淡江大學機構典藏:Item 987654321/109001
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/109001


    Title: Analysis of 3D PPN Guidance Laws for Nonmaneuvering Target
    Authors: Tyan, Feng
    Date: 2015-10-01
    Issue Date: 2016-12-24 02:10:13 (UTC+8)
    Publisher: IEEE
    Abstract: Unlike the traditional ways adopted by most of the researchers, the rotating angle of relative velocity is adopted in this work as the independent variable to analyze the analytical solution of impact angle, capture region (with or without finite line of sight (LOS) turn rate constraint), range to go, time to go, and a defined fuel cost of a traditional pure proportional navigation (PPN) guidance law for both nonmaneuvering moving, and stationary targets.
    Relation: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS 51(4), pp.2932-2943
    DOI: 10.1109/TAES.2015.140676
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

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