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Author SHA1 Message Date
Peter Barker
df190d1e86 Tracker: subclass GCS_MAVLink in place of defining its functions for it 2016-05-29 16:21:21 +10:00
Peter Barker
a1c97f4585 Rover: subclass GCS_MAVLink in place of defining its functions for it 2016-05-29 16:21:21 +10:00
Peter Barker
bb19c57615 Copter: subclass GCS_MAVLink in place of defining its functions for it 2016-05-29 16:21:21 +10:00
Peter Barker
af5a52e2aa Plane: subclass GCS_MAVLink in place of defining its functions for it 2016-05-29 16:21:21 +10:00
Peter Barker
56114dd37a GCS_MAVLink: use subclasses in vehicle directories 
Instead of the vehicles defining functions that are declared in the libraries directory, they will now create subclasses of GCS_MAVLINK
 2016-05-29 16:21:20 +10:00
Leonard Hall
d67f83559c AP_Motors: Single and Coax Fixes 2016-05-29 16:12:29 +10:00
Leonard Hall
e5bdf0a0a2 SITL: Single and Coax fixes 2016-05-29 16:12:13 +10:00
Andrew Tridgell
f96836ab9a Plane: prevent a discrepancy between EKF origin and home for altitude 2016-05-29 15:47:26 +10:00
Andrew Tridgell
ba3576f027 Plane: added tuning error reporting for quadplanes 2016-05-28 17:33:30 +10:00
Andrew Tridgell
26ef71e130 AP_Notify: added tuning error tones 2016-05-28 17:33:30 +10:00
Andrew Tridgell
006aafab3f AP_Tuning: added monitoring of controller output 2016-05-28 17:33:30 +10:00
Andrew Tridgell
6330060e49 AC_AttitudeControl: added monitoring of controller error 
use RMS P+I+FF output. Thanks to Leonard for the suggestion
 2016-05-28 17:33:30 +10:00
Andrew Tridgell
fdac1d26cc AP_Tuning: added TUNE_MODE_REVERT parameter 2016-05-28 17:33:30 +10:00
Randy Mackay
47c5eaa3ac Tracker: Version and ReleaseNotes for 0.7.7 2016-05-28 16:09:41 +09:00
Randy Mackay
5fb6e4edae Copter: 3.4-rc1 release notes 2016-05-28 15:45:32 +09:00
Randy Mackay
be3b1cb6ab Copter: convert STB_ params to ATC_ANG_ 2016-05-28 15:45:30 +09:00
Randy Mackay
72b86a3f99 AP_Motors: remove unused stabilizing flag 
Also initialise some members to resolve converity warnings
 2016-05-28 15:45:29 +09:00
Andrew Tridgell
b56d784ae4 Plane: limit to zero pitch in quadplane on initial transition 2016-05-28 15:08:46 +10:00
Andrew Tridgell
7ec513668e GCS_MAVLink: reserve some space when param fetch fails 
this ensures we give some buffer space for parameter fetch when we are
low on buffer space

we reserve 100 bytes for 2 seconds after a param fetch fails due to
low buffer space
 2016-05-28 15:08:46 +10:00
Andrew Tridgell
f02c8f732c DataFlash: fixed BAR2 format for drift offset 2016-05-28 15:08:46 +10:00
Pierre Kancir
ee168bee8d APMrover2 : correct arming and failsafe in skid steer mode 
Commit 3636b53#diff-e22a85a55f71f1b9b2d3f293dea61368 introduce arming for rover. But in skid steering mode it was only applied on throttle and the rover still pivot.
The patch also correct rover behaviour in case of failsafe or loitering.
 2016-05-28 14:34:43 +10:00
Andrew Tridgell
168f4e52cf autotest: try to fix build of binaries 2016-05-28 07:29:23 +10:00
Andrew Tridgell
20cf326093 Plane: lower throttle threshold for quadplane is_flying 2016-05-28 07:10:13 +10:00
Paul Riseborough
a94a19bd09 AP_NavEKF2: Fix bug causing continual yaw resets 2016-05-28 06:52:11 +10:00
Tom Pittenger
57d6ccc0dd AP_HAL_PX4: skip the 100ms delay on first px4io safety_state async attempt 2016-05-27 11:30:50 -07:00
Tom Pittenger
e3930b45df Plane: force the safety_state immediately because we want it to be in effect while we make mixer changes 2016-05-27 21:34:40 +10:00
Tom Pittenger
4785650c95 Plane: remove redundant calls to safety_state 2016-05-27 21:34:40 +10:00
Tom Pittenger
d3ac1dc161 AP_HAL: defer calls to safety_state switch to queue an async attempt. 
