Conditions of unmanned aerial vehicle robust stabilization with incomplete definiteness of the mathematical model and external perturbations is considered. The synthesis of an optimal unmanned aerial vehicle control system based on the system with variable structure is presented for the criterion of minimum energy consumption. Formation of compounding and corrective feedbacks to ensure minimal errors of the robust stabilization of the unmanned aerial vehicle is proposed. The simulation results of the stabilization process in the form of “error tubes” are presented demonstrating the effectiveness of the proposed approach.
Control Systems with Suboptimal Models for Stabilization of UAV
01.10.2019
481344 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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