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Annotation to the degree project of the student Bogoslavets

Robust controller of unmanned aerial vehicle motion parameters on aeroballistic trajectory is developed. Synthesis was carried out using the 2-Riccati approach of the -theory. In the presence of control object model parametric disturbances, the regulator provides the specified quality of the transient process, as well as the absence of a static error in the control of a velocity bearing angle. The regulator turns the control body on the basis of information only about the velocity bearing angle. The results of simulation of the synthesized robust controller, as well as the PID controller under the same conditions, are presented.

Key words: unmanned aerial vehicle, robust controller, velocity bearing angle

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