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.
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