dark0707
/
px4-firmware
forked from Archive/PX4-Autopilot
1
0
Fork 0
Code Pull Requests Activity
1,521 Commits 514 Branches 136 Tags 234 MiB
Commit Graph

190 Commits

Author SHA1 Message Date
Paul Riseborough 3758c5a09d EKF: down-sample drag specific force data 2017-04-16 13:07:12 +02:00
Paul Riseborough 5cf31e439d EKF: Add specific drag fusion tuning parameters 2017-04-16 13:07:12 +02:00
Paul Riseborough 465b145929 EKF: Add multi-rotor drag model for wind estimation 2017-04-16 13:07:12 +02:00
Paul Riseborough 7b996c5972 EKF: Increase measurement error allowance for accelerometer clipping 2017-04-07 16:37:27 +10:00
Paul Riseborough f0bbbc8dc6 EKF: Add reporting of bad accel status 2017-04-07 08:47:13 +10:00
Paul Riseborough 2f2ac5be43 EKF: Improve protection against severe IMU accel errors 
Use vertical velocity and position innovation failure to detect bad accelerometer data caused by clipping or aliasing which can cause large vertical acceleration errors and loss of height estimation. When bad accel data is detected:

1) Inhibit accelerometer bias learning
2) Force fusion of vertical velocity and height data
3) Increase accelerometer process noise
 2017-04-07 08:47:13 +10:00
Paul Riseborough 040639837e EKF: Use common timeout test for reporting deadreckoning 
Use a parameter to set the time-out threshold
Use a class variable for the time-out flag
Clean up comments
 2017-03-15 07:57:38 +01:00
Paul Riseborough 588b27bde7 EKF: inhibit accelerometer bias learning if manoeuvre levels are excessive 
This prevents bad scale factors and other errors associated with rapid manoeuvres corrupting the accelerometer bias estimates.
 2017-03-10 10:14:06 +01:00
Paul Riseborough 324fe3b0c7 EKF: Add accel bias estimation fault to reporting 2017-03-10 10:14:06 +01:00
Paul Riseborough cf31945038 EKF: Fix use of incorrect timestamp 
This was incorrectly using the IMU (1/250 sec) timestamp instead of the EKF (1/100 sec) value.
The corresponding accelerometer limit has been made a parameter and adjusted to match previous behaviour.
 2017-03-10 10:14:06 +01:00
Paul Riseborough 3dadc98b43 EKF: enable scaling of range observation variance with height 2017-02-22 14:12:05 +01:00
Paul Riseborough cf9c8de167 EKF: Add arbitrary pitch offset for range sensor 2017-02-22 14:12:05 +01:00
Paul Riseborough 3b61528f0f EKF3: initialise default value for EV fusion gate 2017-01-15 10:02:31 +01:00
Lorenz Meier bf8a9a3d09 EKF: Whitespace fixes 2016-12-17 13:45:28 +01:00
Paul Riseborough d5b398ddb1 EKF: Minimise data buffer lengths 
Saves RAM and reduces output predictor errors by using the smallest data buffer length that meets time delay and update rate requirements.
 2016-11-07 09:06:45 +11:00
Paul Riseborough 6c7703d485 EKF: Update tuning for synthetic sideslip fusion 
Used value that worked well for replay of flight logs
 2016-11-05 12:19:01 +01:00
CarlOlsson dec686afd7 updated parameters 2016-11-05 12:19:01 +01:00
CarlOlsson beb90f008d adopted code for upstream changes 2016-11-05 12:19:01 +01:00
CarlOlsson 738414d36e adopted common.h 2016-11-05 12:19:01 +01:00
Roman c5f750dcca ekf reset: more granular reset / timeout strategy for gps fusion 
- if both gps position and velocity measurements are rejected for 7 seconds
do a reset
- if only gps position measurements are rejected then wait for 14 seconds
as we still have velocity measurements to constrain the drift in position
- introduced ecl internal parameter for the timeout

Signed-off-by: Roman <bapstroman@gmail.com>
 2016-10-24 11:40:12 +02:00
Paul Riseborough 1093e6d789 EKF: fix documentation error 2016-10-13 22:37:14 +02:00
Paul Riseborough 352750e5d1 EKF: publish ekf solution status summary data 2016-10-06 09:02:29 +02:00
Paul Riseborough b5ba4f280f EKF: reduce output predictor velocity time constant 2016-10-03 14:13:07 +11:00
Beat Küng 9a95898414 gps_message: remove time_usec_vel from struct (unused) 2016-06-27 10:12:23 +02:00
Roman Bapst 1b394460a3 fix comment about filter bias states 
Signed-off-by: Roman Bapst <roman@px4.io>
 2016-06-21 14:13:47 +02:00
Paul Riseborough 65da9173b9 EKF: capture innovation checks and reset events in separate variables 
rename the innovation check status class variable and remove the reset flags from it.
