Tree: 342c3ab202

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1130 Commits (342c3ab202b62ef0d0ea45e6c98535934ac2674a)

 

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Author	SHA1	Message	Date
George Hines	93fde19c25	changes some cell notation for speed	9 years ago
George Hines	0e3a6e214c	completed low-overhead import script, added usage examples	9 years ago
George Hines	8c8653a1a2	initial commit of matlab px4 log importer	9 years ago
Lorenz Meier	f86ef34782	EKF: Fix error message which lied	9 years ago
Paul Riseborough	a352c2f4e3	EKF: Fix posix build error ... Memset cannot be used on a class like this. Setting the time elements to zero achieves the desired result.	9 years ago
Lorenz Meier	6b3ad03419	Merge pull request #86 from CarlOlsson/small_airspeed_fix ... Small airspeed fix	9 years ago
Roman Bapst	f35e78643c	Merge pull request #79 from dagar/integrator_fix ... fw multiply integrator gain in loop	9 years ago
Paul Riseborough	430d4b1cf8	EKF: ensure data in buffers is zero at startup	9 years ago
Paul Riseborough	c6bd93ed40	EKF: Include all output files generated by derivation script	9 years ago
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	9 years ago
Paul Riseborough	eaf94935f0	EKF: Fix bug in initialisation of height and magnetic field ... This prevents zero data being used to form the initial height and magnetic field. Do not start sampling initial values until non-zero time values are retrieved from the buffer.	9 years ago
Paul Riseborough	03eac2f25e	EKF: Apply covariance prediction derivation changes	9 years ago
Paul Riseborough	ac71ec5d37	EKF: Fix scaling error in covariance prediction derivation ... The covariance prediction derivation was using the noise 1-std value instead of the noise variance. This resulted in the values of IMU process noise required to tune not matching the observed covariance growth.	9 years ago
CarlOlsson	8678a939e2	removed reinitialization of intermediate variables	9 years ago
Roman Bapst	2632c930f7	Merge pull request #85 from CarlOlsson/add_error_reporting_tas ... added fault status reporting	9 years ago
Roman Bapst	96b9674cb6	Merge pull request #84 from CarlOlsson/change_to_true_airspeed ... change name to true_airspeed	9 years ago
CarlOlsson	eee6f1048f	Changed vtaspred threshold	9 years ago
CarlOlsson	3ad5b52aea	removed comment	9 years ago
CarlOlsson	616725410d	updated calculation	9 years ago
CarlOlsson	ec9902d802	added fault status reporting	9 years ago
CarlOlsson	1ea26b406a	change name to true_airspeed	9 years ago
Roman Bapst	068c29851c	Merge pull request #80 from PX4/fuse_tas_rebased ... Fuse tas rebased	9 years ago
Roman Bapst	27b894540e	put airspeed fusion logic but don't actually call it yet	9 years ago
Roman Bapst	1b7115dec9	increased airspeed fusion rate to 12.5Hz	9 years ago
CarlOlsson	f5a9afd278	moved init	9 years ago
CarlOlsson	f990d99790	fixed bug	9 years ago
CarlOlsson	4301e1105b	added commas	9 years ago
CarlOlsson	81fc086b76	adopted ekf_interface.h	9 years ago
CarlOlsson	d440c883b5	adopted ekf_interface.cpp	9 years ago
CarlOlsson	f8878d41dc	adopted ekf_helper.cpp	9 years ago
CarlOlsson	6bb2f7638c	adopted ekf.h	9 years ago
CarlOlsson	0918fa04c7	adopted ekf.cpp	9 years ago
CarlOlsson	92abf93c8f	adopted common.h	9 years ago
CarlOlsson	0fb1e0578b	added function for fusing airspeed	9 years ago
Daniel Agar	82cf1827d4	fw multiply integrator gain in loop	9 years ago
Paul Riseborough	0ea55e25f9	Merge pull request #78 from PX4/pr-addGpsHgtOption ... EKF: Add option to use GPS for height and improve height fall-back behaviour	9 years ago
Paul Riseborough	400a6e12ba	EKF: Ensure all data in buffers is initialised ... This is a defensive change to prevent introduction of NaN's into the filter if data is read from the incorrect place in the buffer.	9 years ago
Paul Riseborough	064a0e4dbc	EKF: Don't use GPS to set position noise when not using GPS	9 years ago
Paul Riseborough	c23d72ba29	EKF: Ensure filter control modes are correctly initialised	9 years ago
Paul Riseborough	9f3b1351f7	EKF: Don't initialise velocity to GPS on initial alignment ... For initial alignment the velocity and position should start at zero	9 years ago
Paul Riseborough	687fcc70be	EKF: Explicitly define type conversion for GPS height	9 years ago
Paul Riseborough	e334a5dc57	EKF: Add check for NaN's on attitude states	9 years ago
Paul Riseborough	6b2e2dba90	EKF: Add GPS height option and improve height recovery	9 years ago
Paul Riseborough	63b0cf4360	EKF: Fix baro height offset bug	9 years ago
Paul Riseborough	4bd79c9e5d	Merge pull request #76 from PX4/pr-fixRngHgtMode ... EKF: Fix bugs preventing use of range finder as primary height source Flight testing completed and I have checked that the other pending PR #75 rebases cleanly on it.	9 years ago
Paul Riseborough	49023f3d7e	EKF: fix travis build error	9 years ago
Paul Riseborough	7677a162aa	EKF: Don't start the output observer before the main filter has initialised ... This prevents the possibility of output transients if alignment is delayed.	9 years ago
Paul Riseborough	d2407c3463	EKF: code style updates	9 years ago
Paul Riseborough	c58ab3e256	EKF: Enable fallback to baro alt when using range finder for height	9 years ago
Paul Riseborough	370f643f42	EKF: Enable use of range finder for primary height source	9 years ago