9 Commits

Author SHA1 Message Date
Roman
391b6dfd00 yaw controller: for now do not do turn compensation when inverted and use
the roll setpoint as limit for turn compensation

Signed-off-by: Roman <bapstroman@gmail.com>
2017-02-12 11:40:14 +01:00
Roman
66b7773059 yaw controller: deactivate lateral acceleration control for now but
put comment of how to do it properly

Signed-off-by: Roman <bapstroman@gmail.com>
2017-02-12 11:40:14 +01:00
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