Fuzzy Logic-based Terminal Guidance with Impact Angle Control
Keywords: Terminal guidance, fuzzy logic control, impact angle control, reentry guidance
AbstractThis 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.
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
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