aepko/Ardupilot2
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22,635 Commits 72 Branches 509 Tags 683 MiB
8b405e26ea
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11545 Commits

Author SHA1 Message Date
Tom Pittenger
8b405e26ea GCS_MAVLink: battery2 current is in 10*mAh over mavlink 2016-06-02 16:59:29 -07:00
Tom Pittenger
a8c14e68da AP_Tuning: compile warning: float to double on print 2016-06-02 16:59:27 -07:00
Tom Pittenger
d2c9b02ca5 AP_BattMonitor: remove voltage2() since we have voltage(x) available 2016-06-02 16:59:26 -07:00
Tom Pittenger
4e4bc0bee4 GCS_MAVLink: use voltage(x) instead of voltage2() 2016-06-02 16:59:23 -07:00
Tom Pittenger
a1564bd337 AP_BattMonitor: check actual battery instances instead of max possible instances 2016-06-02 16:59:21 -07:00
Tom Pittenger
8939c5308f AP_Arming: check actual battery instances then max possible instances 2016-06-02 16:59:19 -07:00
Tom Pittenger
3ed2fafefa DataFlash: Log new CUR2 entry for battery2 data 2016-06-02 16:59:16 -07:00
Tom Pittenger
43c7b4d518 DataFlash: do not log CURR.Throttle because it's already logged elsewhere 2016-06-02 16:59:07 -07:00
Tom Pittenger
7a397475af DataFlash: log POWR.vcc and Vservo as float in volts instead of int16 mV 2016-06-02 16:59:05 -07:00
Tom Pittenger
608fbee867 GCS_MAVLink: send current2 over mavlink 2016-06-02 16:59:03 -07:00
Tom Pittenger
7b4c503052 AP_Math: use new check_latlng helper 2016-06-01 17:38:48 -07:00
Tom Pittenger
ce9ecf9f3d AP_Math: added check_latlng helper 2016-06-01 17:38:48 -07:00
Tom Pittenger
64c2510be9 AC_AttitudeControl: fix compile warning float to double promotion in string conversion 2016-06-01 17:38:47 -07:00
Andrew Tridgell
b4bdfa2451 AC_AttitudeControl: return roll, pitch and yaw controller error separately 
as discussed with Leonard
 2016-06-01 17:18:58 +10:00
Grant Morphett
d56e2b6a39 APM_Control: Get steer rate using earth frame. 
Rather then just using the standard z gyro by using the earth frame it
takes into account when a rover leans over in hard corners.  My rover
leans 15 degrees no problem which is why this is needed.
 2016-06-01 10:05:20 +09:00
Andrew Tridgell
b855c70139 GCS_MAVLink: don't route RADIO and RADIO_STATUS packets 
they don't mean anything off the local link
 2016-05-31 22:13:05 +10:00
Paul Riseborough
24d8cc62e2 AP_NavEKF2: rework yaw and magnetic heading reset logic 
Splits in-flight yaw alignment completed status into separate yaw and magnetic field flags.
Reduce the number of places where decisions to perform a yaw and field reset are made.
Don't perform a reset unless there is is data in the buffer
Don't use 3-axis fusion if the field states still need to be reset.
When starting 3-axis fusion request a reset if not previously performed.
Ensure magnetometer and GPs heading resets are alwasy perfomred with data at teh correct time horizon.
 2016-05-31 16:12:53 +10:00
Andrew Tridgell
a6cbc5d4a5 AP_AHRS: use EKF for groundspeed estimate if available 2016-05-31 15:56:25 +10:00
Leonard Hall
a16018f9fe AP_Motors: Missed Single fix 2016-05-31 12:44:17 +10:00
Peter Barker
1e146256cc GCS_MAVLink: move telemetry_delayed up into base class 2016-05-31 08:46:09 +10:00
Grant Morphett
944541b287 PID: Added PID_Info to class for PID logging 2016-05-31 08:44:52 +10:00
Andrew Tridgell
abe850c397 PID: fixed example build 2016-05-31 08:36:14 +10:00
Andrew Tridgell
38965f4617 DataFlash: fixed example build 2016-05-31 08:36:07 +10:00
Andrew Tridgell
04f87a452e HAL_SITL: fixed tcp client mode 2016-05-30 16:42:28 +10:00
Peter Barker
e828525c94 GCS_MAVLink: adjust_rate_for_stream_trigger is no longer virtual 2016-05-29 21:24:41 +10:00
Peter Barker
43fed65f37 GCS_MAVLink: move adjust_rate_for_stream up 2016-05-29 19:38:49 +10:00
Andrew Tridgell
f4f0ae8c8b SITL: auto-reconnect FlightAxis on reset button 2016-05-29 19:17:29 +10:00
Peter Barker
03ded35d7c GCS_MAVLink: update routing example for mavlink namespacing 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
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
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
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
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
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
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