Terminal open-loop control for a hypervelocity unmanned flying vehicle in the atmosphere. Part I

DOI10.1134/S1064230711050121zbMath1266.93104MaRDI QIDQ353707

M. N. Krasil'shchikov, K. I. Sypalo

Publication date: 16 July 2013

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

zbMATH Keywords

algorithmhypervelocity flying vehiclerational hitting trajectoryterminal open-loop control

Mathematics Subject Classification ID

Application models in control theory (93C95) Automated systems (robots, etc.) in control theory (93C85)

Related Items (3)

A method to maneuver aeroballistic missiles under counteractions ⋮ Adaptive three-dimensional guidance of flying vehicle at fixed point with specified approach direction ⋮ Trajectory control of a high altitude hypervelocity flying vehicle in the midcourse active phase of the flight

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