Approaches to Optimizing Guidance Methods to High-Speed Intensively Maneuvering Targets. Part I. Justifying Requirements for Ways to Optimize Guidance Methods

Abstract

High-speed aircraft capable of complex spatial maneuvers and having several technical, economic, and tactical advantages are increasingly used in aerospace warfare. In this regard, a topical problem is to optimize interception systems for such targets. The operation features of interception systems are considered based on analyzing flight path features of high-speed aircraft. Requirements for ways to optimize guidance methods are formulated.