期刊文献+

引入PI校正的两回路自动驾驶仪设计方法

PI compensation strategy applied to two-loop autopilot
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摘要 针对引入PI校正后自驾仪设计人工调节的繁琐性问题,利用极点配置算法,提出了PI校正、纯比例校正、零极点对消三种情况下的设计参数的解析算法,并在仿真结果中分析了上述三种系统的特性及产生原因。实验表明,利用本方法设计出的系统能满足稳定裕度和响应速度要求,快捷有效。 The normal PI compensation will lead to complexity increasing problem in the period of two-loop aatopilot de-sign. Therefore, we present novel analytical expressions of parameters design method using the theory of pole placement in some situations, such as PI controller, pure P controller or pole-zero cancellation. We apply this new method to two-loop autopilot. On the basis, we discuss the system characters as well as its results of this method in those mentioned situations. The results of experiment show that the new systems can reach the requirements of the stability margin and the response speed, this approach is convenient.
出处 《战术导弹控制技术》 2013年第3期32-36,共5页
关键词 两回路自动驾驶仪 PI校正 极点配置 two-loop autopilot PI compensation strategy pole placement
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参考文献6

  • 1Bruyere, L, Tsourdos, A, White, BA et al. Polynomial approach for design and robust analysis of lateral missile control [ J ]. International Journal of Systems Science, 2006, 37(8) :585-597.
  • 2Capello E, Sartori D, Guglieri G. , et al. Robust assess- ment for the design of multi-loop proportional integrative derivative autopilot [ J ]. IET control theory & appli- cations, 2012, 6(11):1610-1619.
  • 3Lin D F, Fan J F. Missile Autopilot Design Using Back- stepping Approach[ C ]. //Proceeding of the Second In- ternational Conference on Computer and Electrical Engi- neerint~ ('ICCEE 2009), 2009(" 1 ) :238-241.
  • 4温求遒,夏群力,祁载康.三回路驾驶仪开环穿越频率约束极点配置设计[J].系统工程与电子技术,2009,31(2):420-423. 被引量:16
  • 5何镜,夏群利,孙静,刘大卫,孙旭光.两回路驾驶仪加速度计杠杆效应研究[J].兵工学报,2012,33(8):962-967. 被引量:2
  • 6Garnell P. Guided weapon control systems [ M ]. Oxford : Pergamon Press, 1977.

二级参考文献15

  • 1陈奎兆,王江云.飞行仿真器自动飞行系统研究[J].系统仿真学报,2006,18(z2):706-709. 被引量:11
  • 2王娟利,祁载康.带阻尼约束的驾驶仪最速响应鲁棒性设计[J].系统仿真学报,2006,18(z2):888-891. 被引量:1
  • 3Garnell P. Guided weapon control systems[M]. Second Revision by Qi zai-kang , Xia qun-li. Beijing: Beijing Institute of Technology, 2004.
  • 4Zarchan P. Tactical and strategic missile guidance[M]. Washington D C, American institute of Aeronautics and Astronautics, 1994.
  • 5蔡林留.飞弹导引控制系统[M].中国台北:天公书局印行,1989.
  • 6Curtis P, Mraeek D, Brett R. Missile longitudinal autopilots: Comparison of multiple three loop topotogies[J]. AIAA Guidance , Navigation , and Control Conference and Exhibit, ArAA 2005 - 6380.
  • 7Curtis P, Mracek D, Brett R. Missile longitudinal autopilots.. Connections between optimal control and classical topologies[J]. AIAA Guidance, Navigation and Control Conference and Eyhibit, AIAA 2005 - 6381.
  • 8Nesline F W, Paul Z. Why modern controllers can go unstable in practice[J]. Journal of Guidance, 1984, 7(4) :495 - 500.
  • 9Kevin A, Wise. Robust stability analysis of adaptive missile autopilots[J]. AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA 2008 - 6999.
  • 10Garnell P. Guided weapon control systems[ M]. 2nd ed. Oxford: Pergamon Press, 1980.

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