Nonlinear synthesis, optimization and design of the spacecraft gyromoment attitude control systems

被引：0
|
作者：
Somov, YI [1 ]
机构：
[1] Russian Acad Sci, Inst Syst Dynam & Control Theory, Irkutsk 664033, Russia
来源：
CONTROL APPLICATIONS OF OPTIMIZATION 2000, VOLS 1 AND 2 | 2000年
关键词：
nonlinear control systems; optimization; gyros; attitude control; design;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The optimization methods for a high-accuracy nonlinear feedback attitude control of the large-scale flexible spacecraft under their spatial rotation manoeuvers are described. The effective damping of oscillations within such flexible structures, using gyrodynes (single gimbal control moment gyroscopes) with electromagnetic suspended rotors, are developed. Some mathematical methods, software for computer-aided design and results are presented. Copyright (C) 2000 IFAC.
引用
收藏
页码：337 / 342
页数：6
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