|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||701/010; 701/007; 701/011; 244/076C; 244/177; 244/194|
|우선권정보||FR-08 00701 (2008-02-11)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 10|
Disclosed is a method and device for attenuating lateral effects on an aircraft due to turbulence encountered by the aircraft during flight. The lateral effects are attenuated by applying a roll control order to control a first controllable movable member that acts on aircraft roll and minimizes aircraft roll-wise disturbances due to wind, and a yaw control order that controls a second controllable movable member to act on aircraft yaw. The roll and yaw control orders are calculated based on a sideslip value of the aircraft, while the yaw control order i...
1. A method for attenuating lateral effects on an aircraft due to turbulence encountered by the aircraft during flight, the method comprising the steps of: a) estimating, by a roll moment estimator, a roll moment of the aircraft due to wind;b) measuring current values of first aircraft parameters;c) calculating, by a calculating unit, based on said estimated roll moment and said measured current values, the following: a roll control order to control at least one first controllable movable member to act on aircraft roll, said roll control order applied to...