English  |  正體中文  |  简体中文  |  Items with full text/Total items : 57023/90721 (63%)
Visitors : 12426006      Online Users : 69
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/106310

    Title: A simple adaptive GIPN missile guidance law
    Authors: Tyan, Feng;Shen, Jeng-fu
    Date: 2006-06-14
    Issue Date: 2016-04-22 13:45:38 (UTC+8)
    Publisher: IEEE
    Abstract: 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
    Relation: American Control Conference 2006, pp.345-350
    DOI: 10.1109/ACC.2006.1655379
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

    Files in This Item:

    File Description SizeFormat

    All items in 機構典藏 are protected by copyright, with all rights reserved.

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