淡江大學機構典藏:Item 987654321/106310
English  |  正體中文  |  简体中文  |  全文笔数/总笔数 : 62830/95882 (66%)
造访人次 : 4047701      在线人数 : 610
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
搜寻范围 查询小技巧：
  • 您可在西文检索词汇前后加上"双引号"，以获取较精准的检索结果
  • 若欲以作者姓名搜寻，建议至进阶搜寻限定作者字段，可获得较完整数据
    •  进阶搜寻


    jsp.display-item.identifier=請使用永久網址來引用或連結此文件: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/106310


    题名: A simple adaptive GIPN missile guidance law
    作者: Tyan, Feng;Shen, Jeng-fu
    日期: 2006-06-14
    上传时间: 2016-04-22 13:45:38 (UTC+8)
    出版者: IEEE
    摘要: In this paper, a simple yet effective adaptive ideal proportional navigation (AIPN) guidance law is proposed. Unlike some other approaches adopted from optimal control, two points boundary value problem is avoided. All the formulation and analysis are performed in a line of sight (LOS) fixed natural coordinate, and the closed-form solution for the case of nonmaneuvering target is derived. For the purpose of comparison, a state feedback type control law is constructed using the state-dependent Riccati (SDRE) technique. Numerical examples show that for both maneuvering and nonmaneuvering target, the proposed AIPN guidance law outperforms the IPN, and the SDRE based guidance law in the sense of time to go and defined cost
    關聯: American Control Conference 2006, pp.345-350
    DOI: 10.1109/ACC.2006.1655379
    显示于类别:[航空太空工程學系暨研究所] 期刊論文

    文件中的档案:

    档案 描述 大小格式浏览次数
    index.html0KbHTML345检视/开启

    在機構典藏中所有的数据项都受到原著作权保护.

    TAIR相关文章

    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - 回馈