKF2: Changed sqrt method to sqrtf method.
AP_NavEKF2: Changed sqrt method to sqrtf method.
2016-12-07 15:41:41 +00:00
Randy Mackay fc5f4c20cd AP_NavEKF2: remove redundant check of beacon nullptr
thanks to muramura for spotting this
2016-12-01 14:53:26 +09:00
priseborough 665ba1c009 AP_NavEKF2: Fix bug in reporting of vertical position reset
Fixes a bug that allows the last reported reset time to to wind back and an out of date reset delta to be reported if a switch to a core that has previously been reset occurs.
Allows multiple consumers provided they access on the same frame.
2016-12-01 10:35:38 +09:00
priseborough 7f347e39dd AP_NavEKF2: Fix bug in reporting of horizontal position reset
Fixes a bug that allows the last reported reset time to to wind back and an out of date reset delta to be reported if a switch to a core that has previously been reset occurs.
Allows multiple consumers provided they access on the same frame.
2016-12-01 10:35:38 +09:00
priseborough 656d9bb2c4 AP_NavEKF2: Fix bug in reporting of yaw reset
Fixes a bug that allows the last reported reset time to to wind back and an out of date reset delta to be reported if a switch to a core that has previously been reset occurs.
Allows multiple consumers provided they access on the same frame
2016-12-01 10:35:38 +09:00
Randy Mackay 66a9093cd0 AP_NavEKF2: getRangeBeaconDebug returns false on failure to get beacon data 2016-11-30 17:56:51 +09:00
priseborough 0ec8f0932a AP_NavEKF2: Prevent output of NaN's in range beacon debug output
This can happen if this accessor function is called before the EKF states are initialised
2016-11-30 17:56:50 +09:00
Randy Mackay fbecda7eeb AP_NavEKF2: change order of variable initialisation
No functional change, this modifies the init order to match the declaration order.
2016-11-30 17:56:49 +09:00
Randy Mackay 82854953e7 AP_NavEKF2: minor comment fix 2016-11-30 17:56:48 +09:00
Randy Mackay 14a73e499a AP_NavEKF2: initialise two range beacon structures 2016-11-30 17:56:47 +09:00
priseborough 2ee8250807 AP_NavEKF2: Changes from code review by @muramura 2016-11-30 17:56:46 +09:00
Randy Mackay 1f4606e48a AP_NavEKF2: protect against null beacon 2016-11-30 17:56:45 +09:00
Randy Mackay 51ccfca31c AP_NavEKF2: fix format of statustext for beacon init 2016-11-30 17:56:44 +09:00
priseborough ef03a85cd3 AP_NavEKF2: add range beacon interface and fusion method 2016-11-30 17:56:43 +09:00
priseborough 0a177d04fd AP_NavEKF2: Simply core switch implementation
Functionally equivalent
2016-11-24 19:58:10 +09:00
priseborough 7d48054e6f AP_NavEKF2: Group GPS innovation tests when compiling error score 2016-11-24 19:58:07 +09:00
Randy Mackay e9ea06bd10 AP_NavEKF2: minor comment fix 2016-11-24 19:58:03 +09:00
priseborough 0df45703f1 AP_NavEKF2: Fix errors in position reset delta publishing 2016-11-24 19:57:47 +09:00
priseborough f6021c959d AP_NavEKF2: capture and publish vertical position reset deltas
Calculate the change in vertical position due to a internal EKF state reset or a EKF core switch
2016-11-24 19:57:45 +09:00
priseborough e62863f9a1 AP_NavEKF2: Reduce unnecessary EKF core switching
1) Do not switch to a core until its states have been updated.
2) Distinguish between mandated switches required for health failure and optional switches required due to innovation checks failing.
3) Apply hyseresis to innovation check levels
2016-11-24 19:57:41 +09:00
murata c808ee2f49 Global: To nullptr from NULL.
RC_Channel: To nullptr from NULL.

AC_Fence: To nullptr from NULL.

AC_Avoidance: To nullptr from NULL.

AC_PrecLand: To nullptr from NULL.

DataFlash: To nullptr from NULL.

SITL: To nullptr from NULL.

GCS_MAVLink: To nullptr from NULL.

DataFlash: To nullptr from NULL.

AP_Compass: To nullptr from NULL.

Global: To nullptr from NULL.

