Invention Grant
US09315258B2 Electric flight control system and method for an aircraft 有权
飞机电动飞行控制系统及方法

Electric flight control system and method for an aircraft
Abstract:
A flight control system includes at least one flight domain protection module intended at least for manual piloting and an auxiliary element configured to automatically transmit to the protection module, upon a detection of automatic piloting of the aircraft using an automatic piloting device, a predetermined auxiliary position, representing a control stick position equivalent, the protection module using the auxiliary position as a control stick position to implement a flight domain protection during the automatic piloting.
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