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This article is cited in 2 scientific papers (total in 2 papers)
Control in Technical Systems
Approaches to optimizing guidance methods to high-speed intensively maneuvering targets. Part I. Justifying requirements for ways to optimize guidance methods
V. S. Verba, V. I. Merkulov Concern of radio engineering Vega, Moscow
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.
Keywords:
high-speed aircraft, complex maneuver, interception system, guidance method, optimization, statistical theory of optimal control, inverse dynamics problems, gradient method, intelligent control.
Citation:
V. S. Verba, V. I. Merkulov, “Approaches to optimizing guidance methods to high-speed intensively maneuvering targets. Part I. Justifying requirements for ways to optimize guidance methods”, Avtomat. i Telemekh., 2024, no. 11, 73–80; Autom. Remote Control, 85:11 (2024), 990–994
Linking options:
https://www.mathnet.ru/eng/at16296 https://www.mathnet.ru/eng/at/y2024/i11/p73
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