期刊文献+

有输入未建模动态的导弹鲁棒控制器设计 被引量:7

Robust Controller Design for Missile System with Input Unmodeled Dynamics
下载PDF
导出
摘要 在导弹系统俯仰通道中存在输入未建模动态情况下,提出了一种基于RBF神经网络和反演控制技术的非线性鲁棒控制器的设计方法。首先应用两个RBF神经网络对输入未建模动态设计了神经网络逆补偿器,然后利用反演控制技术设计了导弹非线性控制器,最后应用Lyapunov稳定性理论推导出RBF神经网络权重矢量调节律,证明了系统的所有信号均有界且全局指数收敛至原点。最后给出的BTT导弹非线性六自由度数字仿真结果显示了该设计方法的有效性。 Based on RBF neural networks and backstepping control techniques, a nonlinear robust controller design method is proposed for missile control systems with input unmodeled dynamics in pitch channel. The neural inverse compensator is designed using two RBF neural networks. Then the nonlinear controller is designed using backstepping control techniques. The tuning rules of RBF neural network weight matrix are derived by the Lyapunov stability theorem. All signals of the closed-loop system are bounded and exponentially converge to the origin globally. Finally, nonlinear six-degree-of-freedom (6-DOF) numerical simulation results for a bank-to-turn (BTT) missile model are presented to demonstrate the effectiveness of the proposed method.
出处 《飞行力学》 CSCD 2003年第4期42-45,共4页 Flight Dynamics
关键词 导弹 鲁棒控制器 设计 非线性系统 RBF神经网络 输入未建模动态 RBF neural network input unmodeled dynamics nonlinear system backstepping
  • 相关文献

参考文献8

  • 1[1]Krstic M,Kanellakopoulos I,Kokotovic P.Nonlinear and adaptive control design[M].New York:Wiley-Interscience Publication,1996.
  • 2[2]Sepulchre R,Jankovic M,Kokotovic P.Constructive nonlinear control[M].London:Springer,1997.
  • 3[3]Acrak M.Unmodeled dynamics in robust nonlinear control[D].Phd dissertation,UCSB,2000.
  • 4[4]Jiang Z P,Hill D J.A robust adaptive backstepping and small-gain approach to adaptive output feedback control[J].IEEE Transactions on Automatic Control,1999,44(9):1 705-1 711.
  • 5[5]Selmic R R,Lewis F L.Deadzone compensation in motion control systems using neural networks[J].IEEE Transactions on Automatic Control,2000,45(4):602-613.
  • 6胡云安,晋玉强,张友安,崔平远.导弹非线性自适应鲁棒控制系统设计[J].飞行力学,2002,20(4):65-68. 被引量:3
  • 7胡云安,晋玉强,郭晓军.导弹自适应反演控制器设计[J].航天控制,2002,20(2):23-28. 被引量:11
  • 8[8]Lee T,Kim Y.Nonlinear adaptive flight control using backstepping and neural networks controler[J].Journal of Guidance,Control,and Dynamics,2001,24(4):675-682.

二级参考文献10

  • 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
  • 4[1]Devaud E,Siguerdidjane H,Font S.Some control strategies for a high-angle-of-attack missile autopilot[J].Control Engineering Practice,2000,8(8):885-892.
  • 5[2]Richard A Hull,Darren Schumacher,QU Zhi-hua.Design and evaluation of robust nonlinear missile autopilots from a performance perspective[A].Proceeding of the American Control Conferences[C].Washington,1995.189-193.
  • 6[3]Sridhar Seshagiri, Hassan K Khalil. Output feedback control of nonlinear systems using RBF neural networks[J].IEEE Transactions on Neural Network,2000,11(1):69-79.
  • 7[4]Li Y,Sundararajan N,Saratchandran P.Neuro-controller design for nonlinear fighter aircraft maneuver using fully tuned RBF networks[J].Automatica,2001,37(8):1 293-1 301.
  • 8[7]Taeyoung Lee,Youdan Kim.Nonlinear adaptive flight control using backstepping and neural networks controler[J].Journal of Guidance,Control and Dynamics,2001,24(4):675-682.
  • 9李崇坚,郭国晓,高龙,李发海.电力系统非线性PID励磁控制器[J].清华大学学报(自然科学版),2000,40(3):48-51. 被引量:7
  • 10胡云安,晋玉强,郭晓军.导弹自适应反演控制器设计[J].航天控制,2002,20(2):23-28. 被引量:11

共引文献12

同被引文献55

引证文献7

二级引证文献22

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