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Volume 40 Issue 6
Jun.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(6): 721-726.
Yuan Qingfeng, Lu Hui, Shen Shituanet al. Auto test system resource description method based on XML[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(1): 114-117. (in Chinese)
Citation: Wang Qing, Qi Chengdong, Dong Chaoyanget al. Integrated guidance and control design for a class of missile with networked packet dropouts[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 721-726. doi: 10.13700/j.bh.1001-5965.2013.0408(in Chinese)
shu

Integrated guidance and control design for a class of missile with networked packet dropouts

doi: 10.13700/j.bh.1001-5965.2013.0408

  • 1. School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;

  • 2. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 09 Jul 2013
  • Publish Date: 20 Jun 2014
    Abstract
  • An integrated guidance and control (IGC) algorithm for a class of missile with networked packet dropouts was researched. Considering that a number of ground-based radars were used to observe on the target simultaneously and the target information was shared with the missile through the network. Networked packet dropouts were described as the communication topology model between the missile and radars. The pitch channel IGC model including three cascaded subsystems was established. In this way, virtual controllers were designed for each subsystem. To guarantee the stability of the missile when packets dropouts occur, the corresponding filters were designed for the virtual controllers. An IGC algorithm was put forward by adopting sliding-mode control and back stepping control method. Sufficient condition to guarantee the bounded-input bounded-output (BIBO) stability of the system was simultaneously derived. Finally, simulation results demonstrate the effectiveness of the proposed method.

     

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    • References(12)
  • [1]
    Michael G M. The navy in the 21 century,part I:surface warfare[J].Johns Hopkins APL Technical Digest,2001,22(1):9-18
    [2]
    Hespanha J P, Naghshtabrizi P,Xu Y G.A survey of recent results in networked control systems[J].Proceedings of IEEE,2007,95(1):138-162
    [3]
    Dong C Y, Xu L J,Chen Y,et al.Networked flexible spacecraft attitude maneuver based on adaptive fuzzy sliding mode control[J].Acta Astronautica,2009,65:1561-1570
    [4]
    王祖典. 网络中心制导技术[J].电光与控制,2005,12(4):38-40 Wang Zudian.Network-centric guidance technology[J].Electronics Optics and Control,2005,12(4):38-40(in Chinese)
    [5]
    吴旭光,路亚娟, 唐苗.基于网络控制系统的鱼雷制导系统结构[J].鱼类技术,2005,13(1):18-21 Wu Xuguang,Lu Yajuan,Tang Miao.Framework of torpedo guidance system based on the networked control systems[J].Torpedo Technology,2005,13(1):18-21(in Chinese)
    [6]
    王昭磊,王青, 董朝阳.制导武器控制系统设计[J].现代防御技术,2011,39(6):9-14 Wang Zhaolei,Wang Qing,Dong Chaoyang.Design of control system of guided weapons[J].Modern Defense Technology,2011,39(6):9-14(in Chinese)
    [7]
    Hou M Z, Duan G R.Adaptive dynamic surface control for integrated missile guidance and autopilot[J].International Journal of Automation and Computing,2011,8(1):122-127
    [8]
    Kim B S, Calise A J,Sattigeri R J.Adaptive,integrated guidance and control design for line-of-sight-based formation flight[J].Journal of Guidance,Control,and Dynamics,2007,30(5): 1386-1398
    [9]
    Shtessel Y B, Tournes C H.Integrated higher-order sliding mode guidance and autopilot for dual-control missiles[J].Journal of Guidance,Control,and Dynamics,2009,32(1):79-94
    [10]
    Zhou D, Sun S,Teo K L.Guidance laws with finite time convergence[J].Journal of Guidance,Control,and Dynamics,2009,32(6):1838-1846
    [11]
    Idan M, Shima T,Golan O M.Integrated sliding mode autopilot-guidance for dual-control missiles[J].Journal of Guidance,Control,and Dynamics,2007,30(4):1081-1089
    [12]
    Khalil H K.Nonlinear systems[M].3rd ed.New Jersey:Prentice- Hall,2002:145-146
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