Fuzzy Logic-based Terminal Guidance with Impact Angle Control

Defence Science Journal

S.E. Talole¹  Samir Chabra¹ 

[1] Defence Institute of Advanced Technology, Pune

关键词: Terminal guidance;    fuzzy logic control;    impact angle control;    reentry guidance;   

DOI  :  

学科分类：社会科学、人文和艺术（综合）

来源: Defence Scientific Information & Documentation Centre

【 摘 要 】

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.

【 授权许可】

Unknown