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18,883 Commits 70 Branches 507 Tags 660 MiB
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18883 Commits

Author SHA1 Message Date
Jonathan Challinger 78af6d61de AP_Compass: only play compass cal cancel tone if a cal was running 2015-10-21 08:24:49 +11:00
Jonathan Challinger 3b480bd6ec AP_InertialSensor: fix order of accelerometer corrections 2015-10-21 08:22:36 +11:00
Jonathan Challinger 562db11159 AP_Compass: fix potential AP_Notify concurrency problem 2015-10-20 20:54:02 +09:00
Andrew Tridgell 3af4a7fee7 autotest: make CopterAVC use EKF2 
this gives some testing of EKF2 in autotest
 2015-10-20 21:00:59 +11:00
Paul Riseborough cd8b9c7d26 AP_NavEKF: prevent high rate mag data locking out other data fusion 2015-10-20 20:16:04 +11:00
Paul Riseborough ab8c28a7cc AP_NavEKF: Fix bug allowing takeoff in GPS modes without aiding 
The legacy EKF switches GPs aiding on on arming, whereas the new EKF switches it on based on GPS data quality.
This means the decision to arm and therefore the predicted solution flags must now reflect the actual status of the navigation solution as it will no longer change when motor arming occurs.
 2015-10-20 20:16:00 +11:00
Paul Riseborough e076ed7f66 AP_NavEKF2: Remove compiler warning message 2015-10-20 18:16:16 +11:00
Andrew Tridgell b0aa7cb990 DataFlash: use new perf API 2015-10-20 18:16:16 +11:00
Andrew Tridgell cb0f7cb370 NavEKF2: use new perf counter API 2015-10-20 18:16:15 +11:00
Andrew Tridgell f66966ccae NavEKF: use new perf counter API 2015-10-20 18:16:15 +11:00
Andrew Tridgell 8dbb51c64e HAL_PX4: implement AP_HAL::Util perf calls for PX4 2015-10-20 18:09:57 +11:00
Andrew Tridgell 28fa05c965 AP_HAL: added generic perf counter 
simple wrapper around PX4 API, but ready for use by other HALs
 2015-10-20 18:09:57 +11:00
Randy Mackay 3f9d62d6b4 Copter: 3.3.1-rc1 release notes 2015-10-20 16:00:41 +09:00
Randy Mackay 1858a0544f Copter: guided takeoff checks auto-armed status 
This resolves an edge case in which the vehicle could takeoff with auto-armed false
 2015-10-20 15:51:55 +09:00
Andrew Tridgell 16bc7d8b2e Tools: fixed datestamp on compiler download 2015-10-20 15:54:44 +11:00
Andrew Tridgell 279a320f44 Tools: switch autobuild to 4.9 compiler 2015-10-20 15:28:13 +11:00
Paul Riseborough 60c2e81d19 AP_NavEKF2: Apply optimisations to declination fusion covariance update 
These are the same type of optimisations that were successful with the magnetometer fusion
 2015-10-20 15:21:41 +11:00
Paul Riseborough 0054291cf4 AP_NavEKF2: Apply optimisations to side-slip fusion covariance update 
These are the same optimisations that were successful with the magnetometer fusion
 2015-10-20 15:21:40 +11:00
Paul Riseborough 5e4bc4e954 AP_NavEKF2: Apply optimisations to airspeed fusion covariance update 
These are the same optimisations that were successful with the magnetometer fusion
 2015-10-20 15:21:40 +11:00
Paul Riseborough a29147d6d2 AP_NavEKF2: Apply optimisations to optical flow covariance update 
These are the same optimisations that were successful with the magnetometer fusion
 2015-10-20 15:21:40 +11:00
Paul Riseborough b5e43288d4 AP_NavEKF2: Down to 12 from 14 usec for perf test[8] 2015-10-20 15:21:40 +11:00
Paul Riseborough 0f530bb5a0 AP_NavEKF2: Correct comments 2015-10-20 15:21:40 +11:00
Andrew Tridgell d1dfd5fd01 AP_NavEKF2: use common header for optimisation level and irq disable 2015-10-20 15:21:40 +11:00
Andrew Tridgell a017ae7e00 AP_NavEKF2: down to 218us for test[9] 2015-10-20 15:21:40 +11:00
Andrew Tridgell fc23be8025 AP_NavEKF2: enable fine grained perf tuning for mag fusion 2015-10-20 15:21:40 +11:00
Andrew Tridgell b6c1352e4c AP_NavEKF2: added 10 test perf counters 
used for fine grained performance tuning
 2015-10-20 15:21:40 +11:00
Paul Riseborough 824436dfb6 AP_NavEKF2: Explicitly define constants as floats 2015-10-20 15:21:40 +11:00
Paul Riseborough 2fbd050418 AP_NavEKF2: Use blended accelerometer data 
If high vibration levels cause offsets between the two, it switches to the accelerometer with lower vibration levels. The default behaviour is to use the average of both accelerometers.
