Fuzzy Logic-based Terminal Guidance with Impact Angle Control

  • Samir Chabra Defence Institute of Advanced Technology, Pune
  • S.E. Talole Defence Institute of Advanced Technology, Pune
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.
Published
2007-07-01
How to Cite
ChabraS., & TaloleS. (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
Section
Aeronautical Systems