Efficient control of the direction of thrust during highspeed maneuver in the plane

The controlled motion of an inertial object during a high-speed maneuver in a vertical plane is investigated. The generated thrust is limited in magnitude, the control is the angle that sets its direction, the initial velocity is generally non-zero, and external forces are not considered. The goal i...

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Bibliographic Details
Main Authors: Sergey A. Reshmin, Madina T. Bektybaeva
Format: Article
Language:English
Published: Peoples’ Friendship University of Russia (RUDN University) 2023-12-01
Series:RUDN Journal of Engineering Research
Subjects:
Online Access:https://journals.rudn.ru/engineering-researches/article/viewFile/37067/22837