7 Commits

Author	SHA1	Message	Date
Roman	f300877db4	yaw controller: computed desired yaw rate based on coordinated turn constraint ... Signed-off-by: Roman <bapstroman@gmail.com>	2017-02-12 11:40:14 +01:00
Roman	ac7fc30ea7	fw attitude controllers: restructuring in order to allow acro flight mode ... - split rate control into body rate control and euler rate control - this allows standard attitude control but also direct rate control of all three axes - allow activation/deactivation of turn compensation Signed-off-by: Roman <bapstroman@gmail.com>	2017-02-12 11:40:14 +01:00
Daniel Agar	2750961be6	c++11 initialization cleanup (#237)	2017-02-05 13:05:10 -05:00
Lorenz Meier	10c6ae77ae	Attitude fw yaw: Initialize yaw rate properly	2016-12-17 13:45:28 +01:00
Lorenz Meier	199c423f1f	Attitude fw: Remove builtin perf counters	2016-05-05 20:06:01 +02:00
Daniel Agar	82cf1827d4	fw multiply integrator gain in loop	2016-03-25 17:28:39 -04:00
Lorenz Meier	e5743d503c	Initial import	2015-10-26 16:06:30 +01:00