eb41d25ff6
reduces update rate of progress display, stores message time (not TIME message) as floating point seconds, automatically extracts TIME message, updates usage samples accordingly
9 years ago
2ad21bc8c7
adds function header comments and method attribution
9 years ago
f6413a1924
renames test script for clarity
9 years ago
93fde19c25
changes some cell notation for speed
9 years ago
0e3a6e214c
completed low-overhead import script, added usage examples
9 years ago
8c8653a1a2
initial commit of matlab px4 log importer
9 years ago
f86ef34782
EKF: Fix error message which lied
9 years ago
a352c2f4e3
EKF: Fix posix build error
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Memset cannot be used on a class like this. Setting the time elements to zero achieves the desired result.
9 years ago
6b3ad03419
Merge pull request #86 from CarlOlsson/small_airspeed_fix
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Small airspeed fix
9 years ago
f35e78643c
Merge pull request #79 from dagar/integrator_fix
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fw multiply integrator gain in loop
9 years ago
430d4b1cf8
EKF: ensure data in buffers is zero at startup
9 years ago
c6bd93ed40
EKF: Include all output files generated by derivation script
9 years ago
470098e182
EKF: update default tuning parameters
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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
eaf94935f0
EKF: Fix bug in initialisation of height and magnetic field
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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
03eac2f25e
EKF: Apply covariance prediction derivation changes
9 years ago
ac71ec5d37
EKF: Fix scaling error in covariance prediction derivation
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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
8678a939e2
removed reinitialization of intermediate variables
9 years ago
2632c930f7
Merge pull request #85 from CarlOlsson/add_error_reporting_tas
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added fault status reporting
9 years ago
96b9674cb6
Merge pull request #84 from CarlOlsson/change_to_true_airspeed
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change name to true_airspeed
9 years ago
eee6f1048f
Changed vtaspred threshold
9 years ago
3ad5b52aea
removed comment
9 years ago
616725410d
updated calculation
9 years ago
ec9902d802
added fault status reporting
9 years ago
1ea26b406a
change name to true_airspeed
9 years ago
068c29851c
Merge pull request #80 from PX4/fuse_tas_rebased
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Fuse tas rebased
9 years ago
27b894540e
put airspeed fusion logic but don't actually call it yet
9 years ago
1b7115dec9
increased airspeed fusion rate to 12.5Hz
9 years ago
f5a9afd278
moved init
9 years ago
f990d99790
fixed bug
9 years ago
4301e1105b
added commas
9 years ago
81fc086b76
adopted ekf_interface.h
9 years ago
d440c883b5
adopted ekf_interface.cpp
9 years ago
f8878d41dc
adopted ekf_helper.cpp
9 years ago
6bb2f7638c
adopted ekf.h
9 years ago
0918fa04c7
adopted ekf.cpp
9 years ago
92abf93c8f
adopted common.h
9 years ago
0fb1e0578b
added function for fusing airspeed
9 years ago
82cf1827d4
fw multiply integrator gain in loop
9 years ago
0ea55e25f9
Merge pull request #78 from PX4/pr-addGpsHgtOption
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EKF: Add option to use GPS for height and improve height fall-back behaviour
9 years ago
400a6e12ba
EKF: Ensure all data in buffers is initialised
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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
064a0e4dbc
EKF: Don't use GPS to set position noise when not using GPS
9 years ago
c23d72ba29
EKF: Ensure filter control modes are correctly initialised
9 years ago
9f3b1351f7
EKF: Don't initialise velocity to GPS on initial alignment
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For initial alignment the velocity and position should start at zero
9 years ago
687fcc70be
EKF: Explicitly define type conversion for GPS height
9 years ago
e334a5dc57
EKF: Add check for NaN's on attitude states
9 years ago
6b2e2dba90
EKF: Add GPS height option and improve height recovery
9 years ago
63b0cf4360
EKF: Fix baro height offset bug
9 years ago
4bd79c9e5d
Merge pull request #76 from PX4/pr-fixRngHgtMode
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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
49023f3d7e
EKF: fix travis build error
9 years ago
7677a162aa
EKF: Don't start the output observer before the main filter has initialised
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This prevents the possibility of output transients if alignment is delayed.
9 years ago
George Hines
Lorenz Meier
Paul Riseborough
Lorenz Meier
Roman Bapst
CarlOlsson
Daniel Agar
Paul Riseborough