Global: To nullptr from NULL.
2016-11-02 16:04:47 -02:00
Andrew Tridgell 82365f8670 AP_NavEKF2: save some memory in the position offsets in EKF2
we don't need to copy that vector3f for every sample. A uint8_t does
the job
2016-10-27 17:09:06 +11:00
priseborough c93c3d54f3 AP_NavEKF2: Don't correct for zero IMU position offset
The IMU offset correction involves a significant number of floating point operations and most users will leave the offset parameter at zero.
2016-10-27 14:54:44 +11:00
priseborough 1890bbdafa AP_NavEKF2: Don't correct GPS for zero position offset 2016-10-27 14:54:44 +11:00
priseborough f025c96e63 AP_NavEKF2: Don't correct range finder for zero position offset 2016-10-27 14:54:43 +11:00
priseborough 9a0ce1d5eb AP_NavEKF2: Don't correct flow sensor for zero position offset 2016-10-27 14:54:43 +11:00
priseborough b40016db62 AP_NavEKF2: Fix documentation errors 2016-10-27 14:54:43 +11:00
priseborough 13ca62b1c7 AP_NavEKF2: Correct velocity and position outputs for IMU offset
This can improve position hold performance where it is not practical to have the IMU located at the centroid.
Although this enables the effect of IMU position offsets to be corrected, users will still need to be instructed to place the IMU as close to the vehicle c.g. as practical as correcting for large offsets makes the velocity estimates noisy.
2016-10-27 14:54:43 +11:00
priseborough 21dcf42c27 AP_NavEKF2: Add missing documentation 2016-10-27 14:54:43 +11:00
priseborough 8922861359 AP_NavEKF2: Correct optical flow data for sensor position offset
Correction requires the body rates averaged across the flow sensor sampling interval. This data has been added to the sensor buffer.
The body rate data from the flow sensor driver does not contain the Z component, so an equivalent value sampled from the navigation IMU has been used instead.
The variable omegaAcrossFlowTime has been moved out of the class and into the only function that uses it.
2016-10-27 14:54:43 +11:00
priseborough 16f021c466 AP_NavEKF2: Correct range finder data for body frame position offset 2016-10-27 14:54:43 +11:00
priseborough e884e9cc6e AP_NavEKF2: Correct GPS data for antenna body frame offset 2016-10-27 14:54:43 +11:00
priseborough 064a106808 AP_NavEKF2: Get IMU accelerometer body position offset data 2016-10-27 14:54:42 +11:00
priseborough 397033b7c3 AP_NavEKF2: Add flow sensor body position offset to data buffer 2016-10-27 14:54:42 +11:00
priseborough 92c086b40e AP_NavEKF2: Add rangefinder body position offset to data buffer 2016-10-27 14:54:42 +11:00
priseborough 3148ad4623 AP_NavEKF2: Add GPS antenna position offset data to data buffer 2016-10-27 14:54:42 +11:00
priseborough fd905c23e1 AP_NavEKF2: Add body position offset to optical flow interface 2016-10-27 14:54:42 +11:00
Mathieu OTHACEHE 152edf7189 Global: remove mode line from headers
Using a global .dir-locals.el file is a better alternative than
reincluding the same emacs header in every file of the project.
2016-10-24 09:42:01 -02:00
priseborough 9779511425 AP_NavEKF2: Fix bug in median filter code 2016-10-19 19:45:00 +09:00
Jonathan Challinger dac59cb5da AP_NavEKF2: use exact matrix for trim rotation 2016-10-13 10:02:14 +11:00
priseborough 5d09c78f34 AP_NavEKF2: Always perform optical flow takeoff check when receiving data
A specialised takeoff check is now always performed when we receive new flow data as the default behaviour is to try and use flow data whenever it is received, rather than limit its use to a use to a flow-only mode of operation that had to be selected via user parameter.
2016-10-10 14:49:48 +09:00
priseborough a75a383ef2 AP_NavEKF2: Update protection for out of focus flow data 2016-10-10 14:49:41 +09:00
priseborough 635826c056 AP_NavEKF2: Fix reporting of terrain estimator innovations
Terrain height is relevant whenever optical flow data is present
2016-10-10 14:49:35 +09:00
priseborough b0072b587c AP_NavEKF2: fix reporting of optical flow use status 2016-10-10 14:49:24 +09:00
priseborough ed9ecb28fb AP_NavEKF2: Enable entry into relative position mode on start-up 2016-10-10 14:49:21 +09:00
priseborough e0b8c54194 AP_NavEKF: Update GPS type parameter description 2016-10-10 14:49:18 +09:00
priseborough f9018fcc1b AP_NavEKF2: Enable simultaneous optical flow and GPS use
Enables simultaneous use of GPS and optical flow data with automatic fallback to relative position mode if GPS is lost and automatic switch-up to absolute position status if GPS gained/re-gained.
2016-10-10 14:49:02 +09:00
priseborough ab55991b33 AP_NavEKF2: Report position jumps due to lane switches
Also moves code required to update reset data due to lane switches into separate functionscto improve readability.
2016-10-10 11:56:14 +09:00
Francisco Ferreira 42cd8e9721 AP_NavEKF2: Handle yaw jumps due to core switches
Based on work from Paul Riseborough (priseborough)
2016-09-25 18:24:11 -07:00
Francisco Ferreira 8da22e441b Revert 3 commits about yaw reset core switch
Revert "AP_NavEKF2: Fix bug in published yaw reset value found during code review"
commit 175faf1e41.

