导弹自动驾驶仪模糊滑模控制设计

2011 IEEE GCC Conference and Exhibition (GCC) Pub Date : 2011-04-19 DOI:10.1109/IEEEGCC.2011.5752563

N. Sadr, H. Momeni

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引用次数: 10

摘要

本文对导弹自动驾驶仪的滑模控制器进行了研究。研究了这类系统的主要问题——颤振现象;我们用边界层法来克服这个问题。因此，该系统在各种不确定性和外界干扰下都具有鲁棒性。并用李亚普诺夫理论证明了系统的稳定性。在下面，应用模糊控制来计算控制器增益(k)，它负责稳定性。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Fuzzy Sliding mode Control for missile autopilot design

In this paper, we have discussed about the Sliding mode Controller (SMC) for missile autopilot. The chattering phenomenon has been studied as the main problem of these systems; we use boundary layer method to overcome this problem. Therefore, the system is robust under various uncertainties and external disturbances. Also, the stability of the system is proved by the Lyapunov theory. In following, Fuzzy control is applied to calculate the controller gain (k), which is responsible for stability.

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2011 IEEE GCC Conference and Exhibition (GCC)

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