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带有双闭环滤波器的有限时间稳定变结构制导律 被引量:3

Finite Time Stable Variable Structure Guidance Law with Double Closed-loop Filters
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摘要 在末制导过程中,为了取得较高的命中精度,制导律必须使视线(LOS)角速率较快收敛。为了提高制导律的性能,在假设未知不确定时变项有界的前提下,对带有双闭环滤波器的变结构制导律进行了研究。提出的变结构制导律能够使视线角速率及其一阶导数在有限时间内收敛至滑动模态域内,得到更加精确的等效控制并有效克服干扰的影响。通过引入高阶滑动模态,对有关定理进行了重新证明,简化了证明过程,加强了定理的结论,弱化了定理成立的条件。最后利用数值仿真验证了所研究方法的有效性。 In order to achieve higher interception precision,in the process of terminal guidance,the guidance law must ensure that the line of sight(LOS) angular rate converge to zero rapidly.To improve the performance of the guidance law,a variable structure guidance law with double closed-loop filters is studied while assuming the unavailable information as bounded time-varying uncertainties.The method presented here is able to make the LOS angular rate and its first order derivative converge to the sliding mode in a finite time,realize the acquisition of equivalent control accurately and overcome the influence of disturbance.By using the high-order sliding mode,some related theorems are proved again,while the proving process is simplified,the conclusions of the theorems are reinforced and the preconditions are less rigorous.Finally,the effectiveness of the proposed approach is validated by numerical simulation.
出处 《航空学报》 EI CAS CSCD 北大核心 2010年第8期1629-1635,共7页 Acta Aeronautica et Astronautica Sinica
基金 国家"973"计划 武器装备预先研究项目
关键词 有限时间稳定 闭环滤波器 变结构控制 制导律 滑模控制 finite time stability closed-loop filter variable structure control guidance law sliding mode control
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参考文献17

  • 1Holder E J,Sylvester V B.An analysis of modern versus classical homing guidance[J].IEEE Transactions on Aerospace and Electronic Systems,1990,26(4):599-606.
  • 2Imado F,Kuroda T,Lchikawa A.A trade-off study between conventional and augmented proportional navigation[R].AIAA-1996-3882,1996.
  • 3Ha I J,Hur J S,Ko M S.Performance analysis of PNG laws for randomly maneuvering targets[J].IEEE Transactions on Aerospace and Electronic Systems,1990,26(5):713-721.
  • 4Chen R H,Speyer J L,Lianos D.Homing missile guidance and estimation for three-dimensional intercept[R].AIAA-2008-7457,2008.
  • 5Alexander Z,Moshe I.Effect of estimation on the performance of an integrated missile guidance and control system[R].AIAA-2008-7458,2008.
  • 6Babu K R,Sarma I G,Swamy K N.Two robust homing missile guidance laws based on sliding mode control theory[C] ∥National Aerospace and Electronics Conference.1994:540-547.
  • 7Golan O M,Shima T.Precursor interceptor guidance using the sliding mode approach[R].AIAA-2005-5965,2005.
  • 8孙胜,周荻.有限时间收敛变结构导引律[J].宇航学报,2008,29(4):1258-1262. 被引量:37
  • 9高为炳.变结构控制的理论及设计方法[M].北京:科学出版社,1998..
  • 10Xu J X,Pan Y J,Lee T H.Sliding mode control with closed-loop filtering architecture for a class of nonlinear systems[J].IEEE Transactions on Circuits and Systems-II:Express Briefs,2004,51(4):168-173.

二级参考文献7

  • 1Yang C D, Chen H Y. Nonlinear H∞ robust guidance law for homing missiles[J]. Journal of Guidance, Control, and Dynamics, 1998, 21 (6) : 882 - 890.
  • 2Zhou D, Mu C-D, Shen T-L. Robust guidance law with L2 gain performance[ J ]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2001, 44(144) : 82 - 88.
  • 3Zhou D, Mu C-D, Xu W-L. Adaptive sliding-mode guidance of a homing missile [ J ]. Journal of Guidance, Control, and Dynamics, 1999, 22(4) :589 - 594.
  • 4Salehi S, Ryan E. On optimal nonlinear feedback regulation of linear plants[ J ]. IEEE Transactions on Automatic Control, 1982, 27 (6) : 1260- 1264.
  • 5Bhat S, Bernsteln D. Lyapunov analysis of finite-time differential equations[J]. Proceedings of the American Control Conference, Seattle, USA, 1995: 1831- 1832.
  • 6Bhat S, Bernstein D. Continuous finite-time stabilization of the translational and rotational double integrators[J]. IEEE Transactions on Automatic Control, 1998, 43(5): 678-682.
  • 7Shtessel Y, Shkolnikov I. Integrated guidance and control of advanced interceptors using second order sliding modes[J]. IEEE Conference on Decision and Control, Maui, USA, December 2003 : 4587 - 4592.

共引文献131

同被引文献39

  • 1曹邦武,姜长生,关世义,陈谋.电视指令制导空地导弹垂直命中目标的末制导系统研究[J].宇航学报,2004,25(4):393-397. 被引量:28
  • 2康宇,奚宏生,季海波.有限时间快速收敛滑模变结构控制[J].控制理论与应用,2004,21(4):623-626. 被引量:24
  • 3KIM M, GILDER K V. Terminal guidance for impact attitude angle constrained flight trajectories [J]. IEEE Transactions on Aerospace and Electronic Systems, 1973, 9(6): 852 - 859.
  • 4KIM B S, LEE J G, HAN H S. Biased PNG law for impact with an- gular constraint [J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(1): 277 - 288.
  • 5KIM B S, LEE J. Homing guidance with terminal angular against nonmaneuvering and maneuvering target[R]. Reston, VA: AIAA, 1997:189 - 199.
  • 6HONG Y G, HUANG J, XU Y. On an output feedback finite-time stabilization problem [J]. IEEE Transactions on Automatic Control, 2001, 46(2): 305 - 309.
  • 7HONG Y. Finite-time stabilization and stabilizability of a class of controllable systems [J]. Systems & Control Letters, 2002, 46(4): 231 - 236.
  • 8BHAT S, BERNSEIN D. Lyapunov analysis of finite-time differen- tial equations [C] //Proceedings of the American Control Conference. Seattle, WA: IEEE, 1995, 3:1831 - 1832.
  • 9BHAT S, BERNSEIN D. Continuous finite-time stabilization of the translational and rotational double integrators [J]. IEEE Transactions on Automatic Control, 1998, 43(5): 678 - 682.
  • 10SHTESSEL Y B, SHKOLNIKOV I A. Integrated guidance and con- trol of advanced interceptors using second order sliding modes [C] //Proceedings of the IEEE Conference on Decision and Control. Maui, Hawaii: 1EEE, 2003, 5:4587 - 4592.

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