Revert "AP_NavEKF2: use a struct for all yaw step class variables"
commit 77fad065d1.

Partially revert "AP_NavEKF2: Handle yaw jumps due to core switches"
commit 885bfd1b4e.
2016-09-25 18:24:11 -07:00
Randy Mackay 2ebb81b02f AP_NavEKF2: switching compass message to GCS downgraded to INFO 2016-09-21 21:42:44 +09:00
priseborough b6867e085d AP_NavEKF2: Don't report range finder variance on mavlink if not required 2016-09-21 10:41:21 +09:00
priseborough cb1d3c7ed2 AP_NavEKF2: Allow for terrain gradient when using range finder for height 2016-09-13 17:45:03 +09:00
priseborough 60d8adcca0 AP_NavEKF2: Fix height drift on ground using range finder without GPS 2016-09-13 17:44:59 +09:00
priseborough 8797714203 AP_NavEKF2: Fix bug in handling of invalid range finder data 2016-09-13 17:44:43 +09:00
priseborough 175faf1e41 AP_NavEKF2: Fix bug in published yaw reset value found during code review 2016-09-13 17:35:18 +09:00
priseborough 77fad065d1 AP_NavEKF2: use a struct for all yaw step class variables 2016-09-13 17:35:16 +09:00
priseborough 885bfd1b4e AP_NavEKF2: Handle yaw jumps due to core switches 2016-09-13 17:35:14 +09:00
Andrew Tridgell dd812cfc0c AP_NavEKF2: added getPrimaryCoreIMUIndex()
needed for correct AHRS gyro estimate
2016-09-05 12:53:53 +10:00
priseborough e6f36f04db AP_NavEKF2: Enable automatic use of range finder height
The EK2_RNG_USE_HGT parameter sets the height (expressed as a percentage of the maximum range of the range finder as set by the RNGFND_MAX_CM parameter) below which the range finder will be used as the primary height source when the vehicle is moving slowly.

When using a height reference other than GPS, the height datum can drift due to air pressure changes if using baro, or due to terrain height changes if using range finder as the primary height source. To ensure that a consistent height datum is available when switching between altitude sources, the WGS-84 height estimate of the EKF's local positi norigin is updated using a
single state Bayes estimator,

If rngfinder or gps height data is lost whilst being used, there will be a fall-back to baro data.
2016-08-08 10:56:44 +09:00
Jonathan Challinger d1ecc63bf1 AP_NavEKF2: change priority of statustext messages 2016-07-29 13:19:51 +09:00
Andrew Tridgell 567d5cdbe6 AP_NavEKF2: use mavlink messages not printf for state change notifications 2016-07-19 12:16:51 +10:00
priseborough bd7bf21475 AP_NavEKF2: Speed improve switch-over to backup magnetometer
When switching over to a back up magnetometer, ensure that the earth field estimate are reset. other wise mag earth field estimates due to the previous failed mag could cause data from the new mag to be rejected.
2016-07-19 12:16:50 +10:00
priseborough e34cdc6666 AP_NavEKF2: 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.
2016-07-19 12:16:50 +10:00
priseborough e2b8807260 AP_NavEKF2: 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.
2016-07-19 12:16:50 +10:00
priseborough fcc07b5560 AP_NavEKF2: Prevent multiple aiding mode changes per update 2016-07-19 12:16:50 +10:00
priseborough f4f347fb75 AP_NavEKF2: add missing parenthesis and console message 2016-07-19 12:16:50 +10:00
priseborough 9a23152ee4 AP_NavEKF2: 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.
2016-07-19 12:16:50 +10:00
priseborough 230ba2700f AP_NavEKF2: fix documentation errors 2016-07-19 12:16:50 +10:00
priseborough 341d070db8 AP_NavEKF2: Separate filter status update and get functions
The filter status logic calculations were being repeated every time the get function was called.
The logic is now updated once per filter update step and a separate get function added
2016-07-19 12:16:49 +10:00
priseborough b1717649b1 AP_NavEKF2: remove combined NED local position interface 2016-07-19 12:16:49 +10:00
priseborough e374ec634d AP_NavEKF2: Add separate horizontal/vertical local position interfaces 2016-07-19 12:16:49 +10:00
priseborough 04e8726d8a AP_NavEKF2: relax bias convergence check
Enables bias convergence check to pass within 30 seconds when vehicle is static.
2016-07-19 12:16:48 +10:00
priseborough 280395afa1 AP_NavEKF2: Don't declare ready to do aiding unless gyro bias is learned 2016-07-19 12:16:48 +10:00
priseborough 169cd6625d AP_NavEKF2: clean up output predictor 2016-07-19 12:16:48 +10:00
priseborough aaab250f13 AP_NavEKF2: Don't start GPS aiding until gyro calibration has stabilised
If we start GPS aiding before the gyro bias variances have reduced, glitches on the GPS can cause attitude disturbances that degrade flight accuracy during early flight.
2016-07-19 12:16:48 +10:00
priseborough 8793c75da0 AP_NavEKF2: clean up mag field learned logic 2016-07-11 00:44:33 +10:00
priseborough e6592186fc AP_NavEKF2: Tuning update
Slow down magnetic field learning
2016-07-10 08:21:18 +10:00
priseborough 10470b2dc1 AP_NavEKF2: fix bug in initialisation of declination co-variances
Co-variances were being re-zeroed after being set. This meant that the initial declination learning was sensitive to measurement errors which could result in poor initial yaw accuracy.
2016-07-10 08:21:18 +10:00
priseborough 6b04a81b8d AP_NavEKF2: Fix plane in-flight yaw reset bug
Fixes bugs that prevented planes being able to reset yaw to GPS to recovery from takeoff with a bad magnetoemter.

