dark0707
/
px4-firmware
forked from Archive/PX4-Autopilot
1
0
Fork 0
Code Pull Requests Activity
356 Commits 514 Branches 136 Tags 234 MiB
Commit Graph

263 Commits

Author SHA1 Message Date
mcsauder 6c96f45f08 Remove whitespace differences with upstream for pull request. 2016-02-23 19:49:27 -07:00
mcsauder fad1c87631 Merge upstream and resolve merge conflicts. 2016-02-23 19:29:30 -07:00
Roman Bapst 8eb63a150d Merge pull request #53 from bugobliterator/pr-sharedlib 
Shared Library build
 2016-02-23 08:30:46 +01:00
Paul Riseborough a711632017 EKF: Add method to fuse horizontal magnetometer data 
This method is more suitable than a raw heading measurement because it works across a full range of pitch angles.
It has been made the default for ground operation.
 2016-02-20 19:45:32 +11:00
mcsauder 4ce4724105 Added variable initializations back into EstimatorInterface() constructor to resolve a runtime error that occurs with uninitialized variables. 2016-02-19 23:57:06 -07:00
Paul Riseborough 6df6ac0023 EKF: Fix sign error in heading innovation calculation and clean up 2016-02-20 11:54:53 +11:00
Paul Riseborough 90e1bd3e36 EKF: wrap compass yaw estimate 2016-02-19 16:53:55 +11:00
Paul Riseborough 7d6226eb45 EKF: Improve efficiency of yaw angle fusion 
Use direct calculation of Kaman gains with optimised algebra
 2016-02-19 16:25:01 +11:00
Paul Riseborough 7f121e81e4 EKF: Update yaw innovation calculation to match revised derivation 
The new derivation does not use magnetic field measurements in the observation model and instead fuses in a heading measurement directly.
 2016-02-19 16:18:07 +11:00
mcsauder 72243c4a84 Resolve tab/space differences with upstream master. 2016-02-18 03:28:40 -07:00
mcsauder 437f6ca5fb Moved initialization to object constructors to allow C99 compiler compatibility. 2016-02-18 03:21:04 -07:00
bugobliterator ba7f0fc9ff EKF: add licensing information for mathlib header and src 2016-02-17 20:02:08 -08:00
bugobliterator 80632cc12c EKF: add comments and licensing information to builder files 2016-02-17 19:55:47 -08:00
bugobliterator a40eb7cf37 EKF: add check for existence of matrix submodule 2016-02-17 17:51:09 -08:00
bugobliterator 263c48d089 EKF: remove dependecies and allow ekf to be built as standalone shared lib 2016-02-17 17:33:18 -08:00
Paul Riseborough 96c0e18acb Merge pull request #49 from PX4/pr-fixMagCovariance 
EKF: Fix magnetometer fusion and covariance handling
 2016-02-18 10:22:36 +11:00
bugobliterator 2096e24c06 EKF: fix time of sample receive setting 2016-02-17 13:29:12 -08:00
Paul Riseborough a679cdf1fb EKF: Change parameter default to not fuse declination when aiding 
Ground and flight testing has shown declination drift to not be a problem with current tuning and realistic vehicle motion.
 2016-02-17 17:22:02 +11:00
Paul Riseborough abf9476853 EKF: miscellaneous formatting and typo updates 2016-02-16 11:08:30 +11:00
Paul Riseborough ffe1d30864 EKF: Set covariances to zero for un-used states 2016-02-16 11:08:30 +11:00
Paul Riseborough 294aca8609 EKF: Improve variance limiting for stationary states 
Turn off the process noise if they grow too large and use the hard variance limit as a backup. This is numerically more stable than relying on a hard variance limit which does not deal with the covariances.
 2016-02-16 11:08:30 +11:00
Paul Riseborough 1d40507af8 EKF: Set Kaman gains to zero for un-used states 
This is a defensive programming technique. In theory this should not be necessary if the corresponding covariance entries are zero.
 2016-02-16 11:08:30 +11:00
Paul Riseborough 69b8982043 EKF: Initialise variances to zero for un-used states 
Setting these variances to zero makes it less likely that these states will be modified by fusion processing.
 2016-02-16 11:08:30 +11:00
Paul Riseborough d9bf4e9870 EKF: Enable control mode transitions to be detected 
Save the previous value of the filter control modes
 2016-02-16 11:08:30 +11:00
Paul Riseborough 402206a305 EKF: Fix critical bug in fusion of yaw and declination observations 
This bug was in the derivation and resulted from use of a tan instead of an atan operator. The derivations have been reworked and the updated auto-code has been imported as part of this patch.
