Analysis of the characteristics by modeling and simulation of actuator in flight control system

被引：0
|
作者：
Hu, Xiao [1 ]
Mao, Zhenjie [1 ]
Jiao, Zongxia [1 ]
Wu, Shuai [1 ]
Yu, Xiao [2 ]
Li, Fengyu [2 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Aviat Ind Dev Res Ctr China, Beijing 100191, Peoples R China
来源：
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年
关键词：
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
Flight control system consists of flight controller, sensor, and actuator. Currently, the research focuses on the design and optimization of flight controller, regardless the influence of actuator. This paper is devoted to find out the way actuator effects the flight control system in both dynamic and energy consumption by substituting actuator (hydraulic actuator and electro-hydrostatic actuator) model into the model of flight control system. Results revealed that the model with electro-hydrostatic actuator is better than another in energy consumption characteristics, but worse in dynamic characteristics.
引用
收藏
页码：2618 / 2623
页数：6
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