1) If the velocity innovation check had not failed by the time the in-air transition occurred, then the yaw reset would not be performed
2) The velocity states were not being reset
3) The non fly-forward vehicle (copter) reset could occur first and effectively lock out the fly-forward vehicle (plane) yaw check.
2016-07-10 08:21:18 +10:00
priseborough 51dbed2338 AP_NavEKF2: remember mag field states between flight on same power cycle
Remember the mag bias and earth field states learned during flight when the vehicle  lands.
This improves performance for vehicles that do multiple flight on one power cycle
2016-07-10 08:21:18 +10:00
priseborough 136df7cb5c AP_NavEKF2: reduce declination errors on start of 3-axis fusion
Reset co-variances for NE field states.
2016-07-10 08:21:18 +10:00
priseborough 744f19cd2d AP_NavEKF2: Improve scaling of output predictor I gain
Provide consistent overshoot of 5% across a wider range of time constants and prevent selection of larger time constants causing 'ringing' in the position and velocity outputs.
2016-07-09 15:57:36 +10:00
priseborough a49c16d63c AP_NavEKF2: Update output filter tuning
Updated tuning to take advantage of corrected time delta dtEkfAvg
2016-07-09 15:57:36 +10:00
priseborough 55dee347e0 AP_NavEKF2: Fix bug in averaged filter delta time
Average EKF time delta was not being updated.
2016-07-09 15:57:36 +10:00
priseborough 927186339c AP_NavEKF2: Improved output predictor tracking
Implement a PI feedback controller for velocity and position state tracking
2016-07-09 15:57:35 +10:00
priseborough 253f744824 AP_NavEKF2: Collect output predictor tracking data 2016-07-09 15:57:35 +10:00
priseborough 14bb4f4574 AP_NavEKF2: Publish output observer tracking errors 2016-07-09 15:57:35 +10:00
priseborough fa435d0323 AP_NavEKF2: Allow for faster accel bias change in-flight
Fixes a problem observed in a flight log where rapid temperature change caused the accel bias to change faster than the EKF could keep up.
This allows the bias to be learned faster but with acceptable level of noise in the estimate
2016-07-09 15:57:35 +10:00
priseborough 191c34612d AP_NavEKF2: Fix bug in use of corrected IMU data
IMU data was being corrected before being used by the co-variance prediction, whereas the delta angles and velocities in the derivation were supposed to be uncorrected.
This patch creates separate variable for the corrected data
2016-07-09 15:57:35 +10:00
priseborough 118d5b88b2 AP_NavEKF2: Clean up output observer and reduce pos vel time constant
Previous Time constant was too large leading to poor tracking of EKF states in the presence of bad quality IMU data.
2016-07-09 15:57:35 +10:00
Paul Riseborough 4a8689aa97 AP_NavEKF2: remove duplicate if statements from mag fusion 2016-06-28 14:20:13 +10:00
Paul Riseborough e117bedf6a AP_NavEKF2: Adjust output observer tuning
Use more accurate method by default.
Reduce overshoot on quaternion tracking
2016-06-28 14:20:13 +10:00
Paul Riseborough 5c59922574 AP_NavEKF2: Fix bug that could publish bad compass offsets
Magnetometer bias states will subject to larger errors early in flight before flight motion makes the offsets observable and the state variances reduce.
Adds a check on state variances.
Replaces the parameter check with a check of the actual filter fusion method being used.
2016-06-28 14:20:13 +10:00
Paul Riseborough 165335b9e3 AP_NavEKF2: Improve ability to tune magnetic field learning
Allow different process noise to be set for body (sensor bias) and earth field states.
This allows a stable magnetometer bias estimate to be available at end of flight whilst still allowing for external magnetic anomalies during landing.
Adjust default values to give stable mag bias learning and fast learning of external anomalies.
2016-06-28 14:20:12 +10:00
Paul Riseborough 6523481c76 AP_NavEKF2: Improve tracking accuracy of output predictor
Automatically use the highest gain consistent with a 5% overshoot to minimise RMS tracking errors.
Provide an alternative correction method for the position and velocity states that allows the user to specify the time-constant. This can be used to fine tune the output observer for for platform specific sensor errors and control loop sensitivity estimation noise.
2016-06-28 14:20:12 +10:00
Paul Riseborough fe06606193 AP_NavEKF2: Ensure corrected IMU data used by EKF
Don't try to pop new IMU data from the buffer unless we have written data.
Correct IMU data as soon as it is popped from the buffer
2016-06-28 14:20:12 +10:00
Paul Riseborough 1400dc9d02 AP_NavEKF2: Add tuning parameters for magentic yaw fusion
Enable simple magnetic yaw fusion observation noise and innovation consistency check gate width to be tuned independantly.
2016-06-28 14:20:12 +10:00
Paul Riseborough dc6836988c AP_NavEKF2: Improve ground based magnetic anomaly protection for copter
The toilet bowling check during early flight has been removed. This check caused problems where bad compass calibration was the cause of the toilet bowling and resetting to the compass was a bad option. The handling of simultaneous failed mag and velocity innovations is already handled outside the EKF by the failsafe.
