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

页码：412 / 414

页数：3

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