文章基本信息

标题：Guided Missile with an Intelligent Agent
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作者：V. Krishnabrahmam ; N Bharadwaj ; K.N. Swamy 等
期刊名称：Defence Science Journal
印刷版ISSN：0976-464X
出版年度：2013
卷号：50
期号：1
页码：25-30
DOI：10.14429/dsj.50.3319
语种：English
出版社：Defence Scientific Information & Documentation Centre
摘要：Guided missiles involve the use of a conventional deviated pursuit course like proportionalnavigation algorithm and its variants, which is optimal when the speed advantage of the guided missile is veryhighandthe target maneouvering is minimal. Against the present-day aircraft,whichemploys fly-by-wire technology for high maneouverability andhigh speed, missiles needto have amuchhigher speed advantage or to use a combination of artificial intelligence and modern controlalgorithms. Results of simulation of pursuit and evasion with an autonomous intelligent agentincorporated in the control loop are presented.
关键词：Guided missiles;Proportional navigational algorithm;Targets;Fly by wire technology;Control loops