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

74 Commits

Author SHA1 Message Date
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