 2016-02-16 11:08:30 +11:00
Paul Riseborough 7da40a45a4 EKF: Add control mode for wind state estimation 2016-02-16 11:08:30 +11:00
Paul Riseborough de02aebafd EKF: Reset covariance matrix when doing a yaw and magnetic field reset 
The correlation terms in the covariance matrix will be incorrect after a reset, so should be zeroed
 2016-02-14 22:01:53 +01:00
Paul Riseborough dba58aa4c6 EKF: Add control logic for fusion modes 2016-02-14 22:01:53 +01:00
Paul Riseborough 22c177c951 EKF: Re-align yaw and magnetic field states when changing into GPS aiding mode 2016-02-14 22:01:53 +01:00
Paul Riseborough c089079321 EKF: Split tilt and yaw align 2016-02-14 22:01:53 +01:00
Paul Riseborough 020cc5978e EKF: Move calculation of declination into a separate function 2016-02-14 22:01:53 +01:00
Paul Riseborough aa58b3e98c EKF: Split angular alignment into tilt and yaw and use yaw and magnetic field alignment function 2016-02-14 22:01:53 +01:00
Paul Riseborough 2bbe7f9a1c EKF: Update magnetometer fusion to use declination from the specified source 2016-02-14 22:01:53 +01:00
Paul Riseborough 83945581ed EKF: Add function to calculate the magnetic declination to use 2016-02-14 22:01:53 +01:00
Paul Riseborough 9017e077f8 EKF: Publish the magnetic declination we wish to save for next startup 2016-02-14 22:01:53 +01:00
Paul Riseborough 0308f2f796 EKF: Add parameters to control declination source and fusion type 2016-02-14 22:01:53 +01:00
Paul Riseborough 6140d4b21f EKF: Add function to reset yaw and magnetic field states 2016-02-14 22:01:53 +01:00
Roman ad978c642f estimator interface: 
added flag for in_air status of vehicle
 2016-02-14 20:43:22 +01:00
Roman ce0ddc0207 -added comments 
-removed unused print functions
-removed false _imu_time_last variable (correct is _time_last_imu)
 2016-02-14 09:49:26 +01:00
Paul Riseborough 9d7340e187 EKF: Fix bugs in position and velocity resets 
The position reset was not being compensated for velocity and measurement delay
The height was being reset with the position. It has been moved into a separate reset function
The maximum accepted GPS delay of 100msec was inadequate
The states  was being incorrectly reset to the GPS position and Baro height on initial alignment.
 2016-02-14 09:49:26 +01:00
Paul Riseborough da1de2cc4d EKF: Correct for sensor noise and baro offset during alignment 2016-02-14 09:49:26 +01:00
CarlOlsson 1e766c7510 moved fuse function to ekf_helper.cpp 2016-02-12 15:54:32 +01:00
Paul Riseborough fff2bd50f6 EKF: Fix bugs in position and velocity resets 
The position reset was not being compensated for velocity and measurement delay
The height was being reset with the position. It has been moved into a separate reset function
The maximum accepted GPS delay of 100msec was inadequate
The states  was being incorrectly reset to the GPS position and Baro height on initial alignment.
 2016-02-10 15:16:05 +11:00
Paul Riseborough 40e174b81c EKF: Correct for sensor noise and baro offset during alignment 2016-02-10 10:25:27 +11:00
Paul Riseborough 5ea0ef39cd EKF: Update declination fusion logic 
We do not need to run declination fusion if 3-axis mag fusion is not being used.
 2016-02-09 07:54:24 +11:00
Paul Riseborough 47ab5ebcdd EKF: Make PR comply with project convention for indenting 2016-02-08 15:12:38 +11:00
Paul Riseborough cdc42c1de0 EKF: Add simple control logic for magnetic declination constraint 2016-02-08 14:18:43 +11:00
Paul Riseborough dbb8e12948 EKF: Add fusion method to constrain declination when unobservable 
When fusing 3-axis magnetometer data without absolute external aiding leg GPS), the declination is ultimately unobservable and the declination of the  field states and the vehicle heading will slowly drift over time. To prevent this we need to fuse in a declination to constraint the NE earth field estimates.
 2016-02-08 14:18:43 +11:00
Paul Riseborough 9347afe250 EKF: Use unique variable name for mag heading fusion observation Jacobian 2016-02-08 14:18:43 +11:00
Paul Riseborough 6aeccf01ff EKF: Add missing fusion health status messages 2016-02-08 14:18:43 +11:00
Paul Riseborough 2c8c6efb45 EKF: Eliminate use of power function to square numbers 
Use of the power function to square a number can be very inefficient depending on processor and compiler. Replace with an inlined function  that multiplies the number by itself. This has not been put into the maths library because the use of the sq() function is peculiar to the autocode generated for the EKF and an inlined function was desired.
