Motion control problems for multimode unmanned aerial vehicles
- Authors: Syrov A.S.1, Puchkov A.M.1, Rutkovskii V.Y.2, Glumov V.M.2
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Affiliations:
- Mars Moscow Experimental Design Bureau
- Trapeznikov Institute of Control Sciences
- Issue: Vol 78, No 6 (2017)
- Pages: 1128-1137
- Section: Control Sciences
- URL: https://ogarev-online.ru/0005-1179/article/view/150622
- DOI: https://doi.org/10.1134/S0005117917060121
- ID: 150622
Cite item
Abstract
This paper considers flight control specifics for modern unmanned aerial vehicles with paths described by a wide range of altitudes, including super-aerodynamic flights. It is noted that this type of aerial vehicles belongs to multimode dynamic objects with varying characteristics in the course of their operation. Adaptive control methods used in control systems for unmanned aerial vehicles are overviewed. Finally, adaptive control capabilities are studied for the vehicle’s angular position in gliding and cruising modes under combined jet reaction and aerodynamic control.
About the authors
A. S. Syrov
Mars Moscow Experimental Design Bureau
Author for correspondence.
Email: office@mokb-mars.ru
Russian Federation, Moscow
A. M. Puchkov
Mars Moscow Experimental Design Bureau
Email: office@mokb-mars.ru
Russian Federation, Moscow
V. Yu. Rutkovskii
Trapeznikov Institute of Control Sciences
Email: office@mokb-mars.ru
Russian Federation, Moscow
V. M. Glumov
Trapeznikov Institute of Control Sciences
Email: office@mokb-mars.ru
Russian Federation, Moscow
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