 2016-06-01 17:13:00 +10:00
Paul Riseborough 106482b078 EKF: add structure to capture innovation test failures and state resets 2016-06-01 17:13:00 +10:00
Paul Riseborough 1b6c5bbafd EKF: Enable height source to be selected independent of EV aiding 2016-05-27 13:14:52 +10:00
Paul Riseborough e41524ac9d EKF: remove unused variables 2016-05-27 11:21:04 +10:00
Paul Riseborough 57b2a256f7 EKF: Improve initialisation of quaternion covariances 
Convert uncertainty in initial rotate vector into quaternion covariances using symbolic toolbox derived expressions.
Enable setting of initial angle uncertainty via a parameter
 2016-05-17 12:47:20 +10:00
Paul Riseborough 88860d0307 EKF: Enable tuning for IMU switch on bias errors 2016-05-17 11:17:24 +10:00
Paul Riseborough 920d83d68c EKF: Fix bugs preventing use of external vision yaw data 2016-05-14 21:56:41 +10:00
devbharat b681c9a5d0 Added external vision noise parameters etc and position offset 2016-05-14 21:17:29 +10:00
devbharat ff8f03b5dd Added compensation for VI sensor offset. Check sign. 2016-05-14 21:17:29 +10:00
Paul Riseborough e917d6c7f2 EKF: Add fusion of external yaw data 2016-05-14 21:17:29 +10:00
Paul Riseborough 81469d6621 EKF: Add position, height and velocity reset for EV aiding 2016-05-14 21:17:29 +10:00
Paul Riseborough 3a0fcd03d7 EKF: Add interfaces and variables to use ext vision data 2016-05-14 21:17:29 +10:00
Paul Riseborough c7e225124c EKF: Improve output observer position and velocity tracking 
Replace the delayed time feedback mechanism used by the translational states with a direct feedback method.
Time constants for velocity and position convergence can be separately adjusted with tunable parameters
The method is more computationally more expensive because it requires modification of the output buffer history but is acceptable because it only requires 6 FLOP per buffer index for a total of 30*6 = 180 FLOP
The method was not applied to the attitude states because the quaternion operations required at each buffer index would have been computationally prohibitive.
 2016-05-14 12:45:29 +09:30
Carl Olsson b126921894 changed airspeed innovation gate to 5 (#119) 2016-05-12 10:05:26 +02:00
Paul Riseborough 1a24ec5f50 EKF: remove unused flag from control status message 2016-05-10 10:45:06 +10:00
Paul Riseborough 2144a40a3c EKF: redefine accelerometer bias state inhibit switch bit location 2016-05-08 16:03:21 +10:00
Paul Riseborough 020b87933e EKF: replace fault status struct with a union to facilitate logging 2016-05-07 21:11:16 +10:00
Paul Riseborough 310bd97080 EKF: Improve protection against bad pos vel fusion 2016-05-07 14:22:59 +10:00
Paul Riseborough d9aeace6ac EKF: tuning update 2016-05-05 21:23:03 +10:00
Paul Riseborough 1daa6c7866 EKF: update tuning defaults 2016-05-05 21:23:03 +10:00
Paul Riseborough fc6c0c7ebf EKF: Update covariance prediction 
Refresh auto generated code
Make 3-axis accel fusion the default and no accel fusion the option
 2016-05-05 21:23:03 +10:00
Paul Riseborough ecaffe63af EKF: update tuning defaults 2016-05-05 21:23:03 +10:00
Paul Riseborough 29a361d3a3 EKF: Use intuitive units for gyro and accel bias process noise 
This also makes the tuning less sensitive to changes in the EKF update rate.
