|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||701/006; 701/004; 244/076.0R; 244/178; 244/181; 244/228; 318/584|
|§371/§102 date||20070209 (20070209)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 7|
The invention relates to an electric flight control system for aircraft elevators. According to the invention, the flight control system can be controlled in terms of load factor or rate of pitch. The inventive system comprises built-in protections in relation to load factor, incidence and pitch attitude.
The invention claimed is: 1. An electric flight control system for the control in terms of load factor of the elevators of an aircraft, said elevators being controlled by a control section that compels said elevators to take a deflection position dependent on an electrical signal δmc representative of a controlled value of the angle of deflection δm of said elevators, said system comprising: a first calculation section for calculating, on the basis of an electrical signal nzc representative of a controlled value of said load factor, a first ...