| 航天器发展对控制理论的挑战 |
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| 引用本文： | 林来兴.航天器发展对控制理论的挑战[J].航天控制,1991(1). |
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| 作者姓名： | 林来兴 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 本文综述和分析了现代航天器的发展及其对控制理论提出的挑战。这些挑战包括:①挠性空间结构动力学和控制;②鲁棒性和自适应控制;③高精度多变量控制系统的设计方法和理论;④容错控制系统的设计和人工智能研究;⑤大系统控制理论。
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| 关 键 词： | 航天器 控制理论 挠性结构 |
DEVELOPMENT OF SPACECRAFT AND ITS CHALLENGES TO THE CONTROL THEORY |
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| Lin Laixing Beijing Institute of Control Engineering.DEVELOPMENT OF SPACECRAFT AND ITS CHALLENGES TO THE CONTROL THEORY[J].Aerospace Control,1991(1). |
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| Authors: | Lin Laixing Beijing Institute of Control Engineering |
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| Institution: | Lin Laixing Beijing Institute of Control Engineering |
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| Abstract: | This paper surveys and analyzes development of modern spacecraft and its challenges to the control theory. These challenges include following: (1) Dynamics ane control of space f lexible structures; (2) Robust and adaptive control; (3) Design method and theory of high accuracy-multivariable control systems; (4) Design of fault-tolerant control systems and intelligent control; (5) Control theory of large-scale systems. |
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| Keywords: | Spacecraft Control theory Flexible structure |
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