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文章基本信息

  • 标题:Research on Adaptive Sliding Mode Control of Simplified Supersonic Missile System with Three Kinds of Uncertain Parameters
  • 本地全文:下载
  • 作者:Jinyong Yu ; Junwei Lei ; Di Liu
  • 期刊名称:International Journal of Hybrid Information Technology
  • 印刷版ISSN:1738-9968
  • 出版年度:2016
  • 卷号:9
  • 期号:11
  • 页码:303-314
  • 出版社:SERSC
  • 摘要:A new kind of adaptive sliding mode control method is proposed for simplified missile model of pitch channel with time varying and uncertain parameters. Sliding mode control is an effective method for coping with system uncertainties. Adaptive method is integrated with sliding mode method and a Lyapunov function is constructed to guarantee the whole system is stable. Through the theoretical analysis and numericala simulation, comparison between PID control and sliding mode control shows that the adaptive sliding mode control of the uncertain missile system has a better control effect. And with consideration of three kind of parameter uncertainties in simulation, sliding mode control has better robustness.
  • 关键词:Sliding mode control; uncertainty; supersonic missile; PID control; ;robustness
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