zr-v4

Commit Graph

Author	SHA1	Message	Date
Tom Pittenger	3ed2fafefa	DataFlash: Log new CUR2 entry for battery2 data	9 years ago
Tom Pittenger	43c7b4d518	DataFlash: do not log CURR.Throttle because it's already logged elsewhere	9 years ago
Tom Pittenger	7a397475af	DataFlash: log POWR.vcc and Vservo as float in volts instead of int16 mV	9 years ago
Tom Pittenger	608fbee867	GCS_MAVLink: send current2 over mavlink	9 years ago
Tom Pittenger	7b4c503052	AP_Math: use new check_latlng helper	9 years ago
Tom Pittenger	ce9ecf9f3d	AP_Math: added check_latlng helper	9 years ago
Tom Pittenger	64c2510be9	AC_AttitudeControl: fix compile warning float to double promotion in string conversion	9 years ago
Andrew Tridgell	b4bdfa2451	AC_AttitudeControl: return roll, pitch and yaw controller error separately as discussed with Leonard	9 years ago
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.	9 years ago
Andrew Tridgell	b855c70139	GCS_MAVLink: don't route RADIO and RADIO_STATUS packets they don't mean anything off the local link	9 years ago
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.	9 years ago
Andrew Tridgell	a6cbc5d4a5	AP_AHRS: use EKF for groundspeed estimate if available	9 years ago
Leonard Hall	a16018f9fe	AP_Motors: Missed Single fix	9 years ago
Peter Barker	1e146256cc	GCS_MAVLink: move telemetry_delayed up into base class	9 years ago
Grant Morphett	944541b287	PID: Added PID_Info to class for PID logging	9 years ago
Andrew Tridgell	abe850c397	PID: fixed example build	9 years ago
Andrew Tridgell	38965f4617	DataFlash: fixed example build	9 years ago
Andrew Tridgell	04f87a452e	HAL_SITL: fixed tcp client mode	9 years ago
Peter Barker	e828525c94	GCS_MAVLink: adjust_rate_for_stream_trigger is no longer virtual	9 years ago
Peter Barker	43fed65f37	GCS_MAVLink: move adjust_rate_for_stream up	9 years ago
Andrew Tridgell	f4f0ae8c8b	SITL: auto-reconnect FlightAxis on reset button	9 years ago
Peter Barker	03ded35d7c	GCS_MAVLink: update routing example for mavlink namespacing	9 years ago
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	9 years ago
Leonard Hall	d67f83559c	AP_Motors: Single and Coax Fixes	9 years ago
Leonard Hall	e5bdf0a0a2	SITL: Single and Coax fixes	9 years ago
Andrew Tridgell	26ef71e130	AP_Notify: added tuning error tones	9 years ago
Andrew Tridgell	006aafab3f	AP_Tuning: added monitoring of controller output	9 years ago
Andrew Tridgell	6330060e49	AC_AttitudeControl: added monitoring of controller error use RMS P+I+FF output. Thanks to Leonard for the suggestion	9 years ago
Andrew Tridgell	fdac1d26cc	AP_Tuning: added TUNE_MODE_REVERT parameter	9 years ago
Randy Mackay	72b86a3f99	AP_Motors: remove unused stabilizing flag Also initialise some members to resolve converity warnings	9 years ago
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	9 years ago
Andrew Tridgell	f02c8f732c	DataFlash: fixed BAR2 format for drift offset	9 years ago
Paul Riseborough	a94a19bd09	AP_NavEKF2: Fix bug causing continual yaw resets	9 years ago
Tom Pittenger	57d6ccc0dd	AP_HAL_PX4: skip the 100ms delay on first px4io safety_state async attempt	9 years ago
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	9 years ago
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	9 years ago
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.	9 years ago
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	9 years ago
Paul Riseborough	de15928921	AP_NavEKF2: prevent potential arithmetic error in declination fusion	9 years ago
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	9 years ago
Paul Riseborough	ac329ec31c	AP_NavEKF2: use observation noise to set initial magnetic field variances	9 years ago
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.	9 years ago
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.	9 years ago
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.	9 years ago
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	9 years ago
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.	9 years ago
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	9 years ago
Paul Riseborough	da0622827d	AP_NavEKF: update tuning defaults Increase speed of scale factor learning	9 years ago
Andrew Tridgell	4c66e14563	SITL: fixed air resistance bug for heli, balloon and singlecopter	9 years ago
Randy Mackay	d26a9d4a22	SITL: fix compiler warning by defaulting frame_type	9 years ago

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11739 Commits (8fd31111ad4560ed6b7e44b13d4e01e709a13648)