A method to maneuver aeroballistic missiles under counteractions

DOI10.1134/S1064230717030108zbMath1384.93088OpenAlexW2727103138MaRDI QIDQ1745840

L. D. Gorchenko, V. I. Goncharenko

Publication date: 18 April 2018

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230717030108

zbMATH Keywords

trajectory planninganti-interception maneuverhigh-speed aeroballistic missile

Mathematics Subject Classification ID

Application models in control theory (93C95) Automated systems (robots, etc.) in control theory (93C85) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• Terminal open-loop control for a hypervelocity unmanned flying vehicle in the atmosphere. Part I
• Self-guiding of a high velocity pilotless aircraft on the terminal flight leg in atmosphere
• Path planning for unmanned aerial vehicle under complicated conditions and hazards
• Trajectory control of a high altitude hypervelocity flying vehicle in the midcourse active phase of the flight

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