The article is devoted to the synthesis of robust controllers of supersonic unmanned aerial vehicle motion parameters. During the flight, the velocity and altitude of the aircraft varies rapidly within wide limits. Therefore, the required quality of control on each trajectory is provided by a set of dynamic controllers with constant coefficients. The article substantiates the number of such controllers, researches the range of their efficiency. The obtained restrictions on the amplitude-frequency characteristics and weight functions are given. Transients are shown.
Robust controller for supersonic unmanned aerial vehicle
2019
Article (Journal)
Electronic Resource
Unknown
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UNMANNED AERIAL VEHICLE AND REMOTE CONTROLLER FOR THE UNMANNED AERIAL VEHICLE
European Patent Office | 2017
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