Guided Missile with an Intelligent Agent
Keywords: Guided missiles, Proportional navigational algorithm, Targets, Fly by wire technology, Control loops
AbstractGuided 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.
How to Cite
Krishnabrahmam, V., Bharadwaj, N., Swamy, K., & Sarma, V. (2013). Guided Missile with an Intelligent Agent. Defence Science Journal, 50(1), 25-30. https://doi.org/10.14429/dsj.50.3319
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