- this allows for auto-retries if the state does not set correctly
 2016-05-27 21:34:40 +10:00
Tom Pittenger
67aaf7e226 AP_HAL_PX4: defer calls to safety_state switch to queue an async attempt. 
- this allows for auto-retries if the state does not set correctly
 2016-05-27 21:34:40 +10:00
Andrew Tridgell
97e2203e70 AP_NavEKF2: don't do 3D mag fusion on 2nd EKF2 core 
this reduces the risk that mag fusion errors will badly affect
attitude estimation.
 2016-05-27 21:27:06 +10:00
Andrew Tridgell
084a37d4fa autotest: enable LOG_REPLAY and LOG_DISARMED in autotest 
this will give us the ability to analyse any EKF errors
 2016-05-27 21:23:39 +10:00
Peter Barker
480e142cfb autotest.py: remove TARGET no longer required 2016-05-27 08:07:07 -03:00
Peter Barker
3548f90d3a autotest: create SIL object to hold valgrind logpath 2016-05-27 08:07:07 -03:00
Peter Barker
ced07906ad Tools: correct valgrind run in autotest.py 2016-05-27 08:07:07 -03:00
Peter Barker
7b86a05722 Tools: convert autotest build.X and fly.X to use waf build system 2016-05-27 08:07:07 -03:00
Andrew Tridgell
9933069679 Plane: fixed motor test by percentage in quadplane 2016-05-27 11:53:20 +10:00
Andrew Tridgell
d17e3b17bf AP_AHRS: special handling for flying fixed wing with no compass 
we need to accept EKF having no absolute position and velocity before
takeoff with no compass
 2016-05-27 10:18:53 +10:00
Paul Riseborough
de15928921 AP_NavEKF2: prevent potential arithmetic error in declination fusion 2016-05-27 09:00:41 +10:00
Paul Riseborough
722eb0d706 AP_NavEKF2: Fix bug for start of wind speed estimation 
The commencement of airspeed fusion could cause pitch errors due to small variances and large innovations. This issue is addressed by the following changes:
1) The airspeed measurement is used to set wind states to a value that reduces initial innovations.
2) The wind state variances are set to values that better reflect the wind speed uncertainty
 2016-05-27 09:00:41 +10:00
Paul Riseborough
ac329ec31c AP_NavEKF2: use observation noise to set initial magnetic field variances 2016-05-27 09:00:41 +10:00
Paul Riseborough
830751c0ae AP_NavEKF2: remove un-wanted functionality from mag and yaw reset 
The function used to reset magnetic field states and yaw angle should not be used when there is no magnetometer. If it is incorrectly called without a magnetometer it should not change the attitude or field states.
 2016-05-27 09:00:41 +10:00
Paul Riseborough
11c6ea7ef6 AP_NavEKF2: attitude co-variance reset for all post alignment yaw resets 
Whenever the yaw angle is changed, the correlation with other state errors will be incorrect and the terms should be zeroed.
 2016-05-27 09:00:41 +10:00
Paul Riseborough
cdd09df9ac AP_NavEKF: Add function to zero attitude state co-variances 
When changing the vehicle yaw angle, the correlation between the attitude errors and errors in other states is invalid so the corresponding co-variance terms need to be zeroed.
This needs to be done in more than one place.
 2016-05-27 09:00:41 +10:00
Paul Riseborough
6d34ac5ceb AP_NavEKF2: improve switch-over to use of mag field states 
Set initial variances to measurement uncertainties
Always perform a field  and yaw reset
 2016-05-27 09:00:40 +10:00
Paul Riseborough
fe9ddfdfeb AP_NavEKF2: remove code that prevents attitude updates after mag reset 
This code assumes a vehicle is close to level and will not work for all vehicle types. It will be replaced by a different method.
 2016-05-27 09:00:40 +10:00
Paul Riseborough
fe85c68344 AP_NavEKF2: move yaw reset for no compass case 
Should not be in a function that performs reset on magnetic field states
 2016-05-27 09:00:40 +10:00
Paul Riseborough
da0622827d AP_NavEKF: update tuning defaults 
Increase speed of scale factor learning
 2016-05-27 09:00:40 +10:00
Andrew Tridgell
4c66e14563 SITL: fixed air resistance bug for heli, balloon and singlecopter 2016-05-26 20:38:20 +10:00
Randy Mackay
d26a9d4a22 SITL: fix compiler warning by defaulting frame_type 2016-05-26 17:03:28 +09:00
Andrew Tridgell
b76a993f7e autotest: support coaxcopter 2016-05-26 17:09:31 +10:00