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空空导弹电动舵机自适应模糊滑模控制方法

周静 柴永利 黄丰保

兵工自动化Issue(4):42-46,5.
兵工自动化Issue(4):42-46,5.DOI:10.7690/bgzdh.2014.04.011

空空导弹电动舵机自适应模糊滑模控制方法

Method of Adaptive Fuzzy Sliding Mode Control for Air-to-Air Missile Electromechanical Actuator

周静 1柴永利 1黄丰保1

作者信息

  • 1. 中国空空导弹研究院十一所,河南 洛阳 471009
  • 折叠

摘要

Abstract

In allusion to the characteristics of parametric uncertainties and disturbance in air-to-air missile electromechanical actuator, a novel method, which matched dead zone character in nonlinear system and adaptive regulation, is proposed. The note introduces the simple model of electromechanical actuator (EMA), uses classic adaptive control to making system arriving quirkily sliding surface. When switch function arrived, adaptive control should be changed, the value of switch function used switch value, so switch value would be descended with switch function, finally control system will arrive sliding mode steady. The simulation result proved that the methods enhance electromechanical actuator robustness and performance, and effectively restrain the system chattering.

关键词

空空导弹/电动舵机/自适应模糊控制/鲁棒性

Key words

air-to-air missile/electromechanical actuator/adaptive fuzzy control/robustness

分类

军事科技

引用本文复制引用

周静,柴永利,黄丰保..空空导弹电动舵机自适应模糊滑模控制方法[J].兵工自动化,2014,(4):42-46,5.

兵工自动化

OACSTPCD

1006-1576

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