摘要
通过对飞机配平系统的组成、功能和设计原理研究,结合某型飞机研制的技术特点,针对飞机操纵系统出现的问题进行了原理分析和故障定位,针对性地提出了解决措施,对飞机配平系统的型号应用,具有一定的借鉴意义。
Based on the study of the composition, function and design principle of aircraft leveling system,combined with the technical characteristics of a certain type of aircraft development,this paper makes a theoretical analysis and fault location for the problems of aircraft control system,and puts forward corresponding solutions,which should have certain reference significance for the model of aircraft leveling system.
引文
[1]杨一栋.直升机飞行控制[M].北京:北京国防工业出版社,2007.
[2]高金源,等.计算机控制系统[M].北京:北京航空航天大学出版社,2001.
[3]程鹏.自动控制原理[M].北京:北京高等教育出版社,2003.