Approaches to Optimizing Guidance Methods to High-Speed Intensively Maneuvering Targets. Part I. Justifying Requirements for Ways to Optimize Guidance Methods
V. S. Verba a, * and V. I. Merkulov a, **
a JSC Concern Vega, Moscow, Russia
*email: vvs.msk@gmail.com
**email: mvipost4i@gmail.com
Received 19 March, 2024
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
DOI: 10.1134/S0005117924700267