在平衡点之间操纵一个灵活的航天器

1992 American Control Conference Pub Date : 1992-06-24 DOI:10.23919/ACC.1992.4792476

P. Lucibello

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引用次数: 7

摘要

对柔性航天器的控制问题进行了研究。所处理的问题是平衡点之间的状态转移。利用摄动技术建立了一种学习算法，使航天器系统在有限调谐区间内控制，并建立了一种用于渐近再连接的离散反馈方案。并给出了两个数值算例。

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Steering a flexible spacecraft between equilibrium points

An investigation on the control of a flexible spacecraft is presented. The problem addressed is state transfer between equilibrium points. A perturbation technique is used to build up both a learning algorithm, which steers the spacecraft system in a finite tune interval, as well as a discrete feed back scheme for asymptotic reonentetion. Two numerical examples are also worked out.

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来源期刊

1992 American Control Conference

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