Controlling chaotic attitude motion of spacecraft by the input-output linearization

被引：1
|
作者：
Chen, LQ [1 ]
Liu, YZ
机构：
[1] Bharathiar Univ, Dept Math, Coimbatore 641046, Tamil Nadu, India
[2] IRTT, Dept Math, Erode 638316, India
来源：
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK | 2000年 / 80卷 / 10期
关键词：
D O I：
10.1002/1521-4001(200010)80:10<701::AID-ZAMM701>3.0.CO;2-Y
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
In this paper, the control of chaotic oscillations is investigated. A nonlinear control methodology termed input-output linearization is utilized. Chaotic attitude motion of a spacecraft moving on an elliptic orbit in the gravitational field with both air drag and internal damping is treated as an example. MSC (1991): 70Q05, 70M20.
引用
收藏
页码：701 / 704
页数：4
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