A check for yaw errors due to a ground based magnetic anomaly has been introduced.
The logic for in-flight yaw and magnetic field resets has been cleaned up and variable names improved.
2016-06-28 14:20:12 +10:00
Paul Riseborough 703f56908f AP_NavEKF2: Correct comment 2016-06-28 14:20:12 +10:00
Paul Riseborough 26815ace7a AP_NavEKF2: Remove redundant logic check 2016-06-28 14:20:12 +10:00
Jonathan Challinger bd8c804ab5 AP_NavEKF2: correct comments 2016-06-28 14:20:12 +10:00
Jonathan Challinger ebae95d7f6 AP_NavEKF2: apply corrections to new inertial data when using for output prediction 2016-06-28 14:20:11 +10:00
Jonathan Challinger 2f709dfe86 AP_NavEKF2: improve inertial prediction 2016-06-28 14:20:11 +10:00
Paul Riseborough 262c5fe56d AP_NavEKF2: Make setter loop through all instances
For setters where a success boolean is returned, return false if any instance fails.
2016-06-28 14:20:11 +10:00
Jonathan Challinger 8baf064317 AP_NavEKF2: setTakeoffExpected and setTouchdownExpected loop through instances 2016-06-28 14:20:11 +10:00
Paul Riseborough ec5c460584 AP_NavEKF2: Fix predicted nav reporting
Predicted nav should never be false if current nav is true
2016-06-28 14:20:11 +10:00
Jonathan Challinger 99f481e098 AP_NavEKF2: always calcGpsGoodForFlight 2016-06-28 14:20:11 +10:00
Jonathan Challinger 3382e09580 AP_NavEKF2: add height constraint during takeoff 2016-06-28 14:20:11 +10:00
Paul Riseborough 4bb46af861 AP_NavEKF2: Increase allowable gyro bias offset 2016-06-28 14:20:10 +10:00
Paul Riseborough 24d8cc62e2 AP_NavEKF2: rework yaw and magnetic heading reset logic
Splits in-flight yaw alignment completed status into separate yaw and magnetic field flags.
Reduce the number of places where decisions to perform a yaw and field reset are made.
Don't perform a reset unless there is is data in the buffer
Don't use 3-axis fusion if the field states still need to be reset.
When starting 3-axis fusion request a reset if not previously performed.
Ensure magnetometer and GPs heading resets are alwasy perfomred with data at teh correct time horizon.
2016-05-31 16:12:53 +10:00
Paul Riseborough a94a19bd09 AP_NavEKF2: Fix bug causing continual yaw resets 2016-05-28 06:52:11 +10:00
Andrew Tridgell 97e2203e70 AP_NavEKF2: don't do 3D mag fusion on 2nd EKF2 core
this reduces the risk that mag fusion errors will badly affect
attitude estimation.
2016-05-27 21:27:06 +10:00
Paul Riseborough de15928921 AP_NavEKF2: prevent potential arithmetic error in declination fusion 2016-05-27 09:00:41 +10:00
Paul Riseborough 722eb0d706 AP_NavEKF2: Fix bug for start of wind speed estimation
The commencement of airspeed fusion could cause pitch errors due to small variances and large innovations. This issue is addressed by the following changes:
1) The airspeed measurement is used to set wind states to a value that reduces initial innovations.
2) The wind state variances are set to values that better reflect the wind speed uncertainty
2016-05-27 09:00:41 +10:00
Paul Riseborough ac329ec31c AP_NavEKF2: use observation noise to set initial magnetic field variances 2016-05-27 09:00:41 +10:00
Paul Riseborough 830751c0ae AP_NavEKF2: remove un-wanted functionality from mag and yaw reset
The function used to reset magnetic field states and yaw angle should not be used when there is no magnetometer. If it is incorrectly called without a magnetometer it should not change the attitude or field states.
2016-05-27 09:00:41 +10:00
Paul Riseborough 11c6ea7ef6 AP_NavEKF2: attitude co-variance reset for all post alignment yaw resets
Whenever the yaw angle is changed, the correlation with other state errors will be incorrect and the terms should be zeroed.
2016-05-27 09:00:41 +10:00
Paul Riseborough cdd09df9ac AP_NavEKF: Add function to zero attitude state co-variances
When changing the vehicle yaw angle, the correlation between the attitude errors and errors in other states is invalid so the corresponding co-variance terms need to be zeroed.
This needs to be done in more than one place.
2016-05-27 09:00:41 +10:00
Paul Riseborough 6d34ac5ceb AP_NavEKF2: improve switch-over to use of mag field states
Set initial variances to measurement uncertainties
Always perform a field  and yaw reset
2016-05-27 09:00:40 +10:00
Paul Riseborough fe9ddfdfeb AP_NavEKF2: remove code that prevents attitude updates after mag reset
This code assumes a vehicle is close to level and will not work for all vehicle types. It will be replaced by a different method.
2016-05-27 09:00:40 +10:00
Paul Riseborough fe85c68344 AP_NavEKF2: move yaw reset for no compass case
Should not be in a function that performs reset on magnetic field states
2016-05-27 09:00:40 +10:00
Paul Riseborough da0622827d AP_NavEKF: update tuning defaults
Increase speed of scale factor learning
2016-05-27 09:00:40 +10:00
Paul Riseborough 9eef97d108 AP_NavEKF2: use consistent parameter naming
M_NSE is a measurement noise
P_NSE is a observation noise
I_GATE is an innovation gate