 2016-02-08 11:11:59 +11:00
Paul Riseborough 3f81eb7d1b EKF: fix formatting 2016-02-04 17:15:03 +11:00
Paul Riseborough 9bfc11b660 EKF: Use specific position observation noise when flying without GPS 
A larger position uncertainty is required when flying without GPS to reduce tilt attitude estimation errors caused by vehicle manoeuvring. This needs to be tuneable to allow optimisation for different use cases (e.g. outdoor vs indoor).
 2016-02-03 18:40:32 +11:00
Paul Riseborough 7de1d39ce4 EKF: Improve use of position and velocity observation noise parameters 
Fix bug where noise parameters were not being squared when calculating the observation variance.
Use GPS reported speed accuracy to set velocity observation noise and use the parameter to set the minimum.
 2016-02-03 18:15:38 +11:00
Paul Riseborough 2b1e8fe910 EKF: Update tuning parameters 
Set conservative defaults as a baseline for tuning
Add a missing parameter for magnetometer observation noise.
Correct error in definition of magnetic heading observations noise (previous parameter defined the variance directly, not the noise).
Scale vertical GPS noise to allow for average EPV to EPH ratio.
Update documentation and display names for consistency.
 2016-02-03 17:05:45 +11:00
Lorenz Meier b21a49b3f9 EKF: Use standard C++ initializers 2016-01-31 23:24:36 +01:00
Roman b749a7557b fixed typos 2016-01-31 21:36:58 +01:00
bugobliterator d79e12dfa1 EKF: fix code style 2016-01-31 00:12:16 -08:00
bugobliterator 8200ef4d17 EKF: allocate and unallocate buffer more robustly 2016-01-31 00:12:16 -08:00
bugobliterator c6249a2825 EKF: change estimator base class name to estimation interface 2016-01-31 00:12:07 -08:00
bugobliterator 3cafedd4c1 EKF: start storing samples only when ekf is initialised 2016-01-30 12:46:01 -08:00
bugobliterator b062bd2e38 EKF: move estimator specific variables to estimator core 2016-01-30 12:45:23 -08:00
bugobliterator 287f5eb0c2 EKF: move all estimator specific types to common header 2016-01-30 12:44:19 -08:00
bugobliterator b05e2d825c EKF: move estimator specific initialisations to estimator core 2016-01-30 12:42:24 -08:00
Paul Riseborough f1b82057c0 EKF: Combine GPS velocity innovation gate parameters 
Separate vertical and horizontal parameters for GPS velocity innovation gates are not required
 2016-01-30 12:21:50 -08:00
Paul Riseborough 466a104534 EKF: additional GPS check logic 
Improve naming of NED origin initialisation status
Add check for GPS solution type
Use GPS checks when regaining GPs in-flight
 2016-01-30 12:21:39 -08:00
bugobliterator a779d45cd0 ekf2: fix bug causing faulty imu data storage 2016-01-29 23:56:24 -08:00
bugobliterator 92dc41e885 EKF: fix typo in function declaration 2016-01-29 20:05:07 -08:00
bugobliterator 3eea6cdcc5 EKF: use namespace for structure definitions 
will be moved to a separate file in the future
 2016-01-29 20:04:21 -08:00
bugobliterator 001d621eb1 EKF: move imu data processing code to estimator core 2016-01-29 20:03:25 -08:00
bugobliterator 251996d387 ekf: move gps checks to Ekf library from estimator_base 2016-01-29 17:15:18 -08:00
Paul Riseborough 46b0e9654c Add filter control logic 2016-01-30 09:01:48 +11:00
Paul Riseborough 9236f11c80 EKF: Add position and velocity innovation consistency checks 2016-01-28 16:33:54 +11:00
Paul Riseborough 7713cc8c20 Merge pull request #17 from priseborough/pr-addMagErrHandling 
EKF: Add magnetometer fusion error handling
 2016-01-28 13:43:57 +11:00
Lorenz Meier f4b2c0eecf Merge pull request #11 from mcharleb/PRIu64-fix 
Fixed printf of uint64_t
 2016-01-28 01:01:10 +01:00
Paul Riseborough 802129f384 EKF: Add magnetometer fusion error handling 2016-01-28 09:53:55 +11:00
Paul Riseborough 39eef3a2d7 EKF: Remove use of camel case variable names 
Also fixes bug in GPS speed accuracy check that was using horizontal position accuracy variable by mistake.
