A system and method of controlling flight of an aircraft is disclosed. The system includes a first inceptor that provides a direct mode command for controlling a control axis of the aircraft according to a direct mode and a second inceptor that provides a stable mode command for controlling the control axis of the aircraft according to a stable mode. A processor receives the direct mode command and the stable mode command, forms a combined command for controlling the control axis of the aircraft based on a combination of the direct mode command and the stable mode command, and controls the control axis of the aircraft according to the combined command.
Simultaneous flight path control and attitude control with control axis splitting
2020-05-05
Patent
Electronic Resource
English
Aviation Flight Attitude Control Technology
British Library Conference Proceedings | 2015
|Solar Pressure Three-Axis Attitude Control
AIAA | 1980
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