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標題: A fuzzy guidance law for vertical launch interceptors
作者: Lin, C.L.
Lin, Y.P.
Wang, T.L.
關鍵字: Fuzzy logic control;Guidance and control;Missile;Guidance law;Performance;high-speed target;midcourse guidance
Project: Control Engineering Practice
期刊/報告no:: Control Engineering Practice, Volume 17, Issue 8, Page(s) 914-923.
A fuzzy logic-based guidance design for longer engagement in time and beneficial interception attitudes is investigated and proposed here. The integrated fuzzy logic-based guidance scheme consisting of vertical, midcourse and terminal guidance phases can intercept the target from diverse aspects. The engagement strategy in the vertical guidance phase includes general vertical launch to handle the case of longer engagement ranges, and vertical launch with back turn (BT) to handle shorter engagement ranges. Numerical experimental results show excellent engagement performance and defensible volumes. (C) 2009 Elsevier Ltd. All rights reserved.
ISSN: 0967-0661
DOI: 10.1016/j.conengprac.2009.02.008
Appears in Collections:電機工程學系所

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