af5bbc916c
ekf2: Enable user defeatible saving of declination for next startup
2016-02-15 12:52:49 +01:00
2ca48037fd
ekf2: Add mavlink adjustable parameters for control of magnetometer fusion
2016-02-15 12:52:49 +01:00
11df8168ee
provide ekf2 with landed flag from landing detector
2016-02-14 21:26:47 +01:00
2177c0e18a
ekf2: remove unused print functions
2016-02-14 20:51:01 +01:00
3edf304e55
EKF2: Fix home altitude reporting
2016-02-10 08:38:03 +01:00
fcf642fe4e
fixed bad formating of ekf2 CMakeFile
2016-02-05 18:28:32 +01:00
371e5f70b1
ekf2: fix formatting
2016-02-05 18:28:32 +01:00
a37daf4cec
ekf2: Add position observation noise parameter for 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).
2016-02-05 18:28:32 +01:00
8f020d5a8f
ekf2: 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).
Update documentation and display names for consistency.
2016-02-05 18:28:32 +01:00
c75cc75d25
ekf2 module: be consistent in constructor
2016-01-31 22:28:19 +01:00
0f43a1ebbb
ekf2: fix code style
2016-01-31 22:12:11 +01:00
04ad8ca594
ekf: change the name of estimatorr interface class
2016-01-31 22:12:11 +01:00
92f0032475
ekf2: Add tuning parameters for GPS and Baro innovation gates
2016-01-31 22:12:11 +01:00
6ffcca4b8f
ekf2_main: fix variable pass type
2016-01-31 22:12:11 +01:00
92f2492fff
ekf2: update interface method for vehicle arm status and NED origin
2016-01-31 22:12:11 +01:00
4594b3c69d
ekf2: Add parameters for magnetometer error checks
2016-01-31 22:12:11 +01:00
5e4f76d844
ekf2: Add parameters and support for GPS quality checks
2016-01-31 22:12:11 +01:00
563460444a
ekf2: get the rad to deg conversion right
2016-01-25 19:03:16 +01:00
28754d3f58
ekf2: don't reset GPS position in every loop
2016-01-25 19:03:16 +01:00
c185a12c8e
log ekf2 innovations and innovation variances
2016-01-22 14:24:36 +01:00
21f7641e8d
log ekf2 estimator status
2016-01-22 14:24:36 +01:00
7452cfdf63
EKF2: Fix polling code
2016-01-22 14:21:19 +01:00
1cfa9d924d
Fixed ekf2 stop / start routine
2016-01-22 12:07:17 +01:00
c32938d2a8
EKF2: Update params only as they change
2016-01-22 11:45:29 +01:00
93a9032f87
ekf2: parameter cleanup
2016-01-22 11:40:35 +01:00
e6d2d17109
initialise topic structs properly
2016-01-21 07:25:18 +01:00
0510d2cb56
fixed code style
2016-01-10 21:14:58 +01:00
fe07079367
added parameter interface to ekf2
2016-01-10 21:14:58 +01:00
276855acd2
EKF2: Remove todo
2016-01-01 11:39:16 +01:00
28f5cb8fe6
ekf2: Changes required to enter POSCTL mode
...
Adds missing local position and global position data
2016-01-01 12:30:12 +11:00
b958928095
publish rates and quaternion on attitude topic
2015-12-23 11:40:25 +01:00
2d50002973
Fix stack settings of EKF2
2015-12-23 06:23:16 +01:00
979cda1b10
Add dependency to ECL to CMake
2015-12-23 06:23:16 +01:00
07abac3ea4
ekf2 publish attitude position and control state
2015-12-23 06:23:15 +01:00
63ac712eab
allow testing ekf2 in simulation with jmavsim
2015-12-23 06:23:15 +01:00
19a5f9e73d
updated ecl lib
2015-12-23 06:23:15 +01:00
Paul Riseborough