|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/181 ; 244/195|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 13 인용 특허 : 0|
According to the invention, attenuator means (8) are provided, making it possible to limit the rate of rotation of the airplane on takeoff, so as to avoid the tail of the airplane striking the ground and to reduce the dispersion of the rotation rates.
An electrical system for control of an elevator aerodynamic surface (1) of an airplane in proximity to the ground, of the type including: a control member (2) actuated by the pilot of the airplane and associated with a position sensor (3) delivering an electrical signal representative of the angle of deflection of said elevator aerodynamic surface on the ground and of the desired attitude (q