 2016-01-28 08:37:45 +11:00
Paul Riseborough cc50d26601 EKF: Update comments 2016-01-28 08:13:38 +11:00
Paul Riseborough 4526cb9c4f EKF: remove redundant variable 2016-01-28 07:50:45 +11:00
Paul Riseborough 6326433c47 EKF: Eliminate call to hrt_absolute_time() 
This will make the library more portable
 2016-01-27 19:04:31 +11:00
Paul Riseborough 94a6644684 Add comprehensive user selectable GPS checks 2016-01-25 13:07:57 +11:00
Roman 8d0022ab1e enable estimator state and innovations data logging 2016-01-22 11:31:14 +01:00
Roman 86df68e404 added interface for parameters 2016-01-22 10:45:03 +01:00
nickolasrossi dfbbd36ff7 fix buffer overflow in constrain of wind velocity 2016-01-19 18:25:22 -08:00
Mark Charlebois 79bf35c4b3 Fixed printf of uint64_t 
Must use PRIu64 to prevent compiler errors.

Signed-off-by: Mark Charlebois <charlebm@gmail.com>
 2016-01-18 22:19:10 -08:00
Roman 0b5c90574c fix delta angle bias usage: 
the delta angle bias was applied to imu data which was not coming in the same
time intervall as the filter was operating. Therefore, the delta angle bias
applied to new imu data had to be scaled correctly in order to match
the imu time interval.
 2016-01-14 17:06:02 +01:00
Roman 2af5856361 initialise output height with baro 2016-01-08 06:59:10 +01:00
Roman a41f75ffb1 use full mag fusion 2016-01-08 06:59:10 +01:00
Roman f8354bb5e9 - do not fake vertical gps measurement as we have baro 
- formatting

Conflicts:
	EKF/ekf.cpp
 2016-01-08 06:59:10 +01:00
Roman 2a88fc6cfd initialise vertical position correctly 2016-01-08 06:42:22 +01:00
Roman 5aa5f7f8c3 use correct timestamp for measurements 2016-01-08 06:42:03 +01:00
Mark Charlebois b8837b4dc6 Added hexagon support 
std::to_string is not supported in the Hexagon complier

Signed-off-by: Mark Charlebois <charlebm@gmail.com>
 2016-01-07 14:54:55 -08:00
Paul Riseborough edfb7aefcc EKF: Fix initial alignment errors 
Use the gravity vector to estimate the initial roll and pitch angle
Use the projection of the magnetic field measurement onto the earth axis horizontal plane to calculate the initial heading
 2016-01-03 00:03:03 +11:00
Lorenz Meier 52cb9d02c7 EKF: Initialize all local structs and variables 2016-01-01 12:31:36 +01:00
Paul Riseborough 0cb210d045 EKF: Changes required to enter POSCTL mode 2016-01-01 11:56:38 +11:00
Lorenz Meier eda69e727f Do not print states by default 2015-12-24 13:48:22 +01:00
Roman 457a57c6ff use simple heading fusion 2015-12-22 18:00:59 +01:00
Lorenz Meier 6b49e2495c Fix field initializers 2015-12-22 17:25:08 +01:00
Lorenz Meier 8894786752 Estimator base: Fix printf formatting 2015-12-22 17:24:58 +01:00
Lorenz Meier faf48242ed EKF: Fix ringbuffer warnings 2015-12-22 17:24:43 +01:00
Roman 5e5d6f432a added static gps mode and init mag state correctly 2015-12-22 11:22:17 +01:00
Roman f153a7cb44 added ifdef guard 2015-12-19 09:40:32 +01:00
Roman Bapst d233ca3990 added complementary filter for real time state estimation 2015-12-10 16:36:10 +01:00
Roman Bapst 67646a15b0 added full mag fusion 2015-12-10 09:07:00 +01:00
Roman 8de8b0eb76 prediction and vel pos heading fusion working 2015-12-09 17:47:52 +01:00
Roman 921df43d32 added tests for EKF ringbuffer 2015-12-07 22:41:11 +01:00
Roman d90c8fd7c2 fixed bug in covariance prediction 2015-12-07 22:41:11 +01:00
Roman cfc39bc2f9 implemented prediction of states and covariance matrix 2015-12-07 22:41:11 +01:00
Roman b52e38eb9d fix 2015-12-07 22:41:11 +01:00
Roman cd5db8f494 enhance ringbuffer 2015-12-06 17:07:44 +01:00
Roman b3491bcfc3 added file with ekf helper functions 2015-12-06 13:19:25 +01:00
Roman 859502753d added file with covariance calculations 2015-12-06 13:10:49 +01:00
Roman Bapst 144aa9c461 added base class for data storage 2015-12-05 11:08:06 +01:00