CarlOlsson
c8e3c24150
adopted ekf_helper.cpp
2016-11-05 12:19:01 +01:00
Paul Riseborough
b10b0184c5
EKF: Add IMU vibration calculation and reporting
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Add calculation and reporting of IMU delta angle and velocity coning and high frequency vibration
2016-10-19 21:46:55 +11:00
Roman
17c195d1cd
ekf2 height reset: do not apply height change to height state twice (bug)
...
Signed-off-by: Roman <bapstroman@gmail.com>
2016-10-18 07:58:19 +02:00
Roman
f80b3481a4
reset the newest output sample for all possible resets
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Signed-off-by: Roman <bapstroman@gmail.com>
2016-10-12 08:54:38 +02:00
Roman
238d947239
proper handling of position and velocity reset
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- position reset method was returning before the actual delta values
were written and applied to the output buffer
- apply reset delta also to the output sample which was already taken out
from the output buffer, otherwise the complementary filter solution is
offset from the ekf solution
Signed-off-by: Roman <bapstroman@gmail.com>
2016-10-12 08:54:38 +02:00
Paul Riseborough
352750e5d1
EKF: publish ekf solution status summary data
2016-10-06 09:02:29 +02:00
Paul Riseborough
007e73379f
EKF: Improve reporting of position error
2016-10-06 09:02:29 +02:00
Paul Riseborough
744b79c1b2
EKF: Publish innovation test ratios
2016-10-06 09:02:29 +02:00
Paul Riseborough
65762e5998
EKF: publish output predictor tracking errors
2016-10-03 14:13:07 +11:00
Julian Oes
616aeb9ad7
ekf_helper: fix forgotten return value
2016-09-27 16:36:29 +02:00
Beat Küng
73b8ac954d
ekf_helper.cpp: remove unused includes
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This fixes a compile error with GCC 5.2.0 and cross-compilation:
/usr/arm-none-eabi/include/c++/5.2.0/arm-none-eabi/armv7e-m/fpu/bits/error_constants.h:122:27: error: 'ENOTSUP' was not declared in this scope
not_supported = ENOTSUP,
The problem was that the #include <iomanip> was taken from the host system,
which conflicts with includes from NuttX (NuttX has only basic C++ STL
support)
2016-07-15 12:50:11 +02:00
Paul Riseborough
f5e9ea1626
EKF: Prevent potential divide by zero
2016-06-30 17:06:32 +10:00
Paul Riseborough
7bc9217f00
EKF: Clean up control of observation fusion
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All the decision for a sensor are made within a specific function for that sensor and when there is data to process at the fusion time horizon.
Information and warning messages are improved.
2016-06-30 17:06:32 +10:00
Roman Bapst
bec1a6831e
added method to get gyro bias
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Signed-off-by: Roman Bapst <roman@px4.io>
2016-06-21 14:13:47 +02:00
Roman
703fb4e31b
do not return early in velocity reset method otherwise
...
some code will not be executed
2016-06-08 07:51:18 +02:00
Paul Riseborough
f26aca55a1
EKF: Fix bug in quaternion covariance initialisation function
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The covariances between quaternion and non-quaternion states were not being updated
2016-06-08 13:23:30 +10:00
Paul Riseborough
6a55d908c5
EKF: replace reset event times with event counters
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Using a 64bit integer was unnecessary given it was only being used to detect a new reset event.
2016-06-01 17:13:00 +10:00
Paul Riseborough
9ec09f5f4e
EKF: update output observer and capture reset event for magnetic heading resets
2016-06-01 17:13:00 +10:00
Paul Riseborough
aca0336392
EKF: update vertical position and velocity reset capture
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Use reset event struct members instead of separate variables
2016-06-01 17:13:00 +10:00
Paul Riseborough
0605c88ecc
EKF: capture horizontal position reset events
2016-06-01 17:13:00 +10:00
Paul Riseborough
e3a1b4a3b3
EKF: capture velocity reset events
2016-06-01 17:13:00 +10:00
Paul Riseborough
79705da7e6
EKF: make output predictor states consistent with position reset
2016-06-01 17:13:00 +10:00
Paul Riseborough
54d90261d5
EKF: make output predictor states consistent with velocity reset
2016-06-01 17:13:00 +10:00
Paul Riseborough
ad02818b3d
EKF: Improve height reset for external vision
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reset to measurement closest in time to fusion time horizon
2016-05-27 14:00:50 +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
ae5071f668
EKF: Improve heading reset
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Improves reset of quaternion covariance matrix after a heading reset by preserving variance in roll and pitch and resetting yaw variance to the measurement variance.
