This paper deals with studying control systems of quadcopter motion. A detailed review of the technical literature in this area has been done. The basic ways of the synthesis of the control system are represented. The main characteristics of the two-stage design procedure are given. The basic steps of the above-mentioned procedure are represented. The results of carrying out this design procedure are given. Transient processes of the basic components of the vector state are shown. Results of the simulation of the quadcopter motion are shown. The basic characteristics of the synthesized system are calculated.
Synthesis and Modelling of Control System for Quadrotor Motion
22.10.2024
354615 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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