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標題: On the design of fuzzified trajectory shaping guidance law
作者: Lin, C.L.
Lin, Y.P.
Chen, K.M.
關鍵字: Missile;Guidance;Neuron fuzzy system;Trajectory shaping
Project: Isa Transactions
期刊/報告no:: Isa Transactions, Volume 48, Issue 2, Page(s) 148-155.
Mid course guidance is commonly designed to save as much energy as possible so that the missile's final speed can be maximized while entering the homing stage. For this purpose, a competitive guidance design should be able to generate an admissible flight trajectory as to bring the interceptor to a superior altitude for a favorable target engagement. In this paper, a new adaptive trajectory shaping guidance scheme based on the adaptive fuzzy inference system, which is capable of generating a variety of trajectories for efficient target interception, is presented. The guidance law is developed with the aim of saving the interceptor's energy conservation while improving performance robustness. Applications of the presented approach have included a variety of mission oriented guidance, such as cruise missile guidance, anti-ballistic missile guidance, etc. (c) 2008 ISA. Published by Elsevier Ltd. All rights reserved.
ISSN: 0019-0578
DOI: 10.1016/j.isatra.2008.11.001
Appears in Collections:電機工程學系所

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