This also ensures the new parameter values required to use the EKF2 will be enforced.
2016-05-25 12:06:04 +10:00
Paul Riseborough 74121fdaeb AP_NavEKF2: fix bug preventing in-flight alignment 2016-05-21 15:13:53 +10:00
Paul Riseborough 16cb7078cd AP_NavEKF2: Fix misleading pre-flight status reporting 2016-05-21 15:13:53 +10:00
Paul Riseborough 38d61f5281 AP_NavEKF2: Update status reporting to handle no-magnetometer startup 2016-05-21 15:13:53 +10:00
Paul Riseborough 9aa3cdfaae AP_NavEKF2: Update GPS yaw re-alignment function
Updates to support initial alignment without magnetometer
2016-05-21 15:13:53 +10:00
Paul Riseborough e3c966661b AP_NavEKF2: Remove unnecessary variance reset
This reset is unnecessary give that a synthetic yaw angle is fused at a low rate to prevent variances from becoming badly conditioned.
2016-05-21 15:13:53 +10:00
Paul Riseborough 1179c08473 AP_NavEKF2: Handle case where we are in-flight and haven't yet aligned the yaw
This happens if planes are flown without a compass
2016-05-21 15:13:53 +10:00
Paul Riseborough 581c1aa0d4 AP_NavEKF2: Adjust attitude variance values used after a heading reset
Because these errors are in body frame, a spherical error should be used to accommodate different orientations
2016-05-21 15:13:53 +10:00
Paul Riseborough 5ec8d523f6 AP_NavEKF: remove unwanted co-variance reset
The co-variance resets required following a velocity and position state reset is now performed in the stte reset function
2016-05-21 15:13:53 +10:00
Paul Riseborough 66e4d9d6e8 AP_NavEKF2: Reset co-variance values when doing a pos,vel,hgt reset
Ensures consistent behaviour after resets and reduces attitude disturbances
2016-05-21 15:13:52 +10:00
Paul Riseborough cf8175a073 AP_NavEKF2: Allow immediate use of GPS in-flight for plane without compass
Planes operating without a compass must align the yaw to the GPS heading immediately after launch or takeoff and cannot wait for GPS accuracy checks.
2016-05-21 15:13:52 +10:00
Paul Riseborough 08de4e6d95 AP_NavEKF: Do not perform start-up yaw alignment if no compass
Yaw cannot be aligned until in-flight when there is sufficient GPS velocity.
2016-05-21 15:13:52 +10:00
Paul Riseborough d2694fe5dc AP_NavEKF2: Remove duplicate transition into GPS aiding
This decision is made in one place in setAidingMode()
2016-05-21 15:13:52 +10:00
Paul Riseborough 7201f7d2fd AP_NavEKF2: fix comment 2016-05-21 15:13:52 +10:00
Paul Riseborough 64a8153b68 AP_NavEKF2: update function name
The primary purpose of this function is re-alignment
2016-05-21 15:13:52 +10:00
Paul Riseborough addd213af0 AP_NavEKF2: reduce effect of acceleration on non-GPS mode attitude 2016-05-21 15:13:52 +10:00
Paul Riseborough a3b78e6231 AP_NavEKF2: update tuning defaults 2016-05-21 15:13:51 +10:00
Paul Riseborough 65f63341d7 AP_NavEKF2: Improve numerical error protection in optical flow fusion
Abort fusion of data if variances will become negative and publish the fault
2016-05-21 15:13:51 +10:00
Paul Riseborough 42da33593d AP_NavEKF2: fix yaw fusion numerical health reporting 2016-05-21 15:13:51 +10:00
Paul Riseborough 6eb9d43507 AP_NavEKF2: add numerical error checking and isolation to mag decl fusion 2016-05-21 15:13:51 +10:00
Paul Riseborough b325c5faeb AP_NavEKF2: add error checking and isolation to mag heading fusion 2016-05-21 15:13:51 +10:00
