THE DYNAMICS CONTROL OF THE RIGID WING UAV BY THE EXAMPLE OF USING LQR, LQG AND NONLINEAR CONTROL METHODS
https://doi.org/10.33236/2307-910X-2019-2-26-74-82
Abstract
Small - sized fixed-wing unmanned aerial vehicles (UAVs) have become a popular research topic in recent years.
About the Authors
A. A. Sclyarov
Southern Federal University
Russian Federation
Russian Federation
A. Ingabire
Southern Federal University
Russian Federation
Russian Federation
References
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Review
For citations:
Sclyarov A.A., Ingabire A. THE DYNAMICS CONTROL OF THE RIGID WING UAV BY THE EXAMPLE OF USING LQR, LQG AND NONLINEAR CONTROL METHODS. Modern Science and Innovations. 2019;(2):74-82. (In Russ.) https://doi.org/10.33236/2307-910X-2019-2-26-74-82
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