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Author/Affiliation: Hiroyuki TakanoOpen AccessArticle
9 Pages, 1,410 KB 
Guidance Law Based on Line-of-Sight Rate Information Considering Uncertain Modeled Dynamics
Abstract:
Proportional navigation (PN) is a widely-used guidance law for missiletarget engagement. The goal of the missile intercept problem is to reduce the closest distance between the missile and target by diminishing the line-of-sight rate (LOS rate). In general, PN guidance law necessitates information of the LOS rate and missile velocity. The closing velocity (relative approaching…
Read More(This article belongs to the SP5 (Special Issue on Multidisciplinary Sciences and Engineering 2018) & Section Aerospace Engineering (EAR))