期刊文献+

滑模变结构制导律的抖振问题研究 被引量:10

Study on Chattering of Sliding Mode Variable Structure Guidance Law
下载PDF
导出
摘要 滑模变结构制导律是一种强鲁棒性的制导律,对于系统的参数变化和外部的干扰具有理论上的完全鲁棒性。然而,滑模变结构制导律在滑模面上的高频抖振是其在实际应用当中的主要障碍。本文介绍了目前削弱滑模变结构制导律抖振的主要方法。重点介绍了模糊控制、RBF神经网络控制与滑模变结构控制相结合的智能滑模变结构制导律。智能滑模变结构制导律是解决抖振问题的发展方向。 Sliding mode variable structure guidance law is a strong robustness guidance law. It iscompletely robustness in theory even respect to system parameter variation and external disturbances.However the chattering of the sliding mode variable structure guidance law on the sliding mode is a mainobstacle in practical application. This paper introduces the main methods to weaken the chattering. Theintelligent sliding mode variable structure guidance law combines with fuzzy control theory and RBF neuralnetwork is emphasized. The future direction of chattering reduction is intelligent sliding mode variablestructure guidance law.
出处 《航空兵器》 2015年第2期10-13,共4页 Aero Weaponry
关键词 滑模变结构制导律 抖振 模糊控制 RBF神经网络 sliding mode variable structure guidance law chattering fuzzy control RBF neuralnetwork
  • 相关文献

参考文献10

二级参考文献78

共引文献78

同被引文献60

  • 1陈克俊,赵汉元.一种适用于攻击地面固定目标的最优再入机动制导律[J].宇航学报,1994,15(1):1-7. 被引量:79
  • 2Lin C F, Ohlmeyer E, Bibel J E, Malyevac S. Optimal Design of In- tegrated Missile Guidance and Contorl CAl. 1998 World Aviation conference [C] . Anaheim, CA, 1998.
  • 3Shima T, ldan M, Golan O M. Sliding mode control for integrated missile autopilot guidance EJ~. Journal o{ Guidance, Control, and Dynamics, 2006, 29 (2): 250-260.
  • 4Hou M Z, Duan G R. Integrated guidance and Control for homing missiles against ground fixed targets EJ]. Chinese Journal of Aero- nautics, 2008, 21 (2): 162-168.
  • 5Rogers S. Missile Guidance Comparison [ C ] ff AIAA Guidance, Navigation, and Control Conference and Ex- hibit, Providence, Rhode Island, 2004.
  • 6Yang C D, Yang C C. Analytical Solution of Generalized Three-Dimensional Proportional Navigation[ J ]. Journal of Guidance, Control, and Dynamics, 1996, 19(3) : 721 - 724.
  • 7Song S H, Ha I J. A Lyapunov-Like Approach to Perform- ance Analysis of 3-Dimensional Pure PNG Laws[ J]. IEEETransactions on Aerospace and Electronic Systems, 1994, 30(1) : 238 -248.
  • 8Oh J H, Ha I J. Capturability of the 3-Dimensional Pure PNG Law[ J]. IEEE Transactions on Aerospace and Elec- tronic Systems, 1999, 35 (2) : 491 - 503.
  • 9Chiou Y C, Kuo C Y. Geometric Approach to Three-Di- mensional Missile Guidance Problem[ J]. Journal of Guid- ance, Control, and Dynamics, 1998, 21(2): 335-341.
  • 10Bhat S P, Bernstein D S. Finite-Time Stability of Contin- uous Autonomous Systems [ J ]. Siam Journal on Control and Optimization, 2000, 38 (3) : 751 - 766.

引证文献10

二级引证文献18

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部