Application of redundancy in the servomechanism for the rocket thrust vector control

被引：0
|
作者：
Zhang, XS [1 ]
Shi, L [1 ]
机构：
[1] China Acad Launch Vehicle Technol, Res Inst 18, Beijing, Peoples R China
来源：
PROCEEDINGS OF THE 3RD INTERNATIONAL SYMPOSIUM ON FLUID POWER TRANSMISSION AND CONTROL | 1999年
关键词：
servomechanism; redundancy;
D O I：
暂无
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The intent of this paper is to describe a kind of tripler redundant servomechanism for the rocket thrust vector control. Thr basic methods of fault tolerance are included. The result of performance simulation is presented.
引用
收藏
页码：412 / 414
页数：3
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