 2015-10-20 15:21:40 +11:00
Paul Riseborough 240ea92947 AP_NavEKF: Re-center gyro bias limits on arming 
Allows the gyro bias to vary by up to +-10 deg/second before and after arming.
 2015-10-20 15:21:39 +11:00
Paul Riseborough 8515dda727 AP_NavEKF: Fix bug in vertical position derivative calculation 2015-10-20 15:21:39 +11:00
Paul Riseborough 2b13020c19 AP_NavEKF2: Fix bug in vertical position derivative calculation 2015-10-20 15:21:39 +11:00
Paul Riseborough f6ad79688e AP_NavEKF2: Update start sequence console messages 2015-10-20 15:21:39 +11:00
Paul Riseborough 6b3e114cd6 AP_NavEKF: Enable EKF1 to be disabled to reduce frame over-runs 2015-10-20 15:21:39 +11:00
Paul Riseborough 1a1236f764 AP_NavEKF2: Update magnetometer fusion documentation 2015-10-20 15:21:39 +11:00
Paul Riseborough 8526a8ba7e AP_NavEKF2: Level processor loading between frames 
Don't fuse other measurements on the same frame that magnetometer measurements arrive if running at a high frame rate as there will be insufficient time to complete other operations.
 2015-10-20 15:21:39 +11:00
Paul Riseborough 225b81baf4 AP_NavEKF2: Prevent users breaking filter by setting excessive time delays 
If time deelays greater than the IMU buffer length are used, then it is possible for measurements to be dropped.
 2015-10-20 15:21:39 +11:00
Paul Riseborough a1d6c7ae1e AP_NavEKF2: Improve timing accuracy 
This parameter is a compromise between numerical accuracy of the covariance prediction and sensor timing jitter
Further testing has shown that doing covariance prediction and sensor fusion every 10msec has no observable effect on fusion health and reduces timing hitter noise on magnetometer observations during high rate maneovures
 2015-10-20 15:21:39 +11:00
Paul Riseborough e0ed2dab63 AP_NavEKF2: Adjust IMU FIFO buffer for different IMU data rates 
The values chosen ensure that up to consistent 250 msec of sensor delay compensation is available for different platform types
The revised values also ensure that fusion occurs at different time to when the 10Hz magnetometer measurements are read
 2015-10-20 15:21:39 +11:00
Paul Riseborough baa8692960 AP_NavEKF2: Allow use of magnetometer learning during optical flow nav 
Adds fusion of the declination when there are no earth relative measurements so that the declination angle and therefore the copters yaw angle have an absolute reference.
This enables the length (but not the declination) of the earth field North/East states to change along with the magnetometer offsets.
 2015-10-20 15:21:38 +11:00
Paul Riseborough 1b8a93ef0c AP_NavEKF2: Update function header comments 2015-10-20 15:21:38 +11:00
Paul Riseborough 6899767d28 AP_NavEKF2: Disable magnetic field learning if we have no absolute position reference 2015-10-20 15:21:38 +11:00
Paul Riseborough 75a61df627 Copter: Enable access to EKF2 height tuning 2015-10-20 15:21:38 +11:00
Paul Riseborough d0aba09503 Copter: Access EKF healthy through AHRS object 
Enables EKF2 use
 2015-10-20 15:21:38 +11:00
Paul Riseborough 19785c1033 Copter: Access EKF origin through AHRS object 
Enables EKF2 use
 2015-10-20 15:21:38 +11:00
Paul Riseborough 7c6b31b585 Copter: Access EKF variance checks through AHRS object 
Supports flight using EKF2
 2015-10-20 15:21:38 +11:00
Paul Riseborough 0722ebe8a0 AP_AHRS: Add EKF variance checks 2015-10-20 15:21:38 +11:00
Paul Riseborough 242b9641c8 AP_NavEKF2: Fix in-air logic bug 2015-10-20 15:21:38 +11:00
Paul Riseborough e7de2d3ea3 AP_NavEKF: Update magnetic field learning options 
Provide an option to always do learning
Make field learning decision logic clearer
Change defaults so that plane learns when airborne
Change defaults so that Rover does not learn (large external magnetic interference)
 2015-10-20 15:21:38 +11:00
Paul Riseborough 495809f211 AP_NavEKF2: Allow magnetic field learning to be faster 2015-10-20 15:21:38 +11:00
Paul Riseborough 84a02efd52 AP_NavEKF2: Improve efficiency of Z magnetometer fusion 2015-10-20 15:21:37 +11:00