淡江大學機構典藏:Item 987654321/109001
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    题名: Analysis of 3D PPN Guidance Laws for Nonmaneuvering Target
    作者: Tyan, Feng
    日期: 2015-10-01
    上传时间: 2016-12-24 02:10:13 (UTC+8)
    出版者: IEEE
    摘要: 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.
    關聯: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS 51(4), pp.2932-2943
    DOI: 10.1109/TAES.2015.140676
    显示于类别:[航空太空工程學系暨研究所] 期刊論文

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