留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于自适应反演法的导弹直/气复合制导

张天宇 董长虹

张天宇, 董长虹. 基于自适应反演法的导弹直/气复合制导[J]. 北京航空航天大学学报, 2013, 39(7): 902-906.
引用本文: 张天宇, 董长虹. 基于自适应反演法的导弹直/气复合制导[J]. 北京航空航天大学学报, 2013, 39(7): 902-906.
Zhang Tianyu, Dong Changhong. Compound control system design based on adaptive backstepping theory[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(7): 902-906. (in Chinese)
Citation: Zhang Tianyu, Dong Changhong. Compound control system design based on adaptive backstepping theory[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(7): 902-906. (in Chinese)

基于自适应反演法的导弹直/气复合制导

详细信息
  • 中图分类号: V 448

Compound control system design based on adaptive backstepping theory

  • 摘要: 防空导弹要求能够应对高速、高机动性等复杂对抗环境,直接力/气动力复合制导是防空导弹制导系统设计的关键技术.主要研究了直接力/气动力复合控制导弹的控制律、操纵律以及制导律,针对非线性系统,提出了一种基于自适应反演理论的控制方法;直/气复合切换逻辑采用模糊方法;末制导段应用变结构制导律.以某防空导弹为例进行仿真,结果表明该复合制导方法易于实现,对于高机动目标具有良好的制导精度,显示了该方法的有效性.

     

  • [1] Shtessel Y B,Shkolnikov I A,Levant A.Guidance and control of missile intercaptor using second-order sliding modes[J].Aerospace and Electronic Systems,2009,45(1):110-124
    [2] Jin Y C,Dongkyoung C.Adaptive control based on a parametric affine model for tail-controlled missiles[J].Aerospace and Electronic Systems,2006,42(2):659-669
    [3] 杨志峰,雷虎民,李庆良,等.基于动态逆和鲁棒轨迹跟踪控制的导弹控制系统设计[J].宇航学报,2011,32(2):317-322 Yang Zhifeng,Lei Humin,Li Qingliang,et al.A missile control system design approach based on dynamic inverse and robust trajectory tracking control [J].Journal of Astronautics,2011,32(2):317-322(in Chinese)
    [4] 朱隆魁,汤国建,余梦伦.防空导弹直接力/气动力复合控制系统设计[J].宇航学报,2008,29(6):1895-1900 Zhu Longkui,Tang Guojian,Yu Menglun.Compound control system design with direct thrust and aerodynamic force for air defence missile [J].Journal of Astronautics,2008,29(6):1895-1900(in Chinese)
    [5] Zhong L,Jia X H.Novel backstepping design for blended aero and reaction-jet missile autopilot[J].System Engineering and Electronics,2008,19(1):148-153
    [6] 展建超,杨军,谭震.基于变结构控制的气动力/直接力切换控制设计[J].弹箭与制导学报,2009,29(2):83-86 Zhan Jianchao,Yang Jun,Tan Zhen. Aerodynamic/reaction-jet switching-controller design based on variable structure control[J].Journal of Projectiles,Rockets,Missiles and Guidance,2009,29(2):83-86(in Chinese)
    [7] 任义元,袁建平,方群.空空导弹变结构末制导律研究[J].计算机仿真,2009,26(10):25-29 Ren Yiyuan,Yuan Jianping,Fang Qun.A study of terminal variable structure guidance law of air-to-air missile [J].Computer Simulation,2009,26(10):25-29(in Chinese)
    [8] Yeh F K.Adaptive-sliding-mode guidance law design for missiles with thrust vector control and divert control system[J].Control Theory & Application,2012,6(4):552-559
  • 加载中
计量
  • 文章访问数:  1212
  • HTML全文浏览量:  13
  • PDF下载量:  471
  • 被引次数: 0
出版历程
  • 收稿日期:  2012-07-13
  • 网络出版日期:  2013-07-30

目录

    /

    返回文章
    返回
    常见问答