Paul Riseborough a0b1dc5325 AP_NavEKF2: add error checking and isolation to 3D amg fusion 2016-05-21 15:13:51 +10:00
Paul Riseborough 51a3df0319 AP_NavEKF2: Add error checking and isolation to pos vel fusion 2016-05-21 15:13:51 +10:00
Paul Riseborough 71b589c89c AP_NavEKF2: extend fusion fault reporting coverage 2016-05-21 15:13:50 +10:00
Paul Riseborough 0982bd0b2b AP_NavEKF2: update parameter documentation 2016-05-21 15:13:50 +10:00
Paul Riseborough 46a2993a0d AP_NavEKF: use intuitive units for imu bias process noise parameters 2016-05-21 15:13:50 +10:00
Paul Riseborough 8c374fd679 AP_NavEKF2: correct comments 2016-05-21 15:13:50 +10:00
Paul Riseborough 6be9eaa524 AP_NavEKF2: use receiver estimated accuracy
Adjust the GPS observation noise based on receiver accuracy output if available.
2016-05-21 15:13:50 +10:00
Paul Riseborough dddc213836 AP_NavEKF2: Open up tuning limits
Done to assist tuning assessments
2016-05-21 15:13:50 +10:00
Paul Riseborough cf05e110fc AP_NavEKF2: fix scaling error in use of IMU noise parameters
Also remove process noise from state transition matrix where it was mistakenly left in after the derivation
2016-05-21 15:13:50 +10:00
Andrew Tridgell 4080c6091d AP_NavEKF2: fixed an assumption that _ahrs->get_compass() always works
if MAG_ENABLE=0 in plane there is no compass
2016-05-19 14:16:40 +10:00
Tom Pittenger d67b1edf10 AP_NavEKF2: (potential) compiler warning of float to double promotion 2016-05-17 20:30:51 -07:00
Ricardo de Almeida Gonzaga 64d14356b9 AP_NavEKF2: Fix typos 2016-05-13 19:20:06 -03:00
dgrat 41661f815f AP_Math: Replace the pythagorous* functions with a variadic template
The new function can deal with a variable number of function parameters.
Additionally, I renamed the functions to norm(), because this is the
standard name used in several other projects.
2016-05-10 11:41:26 -03:00
Andrew Tridgell ea508f1b80 AP_NavEKF2: use LOG_REPLAY and EK2_LOG_MASK parameters 2016-05-09 12:26:57 +10:00
Andrew Tridgell 32af886ba9 AP_NavEKF2: use consistent logging timestamps for sensors 2016-05-07 18:27:22 +10:00
Andrew Tridgell 4e4c575f16 AP_NavEKF2: added have_ekf_logging() 2016-05-07 18:27:20 +10:00
Andrew Tridgell b7ba0fa458 AP_NavEKF2: added ad-hoc logging example to EKF2 2016-05-07 18:27:20 +10:00
Andrew Tridgell 223c512188 AP_NavEKF2: added logging of sensor data in EKF2 2016-05-07 18:27:18 +10:00
Andrew Tridgell f92279f436 AP_NavEKF2: allow logging of IMT data from inside EKF2 2016-05-07 18:27:17 +10:00
Andrew Tridgell 9c4dd024bf AP_NavEKF2: auto change EK2_GPS_TYPE for NMEA
this fixes a problem where users of NMEA GPS receivers could not arm
with default EK2 parameters.
2016-05-05 19:46:33 +10:00
Andrew Tridgell ac60901b0c AP_NavEKF2: use vector comparison for new mag vector 2016-04-21 09:56:22 +10:00
Jonathan Challinger 97112ccd44 AP_NavEKF2: check mag instance id when returning mag offsets 2016-04-21 09:51:41 +10:00
Jonathan Challinger 1185cd1be7 AP_NavEKF2: move getMagOffsets into outputs 2016-04-21 09:51:41 +10:00
Jonathan Challinger acfaafe276 AP_NavEKF2: detect changes to magnetometer offset parameters and reset states 2016-04-21 09:51:41 +10:00
Paul Riseborough 1ecc206eee AP_NavEKF2: Allow use in planes without a magnetometer
Implements the following techniques to enable planes to operate without magnetometers.

