Roman 55401ec1b0 fw attitude control: compute integrator correctly ...

- I gain was applied wrongly, such that the integrator value was depending
direcly on the I gain. This made the integrator value jump when the gain
was changed

Signed-off-by: Roman <bapstroman@gmail.com>

2017-02-12 11:40:14 +01:00

..

ecl_controller.cpp

c++11 initialization cleanup (#237)

2017-02-05 13:05:10 -05:00

ecl_controller.h

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_pitch_controller.cpp

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_pitch_controller.h

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_roll_controller.cpp

fw attitude control: compute integrator correctly

2017-02-12 11:40:14 +01:00

ecl_roll_controller.h

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_wheel_controller.cpp

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_wheel_controller.h

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_yaw_controller.cpp

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00

ecl_yaw_controller.h

fw attitude controllers: restructuring in order to allow acro flight mode

2017-02-12 11:40:14 +01:00