Application of Sliding Mode Control to Bank-To-Turn Missile Systems

Proceedings. The First IEEE Regional Conference on Aerospace Control Systems, Pub Date : 1993-05-25 DOI:10.1109/AEROCS.1993.720998

J. Huang, C. Lin

引用次数: 28

Abstract

Sliding mode control is applied to design autopilot for HAVE DASH II bank-to-turn-(BTT) missile systems. The design is evaluated using six degree of freedom simulation and shows a significant improvement over the feedback linearization approach.

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滑模控制在倾斜转向导弹系统中的应用

将滑模控制应用于HAVE DASH II型倾斜转向导弹系统的自动驾驶仪设计。该设计使用六自由度仿真进行评估，并显示出比反馈线性化方法有显着改进。

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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来源期刊

Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,

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