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导弹自适应反演控制器设计 被引量:11

Design of Adaptive Backstepping Controller of Missile
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摘要 提出了一种应用反演控制技术的非线性自适应导弹控制系统的设计方法。首先采用自适应辨识算法来估计系统中存在的不确定性 ,然后利用反演控制技术处理系统中的非匹配不确定性 ,在虚拟控制中引入了微分阻尼项 ,有效地改善了系统动态性能 ,并应用Lyapunov稳定性理论证明了系统是全局指数稳定的。 A design method for nonlinear adaptive missile control systems is proposed based on backstepping control techniques Firstly an adaptive identification algorithm is used to estimate the uncertainty of the system, then backstepping control techniques is used to deal with the mismatched uncertainty of the system, the differential damp terms are introduced into the fictitious control terms that improve the transient performance of the system effectively It is proved by Lyapunov stability theorem that the system is globally exponentially stable Finally numerical simulation results are presented to demonstrate the effectiveness of the proposed method
出处 《航天控制》 CSCD 北大核心 2002年第2期23-28,44,共7页 Aerospace Control
基金 国家 8 6 3高科技项目资助
关键词 导弹 控制器 设计 反演控制 数学模型 非线性系统 自适应控制 Backstepping control\ Mathematical model\ Nonlinear system Adaptive control
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参考文献3

  • 1[1]Emmanuel Devaud and Jean - Philippe Harcaut. Three - Axes Missile Autopilot Design: From Linear to Nonlinear Control Strategies. Journal of Guidance, Control, and Dynamics. 2001. 24 (1): 64 ~ 71
  • 2[2]Taeyoung Lee and Youdan Kim. Nonlinear Adaptive Flight Control Using Backsetpping and Neural Networks Controller. Journal of Guidance, Control, and Dynamics. 2001. 24 (4): 675~ 682
  • 3[4]Marios M and Polycarpou. Stable Adaptive Neural Control Scheme for Nonlinear System. IEEE Transaction on Automatic Control. 1996. 4 (3): 447~451

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