|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||G01C-023/00 G05D-001/00 G05D-003/00 G06F-007/00 G06F-017/00 B64C-013/18 B64C-013/50 G05D-001/06 G05D-001/08|
|우선권정보||FR-13 58827 (2013-09-13)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 5|
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.
1. An electric flight control system for an aircraft, comprising: at least one mobile control surface configured to be deflected as a function of deflection commands received;at least one control stick configured to be actuated manually by a pilot of the aircraft, a position of the control stick generating first guidance commands representative of the position;an automatic piloting device configured to automatically generate second guidance commands; andat least one flight control computer configured to automatically compute control surface deflection co...