de452eb760
Rover: move adjust_rate_for_stream up
9 years ago
9ee62aac30
Plane: move adjust_rate_for_stream up
9 years ago
3cf174c343
Copter: move adjust_rate_for_stream up
9 years ago
43fed65f37
GCS_MAVLink: move adjust_rate_for_stream up
9 years ago
f4f0ae8c8b
SITL: auto-reconnect FlightAxis on reset button
9 years ago
03ded35d7c
GCS_MAVLink: update routing example for mavlink namespacing
9 years ago
df190d1e86
Tracker: subclass GCS_MAVLink in place of defining its functions for it
9 years ago
a1c97f4585
Rover: subclass GCS_MAVLink in place of defining its functions for it
9 years ago
bb19c57615
Copter: subclass GCS_MAVLink in place of defining its functions for it
9 years ago
af5a52e2aa
Plane: subclass GCS_MAVLink in place of defining its functions for it
9 years ago
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
9 years ago
d67f83559c
AP_Motors: Single and Coax Fixes
9 years ago
e5bdf0a0a2
SITL: Single and Coax fixes
9 years ago
f96836ab9a
Plane: prevent a discrepancy between EKF origin and home for altitude
9 years ago
ba3576f027
Plane: added tuning error reporting for quadplanes
9 years ago
26ef71e130
AP_Notify: added tuning error tones
9 years ago
006aafab3f
AP_Tuning: added monitoring of controller output
9 years ago
6330060e49
AC_AttitudeControl: added monitoring of controller error
...
use RMS P+I+FF output. Thanks to Leonard for the suggestion
9 years ago
fdac1d26cc
AP_Tuning: added TUNE_MODE_REVERT parameter
9 years ago
47c5eaa3ac
Tracker: Version and ReleaseNotes for 0.7.7
9 years ago
5fb6e4edae
Copter: 3.4-rc1 release notes
9 years ago
be3b1cb6ab
Copter: convert STB_ params to ATC_ANG_
9 years ago
72b86a3f99
AP_Motors: remove unused stabilizing flag
...
Also initialise some members to resolve converity warnings
9 years ago
b56d784ae4
Plane: limit to zero pitch in quadplane on initial transition
9 years ago
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
9 years ago
f02c8f732c
DataFlash: fixed BAR2 format for drift offset
9 years ago
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.
9 years ago
168f4e52cf
autotest: try to fix build of binaries
9 years ago
20cf326093
Plane: lower throttle threshold for quadplane is_flying
9 years ago
a94a19bd09
AP_NavEKF2: Fix bug causing continual yaw resets
9 years ago
57d6ccc0dd
AP_HAL_PX4: skip the 100ms delay on first px4io safety_state async attempt
9 years ago
e3930b45df
Plane: force the safety_state immediately because we want it to be in effect while we make mixer changes
9 years ago
4785650c95
Plane: remove redundant calls to safety_state
9 years ago
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
9 years ago
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
9 years ago
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.
9 years ago
084a37d4fa
autotest: enable LOG_REPLAY and LOG_DISARMED in autotest
...
this will give us the ability to analyse any EKF errors
9 years ago
480e142cfb
autotest.py: remove TARGET no longer required
9 years ago
3548f90d3a
autotest: create SIL object to hold valgrind logpath
9 years ago
ced07906ad
Tools: correct valgrind run in autotest.py
9 years ago
7b86a05722
Tools: convert autotest build.X and fly.X to use waf build system
9 years ago
9933069679
Plane: fixed motor test by percentage in quadplane
9 years ago
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
9 years ago
de15928921
AP_NavEKF2: prevent potential arithmetic error in declination fusion
9 years ago
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
9 years ago
ac329ec31c
AP_NavEKF2: use observation noise to set initial magnetic field variances
9 years ago
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.
9 years ago
11c6ea7ef6
AP_NavEKF2: attitude co-variance reset for all post alignment yaw resets
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Whenever the yaw angle is changed, the correlation with other state errors will be incorrect and the terms should be zeroed.
9 years ago
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.
9 years ago
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
9 years ago
Peter Barker
Andrew Tridgell
Leonard Hall
Randy Mackay
Pierre Kancir
Paul Riseborough
Tom Pittenger