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    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

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