Guided Missile with an Intelligent Agent

Defence Science Journal

K.N. Swamy¹  N Bharadwaj¹  V. Krishnabrahmam¹  V.V.S. Sarma² 

[1] Defence Research & Development Laboratory, Hyderabad;Indian Institute of Science, Bangalore

关键词: Guided missiles;    Proportional navigational algorithm;    Targets;    Fly by wire technology;    Control loops;   

DOI  :  

学科分类：社会科学、人文和艺术（综合）

来源: 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.

【 授权许可】

Unknown