2016-05-21 19:30:15 +10:00
Paul Riseborough
94a63ec9d5
EKF: don't interfere with quaternion covariances during tilt alignment
2016-05-18 19:25:19 +10:00
Paul Riseborough
e4b2e9c93d
EKF: Improve yaw alignment
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Uses best conditioned of 321 or 312 Euler sequence to calculate initial yaw angle.
Allows alignment of yaw angle using external vision data
2016-05-18 12:16:16 +10:00
Paul Riseborough
57b2a256f7
EKF: Improve initialisation of quaternion covariances
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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
1540e937b1
EKF: Improve tilt alignment monitoring
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Convert quaternion covariances into an angular alignment variance vector and discard the z component so that yaw uncertainty does not affect the result.
2016-05-17 11:17:24 +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
25682dce91
EKF: Prevent badly conditioned covariance calculation when starting or resetting to optical flow
2016-05-08 10:30:40 +10:00
Paul Riseborough
7f5669fb2d
EKF: consolidate covariance corrections
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Combines the forced symmetry, variance limiting and zeroing of covariances for unwanted states in the one function.
This ensures a consistent correction is applied after every covariance prediction or correction.
2016-05-07 20:29:50 +10:00
Paul Riseborough
da9d894441
EKF: Improvements to covariance reset
2016-05-07 12:57:41 +10:00
Paul Riseborough
fe9f88a8b4
EKF: test new derivation
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Use direct attitude parameterisation
Discard scale factors
Add accel bias
2016-05-05 21:23:03 +10:00
Roman
0c77ebf6bd
EKF: Reduce likelihood of bad covariance values after height resets
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The cross terms (covariances) are now reset before the variance variance is set.
The vertical velocity state variance following a reset without GPS has been reduced.
2016-05-01 21:39:56 +10:00
Paul Riseborough
469a7d1711
EKF: rework height reset
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calculate and save the amount that the vertical states have changed and the time of the change
apply the change delta to the output observer states and buffer
2016-04-22 08:43:56 +10:00
Paul Riseborough
2fa8a11a29
EKF: replace unnecessary memcopy
2016-04-19 19:10:41 +10:00
Paul Riseborough
31bf342fc1
EKF: publish GPS check status
2016-04-19 17:38:22 +10:00
Paul Riseborough
e10093854a
EKF: correct outputs for IMU offset
2016-04-12 11:14:31 +10:00
Paul Riseborough
74078cde94
EKF: reset state variance when performing a height reset
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Set vertical position and velocity variances using known sensor error characteristics if we have reset the states to the sensor readings.
2016-04-11 19:40:27 +10:00
Paul Riseborough
f4f108d57d
EKF: Reset vertical velocity when performing a height reset
2016-04-11 19:25:24 +10:00
CarlOlsson
f8878d41dc
adopted ekf_helper.cpp
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
c58ab3e256
EKF: Enable fallback to baro alt when using range finder for height
2016-03-13 21:17:51 +11:00
Paul Riseborough
370f643f42
EKF: Enable use of range finder for primary height source
2016-03-13 18:44:34 +11:00
Paul Riseborough
e0fcce1463
EKF: Make position and velocity reset publish success
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Some users of the position and velocity reset functions will need to know if the reset has been successful.
2016-03-11 11:03:43 +11:00
Paul Riseborough
32b03819ef
EKF: Add function to calculate global position validity
2016-03-11 11:03:43 +11:00
Paul Riseborough
270451e17b
EKF: Update height reset to support range finder height use
2016-03-11 11:03:43 +11:00
Paul Riseborough
f7a53d69f2
EKF: Improve height reset function
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Add a method to reset the vertical velocity to enable in-flight resets
Reset to GPS height if baro height is not available.
2016-03-02 08:39:07 +01:00