Fuzzy Logic-based Terminal Guidance with Impact Angle Control

Authors

  • Samir Chabra Defence Institute of Advanced Technology, Pune
  • S.E. Talole Defence Institute of Advanced Technology, Pune

DOI:

https://doi.org/10.14429/dsj.57.1782

Keywords:

Terminal guidance, fuzzy logic control, impact angle control, reentry guidance

Abstract

This paper presents a new formulation of terminal guidance law which controls the impactattitude angle while minimising the miss distance.  The formulation is based on the fuzzy logic-control approach.  Unlike many prevalent designs, the proposed guidance law does not requirelinearisation of missile-target engagement model. Numerical simulation results demonstrate thatthe proposed guidance law offers satisfactory performance, fulfilling its design goals.

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Published

2007-07-01

How to Cite

Chabra, S., & Talole, S. (2007). Fuzzy Logic-based Terminal Guidance with Impact Angle Control. Defence Science Journal, 57(4), 351–360. https://doi.org/10.14429/dsj.57.1782

Issue

Vol. 57 No. 4

Section

Aeronautical Systems

License

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