|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/38 B60T-007/00 F15B-003/00 G06F-019/00|
|미국특허분류(USC)||244/099.4; 060/567; 060/579; 700/150|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 8 인용 특허 : 19|
Herein disclosed is an actuator control apparatus, comprising primary control means for producing a control signal used to control an operation of an actuator in accordance with an instruction signal indicative of an operation of the actuator, secondary control means for producing a control signal in accordance with the instruction signal; and switching means for selectively switching one of the primary control means and the secondary control means to the other, and in which the secondary control means is less in the number of functions than the primary ...
What is claimed is: 1. An actuator control system, comprising a plurality of actuators for driving one flight control surface of an aircraft; a plurality of actuator control apparatuses being installed for each of said actuators, and producing a control signal used to control said each of actuators; and a flight control computer producing an instruction signal used to control said actuator control apparatuses, each of said actuator control apparatuses comprising: a primary control means for producing a primary control signal in accordance with said inst...