COMPLICATED DYNAMICS IN SPACECRAFT ATTITUDE-CONTROL SYSTEMS

被引：15

作者：

PIPER, GE ^{[1
]}

KWATNY, HG ^{[1
]}

机构：

[1] DREXEL UNIV,DEPT MECH ENGN & MECH,PHILADELPHIA,PA 19104

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1992年 / 15卷 / 04期

关键词：

D O I：

10.2514/3.20914

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

It is shown that a commonly used, momentum exchange, spacecraft attitude control configuration gives rise to complex nonlinear behavior involving multiple limit cycles and strange attractors. However, if the momentum wheel assembly performance parameters are adequately matched to the spacecraft, it is possible to achieve a globally stable equilibrium. The results are based on an analysis of a simple single-axis problem.

引用

页码：825 / 831

页数：7

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