Guided Missile with an Intelligent Agent

Authors

  • V. Krishnabrahmam Defence Research & Development Laboratory, Hyderabad
  • N Bharadwaj Defence Research & Development Laboratory, Hyderabad
  • K.N. Swamy Defence Research & Development Laboratory, Hyderabad
  • V.V.S. Sarma Indian Institute of Science, Bangalore

DOI:

https://doi.org/10.14429/dsj.50.3319

Keywords:

Guided missiles, Proportional navigational algorithm, Targets, Fly by wire technology, Control loops

Abstract

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.

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Published

2013-01-01

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

Issue

Vol. 50 No. 1

Section

Aeronautical Systems

License

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