George Hines
f467e714bd
add double support
2016-06-23 09:24:11 -07:00
George Hines
9994aa7fdb
fix a field name that I missed last time
2016-04-22 17:21:47 -07:00
George Hines
59df1a3552
rename log GUI consistent with its assumptions
2016-04-21 10:58:28 -07:00
George Hines
62bdcf3e9b
supports APM dataflash logs
2016-04-21 10:54:37 -07:00
George Hines
941d3bca0a
changes some graphics arguments for version compatibility, adds a viewer example to the usage samples script
2016-04-07 16:39:32 -07:00
George Hines
684b41494e
adds estimator log viewer UI
2016-04-07 15:13:19 -07:00
George Hines
3773d5a00d
removes accidentally commited px4log test file
2016-04-07 11:59:54 -07:00
George Hines
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
2016-04-07 11:58:51 -07:00
George Hines
2ad21bc8c7
adds function header comments and method attribution
2016-04-07 07:40:40 -07:00
George Hines
f6413a1924
renames test script for clarity
2016-04-07 07:32:53 -07:00
George Hines
93fde19c25
changes some cell notation for speed
2016-04-07 07:22:21 -07:00
George Hines
0e3a6e214c
completed low-overhead import script, added usage examples
2016-04-07 07:18:59 -07:00
George Hines
8c8653a1a2
initial commit of matlab px4 log importer
2016-04-06 17:12:40 -07:00
Lorenz Meier
f86ef34782
EKF: Fix error message which lied
2016-04-05 19:06:35 -07:00
Paul Riseborough
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.
2016-04-05 18:57:21 -07:00
Lorenz Meier
6b3ad03419
Merge pull request #86 from CarlOlsson/small_airspeed_fix
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Small airspeed fix
2016-04-05 16:38:37 -07:00
Roman Bapst
f35e78643c
Merge pull request #79 from dagar/integrator_fix
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fw multiply integrator gain in loop
2016-04-05 22:33:29 +02:00
Paul Riseborough
430d4b1cf8
EKF: ensure data in buffers is zero at startup
2016-04-05 22:23:37 +02:00
Paul Riseborough
c6bd93ed40
EKF: Include all output files generated by derivation script
2016-04-05 22:23:37 +02:00
Paul Riseborough
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
2016-04-05 22:23:37 +02:00
Paul Riseborough
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.
2016-04-05 22:23:37 +02:00
Paul Riseborough
03eac2f25e
EKF: Apply covariance prediction derivation changes
2016-04-05 22:23:37 +02:00
Paul Riseborough
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.
2016-04-05 22:23:37 +02:00
CarlOlsson
8678a939e2
removed reinitialization of intermediate variables
2016-04-05 14:18:47 +02:00
Roman Bapst
2632c930f7
Merge pull request #85 from CarlOlsson/add_error_reporting_tas
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added fault status reporting
2016-04-04 18:52:06 +02:00
Roman Bapst
96b9674cb6
Merge pull request #84 from CarlOlsson/change_to_true_airspeed
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change name to true_airspeed
2016-04-04 18:49:04 +02:00
CarlOlsson
eee6f1048f
Changed vtaspred threshold
2016-04-04 16:27:06 +02:00
CarlOlsson
3ad5b52aea
removed comment
2016-04-04 16:26:46 +02:00
CarlOlsson
616725410d
updated calculation
2016-04-04 16:26:13 +02:00
CarlOlsson
ec9902d802
added fault status reporting
2016-04-04 16:21:12 +02:00
CarlOlsson
1ea26b406a
change name to true_airspeed
2016-04-04 16:10:52 +02:00
Roman Bapst
068c29851c
Merge pull request #80 from PX4/fuse_tas_rebased
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Fuse tas rebased
2016-03-30 17:17:05 +02:00
Roman Bapst
27b894540e
put airspeed fusion logic but don't actually call it yet
2016-03-30 17:01:03 +02:00
Roman Bapst
1b7115dec9
increased airspeed fusion rate to 12.5Hz
2016-03-30 17:01:03 +02:00
CarlOlsson
f5a9afd278
moved init
2016-03-30 17:01:03 +02:00
CarlOlsson
f990d99790
fixed bug
2016-03-30 17:01:03 +02:00
CarlOlsson
4301e1105b
added commas
2016-03-30 17:01:03 +02:00
CarlOlsson
81fc086b76
adopted ekf_interface.h
2016-03-30 17:01:03 +02:00
CarlOlsson
d440c883b5
adopted ekf_interface.cpp
2016-03-30 17:01:03 +02:00
CarlOlsson
f8878d41dc
adopted ekf_helper.cpp
2016-03-30 17:01:03 +02:00
CarlOlsson
6bb2f7638c
adopted ekf.h
2016-03-30 17:01:03 +02:00
CarlOlsson
0918fa04c7
adopted ekf.cpp
2016-03-30 17:01:03 +02:00
CarlOlsson
92abf93c8f
adopted common.h
2016-03-30 17:01:03 +02:00
CarlOlsson
0fb1e0578b
added function for fusing airspeed
2016-03-30 17:01:03 +02:00
Daniel Agar
82cf1827d4
fw multiply integrator gain in loop
2016-03-25 17:28:39 -04:00
Paul Riseborough
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
2016-03-23 11:19:01 -07:00
Paul Riseborough
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.
2016-03-20 15:14:16 +11:00
Paul Riseborough
064a0e4dbc
EKF: Don't use GPS to set position noise when not using GPS
2016-03-16 20:12:36 +11:00
Paul Riseborough
c23d72ba29
EKF: Ensure filter control modes are correctly initialised
2016-03-16 17:22:27 +11:00
Paul Riseborough
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
2016-03-16 17:20:57 +11:00
