|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-013/16 G05D-001/08 G06F-019/00|
|미국특허분류(USC)||701/003; 701/010; 701/011; 244/076C|
|우선권정보||FR-09 03820 (2009-08-03)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 7|
A method and device for reducing on an aircraft lateral effects of a turbulence. The device (1) includes means (2, 3, 5, 7, A1, A2) for calculating and applying a roll control command and a yaw control command enabling the side effects generated by a turbulence event to be attenuated on the aircraft.
1. A method for attenuating on an aircraft (A) the side effects generated by at least one turbulence event undergone by this aircraft (A) upon a flight, method according to which, upon a flight of aircraft (A), automatically and iteratively, comprising: a) estimating a roll moment of aircraft (A), which is due to wind and a yaw moment of the aircraft (A), which is also due to wind;b) measuring the current values of aircraft (A);c) using said estimated roll moment, said yaw moment and said measured current values, calculating: a roll control command for a...