1) When on ground with mag use inhibited, a synthetic heading equal to current heading is fused to prevent uncontrolled covariance growth.
2) When transitioning to in-flight, the delta between inertial and GPS velocity vector is used to align the yaw.
3) The yaw gyro bias state variance is reset following an in-flight heading reset to enable the yaw gyro bias to be learned faster.
2016-04-15 08:31:47 +10:00
Paul Riseborough 6d9ba8c527 AP_NavEKF2: Improve protection against ground based mag interference
Reset the mag field states and yaw earlier than the normal 5m height threshold if toilet bowling is detected.
2016-03-17 10:55:11 +11:00
Lucas De Marchi e40b87cd0e AP_NavEKF2: replace header guard with pragma once 2016-03-16 18:40:42 +11:00
Paul Riseborough 38b3625ed8 AP_NavEKF2: Fix bug in initial alignment calculation
The bug caused the initial roll angle to be incorrect if the vehicle was powered up when inverted, causing long alignment times.
2016-03-02 09:10:09 +09:00
Paul Riseborough 2888bdd6d5 AP_NavEKF: Protect against possible div by 0 2016-03-01 10:08:47 -03:00
Paul Riseborough 7d6b926749 AP_NavEKF2: Improved magnetic heading fusion
Use an Euler yaw heading that switches between a 321 and 312 rotation
sequence to avoid areas of singularity.  Using Euler yaw decouples the
observation from the roll and pitch states and prevents magnetic
disturbances from affecting roll and pitch via the magnetometer fusion
process.
2016-03-01 10:08:47 -03:00
Paul Riseborough bb74371c58 AP_NavEKF2: Do not use GPS height if GPS accuracy is poor
If we are using GPS height, revert back to using Baro height if the GPS accuracy is poor.
2016-03-01 15:13:13 +09:00
dgrat 5148e41c1a AP_Math: Cleaned macro definitions
Moved Definitions into a separate header. Replaced PI with M_PI and
removed the M_PI_*_F macros.
2016-02-27 02:51:33 -03:00
Paul Riseborough 7459bfb96b AP_NavEKF2: Eliminate simple compass fusion singularities near +-90 deg pitch
The use of yaw angle fusion during startup and ground operation causes problems with tail-sitter vehicle types.
Instead of observing an Euler yaw angle, we now observe the yaw angle obtained by projecting the measured magnetic field onto the the horizontal plain.
This avoids the singularities associated with the observation of Euler yaw angle.
2016-02-22 16:29:36 +11:00
Paul Riseborough 4aefe1caee AP_NavEKF2: Fix sign error in magnetic heading innovation calculation 2016-02-20 08:55:48 +11:00
Peter Barker 475a2040a1 AP_NavEKF2: avoid use of undefined #defines
Ensure EKF_DISABLE_INTERRUPTS is defined

Do not define MATH_CHECK_INDEXES, assume it is defined
2016-02-19 12:34:24 -02:00
Paul Riseborough 047e9fabaf AP_NavEKF2: Fix bug in simple heading fusion
The innovation calculation should have been updated when the heading fusion maths was updated.

We now use a direct heading or yaw angle measurement in the derivation, not the difference between observed and published declination.
2016-02-19 15:35:11 +09:00