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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/195 ; 244/228 ; 244/194 ; 244/196|
|§371/§102 date||19890109 (19890109)|
|발명자 / 주소||
|출원인 / 주소||
|인용정보||피인용 횟수 : 32 인용 특허 : 4|
System for controlling roll and yaw of an aircraft. The system includes a device capable of elaborating, from electric signals respectively representative of the position of a first voluntary actuation member, the rolling speed, the attitude, the yaw speed, the sideslip and of the position of a second voluntary actuation member, a single electrical order for roll control formed by a linear combination of the electric signals. There is a device capable of elaborating, from the same electric signals, an electrical order for yaw control formed by a linear c...
System for controlling roll and yaw of an aircraft (1) comprising roll control surfaces (8, 9) actuated from a first voluntary actuation member (14) and a rudder (11) actuated from a second voluntary actuation member (15), via a mechanical transmission (24), said first and second voluntary actuation members (14, 15) being associated with transducers (37, 39-41) delivering respectively first and second electrical signals depending on the position of said members, said aircraft comprising in addition means (43, 47) capable of delivering third, fourth, fift...