 2016-05-05 21:23:03 +10:00
Paul Riseborough 799865c934 EKF: update default tuning parameters 2016-05-05 21:23:03 +10:00
Paul Riseborough 311d046a26 EKF: Enable optional activation of XY delta velocity bias estimation 2016-05-05 21:23:03 +10:00
Paul Riseborough 67d23948b5 EKF: preliminary re-tune 2016-05-05 21:23:03 +10:00
Paul Riseborough 03c35266ef EKF: remove unused parameter 2016-05-05 21:23:03 +10:00
Paul Riseborough fe9f88a8b4 EKF: test new derivation 
Use direct attitude parameterisation
Discard scale factors
Add accel bias
 2016-05-05 21:23:03 +10:00
Paul Riseborough e3365525c2 EKF: rework height reset logic 2016-04-22 08:39:24 +10:00
Roman Bapst 99fc61c27c ekf2 airspeed fusion: 
- finished logic for fusion
- fixed bug where previous control status was set in the wrong location
 2016-04-19 09:53:31 +02:00
Lorenz Meier 3455931617 EKF init: Fix initialization statement 2016-04-17 19:29:23 +02:00
Paul Riseborough ea38aa130f EKF: update default time delay parameter values 2016-04-14 08:53:59 +10:00
Paul Riseborough b46053415f EKF: Compensate optical flow data for sensor position offset 2016-04-12 11:14:31 +10:00
Paul Riseborough 3580940e10 EKF: Add sensor position offset parameters 2016-04-12 11:14:31 +10:00
Paul Riseborough 470098e182 EKF: update default tuning parameters 
Parameters needed to be changed when covariance prediction error was corrected.
The magnetic earth and body field process noise now use separate parameters to help with tuning
 2016-04-05 22:23:37 +02:00
CarlOlsson 1ea26b406a change name to true_airspeed 2016-04-04 16:10:52 +02:00
CarlOlsson f990d99790 fixed bug 2016-03-30 17:01:03 +02:00
CarlOlsson 92abf93c8f adopted common.h 2016-03-30 17:01:03 +02:00
Paul Riseborough 6b2e2dba90 EKF: Add GPS height option and improve height recovery 2016-03-16 10:40:51 +11:00
Paul Riseborough eab0ef4266 EKF: Update default process noise for terrain estimator 2016-03-11 11:03:43 +11:00
Paul Riseborough 962fd0aaf2 EKF: Adjust terrain process noise for gradient effect 2016-03-11 11:03:43 +11:00
Paul Riseborough 5acd1cbac4 EKF: Make definitions of parameters clearer for external use 2016-03-11 11:03:43 +11:00
Paul Riseborough b3b0f1347a EKF: Make normal GPS mode the default 2016-03-11 11:03:43 +11:00
Paul Riseborough dca186c6e8 EKF: Add required declarations for optical flow 2016-03-11 11:03:43 +11:00
Paul Riseborough 57d4064d7b EKF: Increase default heading observation noise 
Improves robustness when operating in a bad magnetic field environment
 2016-03-01 15:28:53 +11:00
Paul Riseborough f55a0bff53 EKF: Fix code style 2016-02-25 08:17:50 +11:00
mcsauder f9f00fa52b Remove unnecessary include. 2016-02-23 14:00:39 -07:00
mcsauder 79d07c831f Convert spaces to tabs to match upstream. 2016-02-23 19:53:55 -07:00
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
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 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
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 7da40a45a4 EKF: Add control mode for wind state estimation 2016-02-16 11:08:30 +11:00
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 0308f2f796 EKF: Add parameters to control declination source and fusion type 2016-02-14 22:01:53 +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 47ab5ebcdd EKF: Make PR comply with project convention for indenting 2016-02-08 15:12:38 +11:00
Paul Riseborough 6aeccf01ff EKF: Add missing fusion health status messages 2016-02-08 14:18:43 +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 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
bugobliterator d79e12dfa1 EKF: fix code style 2016-01-31 00:12:16 -08:00
bugobliterator 287f5eb0c2 EKF: move all estimator specific types to common header 2016-01-30 12:44:19 -08:00