Spacecraft Guidance and Robust Attitude Control with Precise Pointing the Flexible Antennas

被引：5
|
作者：
Somov, Ye. I. [1 ]
Butyrin, S. A. [1 ]
Somov, S. Ye. [1 ]
机构：
[1] Russian Acad Sci, Samara Sci Ctr, Moscow 443001, Russia
来源：
2009 IEEE CONTROL APPLICATIONS CCA & INTELLIGENT CONTROL (ISIC), VOLS 1-3 | 2009年
关键词：
D O I：
10.1109/CCA.2009.5281102
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on spacecraft attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented.
引用
收藏
页码：1057 / 1062
页数：6
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