analyse_logdata_ekf:
- add sideslip innovation fail check flag to fix wrongly selected
bits for hagl innovation and optical flow innovations
- plot sideslip innovation fail
- add gps fix type fail flag to fix wrongly selected bits for all
gps check fail flags
- plot gps fix type
- ecl in PX4/Firmware (f7937d783496e954efc52439148ef66824d9c80a): https://github.com/PX4/ecl/commit/1fdf33b343e361de6410515a0359f3cb7f34d499
- ecl current upstream: https://github.com/PX4/ecl/commit/d177e96508d2572f6fa8eb7ff41852749c882548
- Changes: https://github.com/PX4/ecl/compare/1fdf33b343e361de6410515a0359f3cb7f34d499...d177e96508d2572f6fa8eb7ff41852749c882548d177e96 2018-06-08 Paul Riseborough - EKF: Fix bug causing slow drift when high rate flow data is used
ee2dc7d 2018-05-30 Paul Riseborough - EKF: Rework optical flow selection logic
e383b6a 2018-05-29 Paul Riseborough - EKF: rework optical flow selection logic
487e6a0 2018-05-28 Paul Riseborough - EKF: enable user selection of auto mag free operation
6bdbe03 2018-05-28 Paul Riseborough - EKF: Fallback to optical flow for all in-flight loss of navigation scenarios
b4d2b8c 2018-05-19 Mohammed Kabir - EKF : introduce new architechture for navigation limits
8a71339 2018-05-19 Paul Riseborough - EKF: Improve ground effect compensation
39697f1 2018-05-18 Paul Riseborough - EKF: rework optical flow switching
1cfe845 2018-05-18 Paul Riseborough - EKF: rework GPS quality check
99a8038 2018-05-18 Paul Riseborough - EKF: improve optical flow GPS quality checking
7f36add 2018-05-18 Paul Riseborough - EKF: scale GPS vertical accuracy check when using optical flow
fc9f532 2018-05-18 Paul Riseborough - EKF: relax range finder data continuity check
93c456f 2018-05-18 Paul Riseborough - EKF: Improve protection against badly conditioned dVel bias covariances
225057a 2018-05-18 Paul Riseborough - EKF: Fix bug preventing use of terrain estimator
adb4a09 2018-05-17 Paul Riseborough - EKF: Fix bug causing large yaw innovations when GPS is lost
f59cd0f 2018-05-16 Paul Riseborough - EKF: Don't make detection of indoor operation dependent on optical flow
1562a82 2018-05-16 Paul Riseborough - EKF: Add parameter to adjust on-ground movement detector sensitivity
ea9e824 2018-05-16 Paul Riseborough - EKF: Improve detection of indoor flight condition
565f992 2018-05-16 Paul Riseborough - EKF: Reduce effect of yaw gyro bias when using optical flow indoors
e10798b 2018-05-16 Paul Riseborough - EKF: Add on ground movement detector
2d3b652 2018-05-15 Paul Riseborough - EKF: Reset yaw gyro bias learning when resuming use of magnetometer
8191068 2018-05-15 Paul Riseborough - EKF: Don't start using mag if optical flow use is interrupted
4889e84 2018-05-15 Paul Riseborough - EKF: Don't fuse multi rotor drag if yaw angle is bad
092a8d8 2018-05-15 Paul Riseborough - EKF: Fix GPS validity time check error
0160aaa 2018-05-15 Paul Riseborough - EKF: Don't use magnetometer with optical flow only nav if GPS checks are failing
8451676 2018-05-14 Paul Riseborough - EKF: Use stricter GPS accuracy test when optical flow is being used
a80b3ab 2018-05-27 Daniel Agar - set MODULE define for each library
High rate optical flow data could make flow fusion to run every major update cycle, resulting in the calculation of bias errors in the body rates used to compensate flow data failing time validity checks and not running. This resulted in a slow drift of the nav solution if bias errors were present in the in the gyro data used for flow sensor motion compensation.
This is required because it can take several seconds for an optical flow sensor operation to be confirmed and there are also many use cases for indoor operation where no optical flow is used.
If magnetometer use is being inhibited because an indoor condition has been detected (optical flow and poor or no GPS) and the optical flow fusion checks fail causing the EKF to stop navigating, we do not want the EKF to start using the magnetometer.
- P and D gains are too high for a racer
- default I gain is too low (0.25 is still quite low)
- use the thrust curve param instead of TPA
- improve responsiveness in Manual & increase max tilt angle to 60 degrees
- enable one-shot
- enable high-rate logging profile
- disable RC filter
Implements a better method of determining when to switch from velocity to altitude control to keep height limit from being exceeded.
This method removes the overshoot and transients in height caused by the switching of the previous algorithm.
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