Tree: 4d95a9d1c3

AP_Periph-1.3

Copter-4.2

Copter-4.2-BW

apm_2208

apm_2208-rover

apm_2208-rover-debug

c421

copter407

gps-1.3.1

main

master

master_rangefinder

mission-4.1.18

periph-1.3.1

release-4.2.3

rover_4.3

zr-sdk-4.3.1

zr-v5.0

zr-v5.1

zr/Rover-4.3

zr/main-4.3

zr_rover4.2

数字绿土/zr-v5.0

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Commit Graph

602 Commits (4d95a9d1c36075f535b9b1cb9599cd971b222230)

Author	SHA1	Message	Date
priseborough	7202acc1b5	AP_NavEKF3: Default EKF3 to off ... Will revert this and set EKF2 to off by default after testing is completed on all platform types	8 years ago
priseborough	39969e7d8e	AP_NavEKF3: added EKF3 for EKF experimentation ... AP_NavEKF3: Implement same maths as PX4/ecl EKF Replace attitude vector states with quaternions Remove gyro scale factor states Add XY accel delta velocity bias estimation Initial tuning Add GPS body frame offset compensation AP_NavEKF3: Fix bugs and consolidate aiding switch logic Switching in and out of aiding modes was being performed in more than one place and was using two variables. The reversion out of GPS mode due to prolonged loss of GPS was not working. This consolidates the logic and ensures that PV_AidingMode is only changed by the setAidingMode function. AP_NavEKF3: prevent multiple fusion mode changes per filter update AP_NavEKF3: Update tuning defaults AP_NavEKF3: Fix bug causing switching in and out of aiding If the GPS receiver was disconnected and no data received, then then the gpsGoodToAlign check did not get a chance to run and becasue it was previously true the EKF would switch back into aiding. This prevents this by ensuring that gpsGoodToAlign defaults to false when the check is not being performed. An additional check has also been dded to ensure that there is GPS data to fuse before we declare ready to use GPS. AP_NavEKF3: Fix bug preventing planes recovering from bad magnetometers This bug created a race condition whereby if the EKF had to reset the yaw to the GPS ground course to recover from a bad magnetometer, the new heading could be over-written by the bad magnetic heading when the plane reached the height for the scheduled reset. AP_NavEKF3: Improve switch-over to backup magnetometer When switching over to a back up magnetometer, ensure that the earth field estimate are reset. Otherwise mag earth field estimates due to the previous failed mag could cause data from the new mag to be rejected. AP_NavEKF3: enable automatic use of range finder height AP_NavEKF3: Fix bug in handling of invalid range data AP_NavEKF3: Fix height drift on ground using range finder without GPSAP_NavEKF3: AP_NavEKF3: Handle yaw jumps due to core switches AP_NavEKF3: Enable simultaneous GPS and optical flow use AP_NavEKF3: fix console status reporting AP_NavEKF3: send messages to mavlink instead of console This allows the GCS to better handle the display of messages to the user. AP_NavEKF3: replace deprecated function call AP_NavEKF3: Compensate for sensor body frame offsets AP_NavEKF3: Fix bug in median filter code AP_NavEKF3: save some memory in the position offsets in EKF3 We don't need to copy that vector3f for every sample. A uint8_t does the job AP_NavEKF3: Add fusion of range beacon data AP_NavEKF3: Bring up to date with EKF2 AP_NavEKF3: Misc range beacon updates AP_NavEKF3: Add mising accessors AP_NavEKF3: remove duplicate include AP_NavEKF3: Prevent NaN's when accessing range beacon debug data AP_NavEKF3: Update range beacon naming AP_NavEKF3: updates AP_NavEKF3: miscellaneous changes AP_NavEKF3: misc updates AP_NavEKF3: misc range beacons updates AP_NavEKF3: add missing rover default param	8 years ago