1624 Commits

Author SHA1 Message Date
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
Roman Bapst
d21ce70eeb Merge pull request #45 from CarlOlsson/move_fuse_function_to_helper
moved fuse function to ekf_helper.cpp
2016-02-13 08:21:28 +01:00
CarlOlsson
1e766c7510 moved fuse function to ekf_helper.cpp 2016-02-12 15:54:32 +01:00
Lorenz Meier
0a9f7e58db Merge pull request #43 from PX4/pr-baroHeightOffset
Correct for sensor noise and baro offset during alignment
2016-02-10 08:02:48 +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
a6515543da Merge pull request #41 from PX4/pr-magFusionUpdates
EKF2: Prevent declination/heading drift during non-GPS operation
2016-02-09 07:57:34 +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
a22886544d EKF: Add missing Kalman gain to Declination fusion autocode 2016-02-08 14:02:08 +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
42a943b37e EKF: Fix text errors introduced when editing optical flow fusion autocode fragment 2016-02-07 21:49:50 +11:00
Paul Riseborough
f99256286b Merge pull request #40 from PX4/pr-updateOpticalFlowAutoCode
Update EKF Optical Flow Fusion Autocode Fragments
2016-02-07 19:35:38 +11:00
Paul Riseborough
384ce06110 EKF: Add alternative code fragments for optical flow fusion
These fragments were generated using the inbuilt matlab symbolic toolbox autocoder and may be more efficient than the other method
2016-02-07 19:31:13 +11:00
Paul Riseborough
dba462b9f3 EKF: Improve efficiency of optical flow fusion auto generated code fragments 2016-02-07 19:29:49 +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