Simulation of quadcopter flight altitude stabilization system

Recently, unmanned aerial vehicles have been an important part of scientific research in various fields. Quadrocopter is an unmanned aerial vehicle with four rotors, two of which rotate clockwise, the other two counterclockwise. Changing the speed of screw rotation allows you to control the movement...

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Veröffentlicht in:Nexo (Managua, Nicaragua) Nicaragua), 2020-12, Vol.33 (2), p.638-650
Hauptverfasser: Yu. Babich, Mikhail, M. Butaev, Mikhail, Pashchenko, Dmitry V., Martyshkin, Alexey I., Trokoz, Dmitry A.
Format: Artikel
Sprache:eng
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Beschreibung
Zusammenfassung:Recently, unmanned aerial vehicles have been an important part of scientific research in various fields. Quadrocopter is an unmanned aerial vehicle with four rotors, two of which rotate clockwise, the other two counterclockwise. Changing the speed of screw rotation allows you to control the movement of the apparatus. The article proposed and tested a mathematical model of a quadcopter. They presented the development of a simple control algorithm that allows to stabilize the height and angular position. The research results show the efficiency of the algorithm and the possibility of its practical implementation. The developed mathematical model can be used instead of a real quadcopter, which will significantly reduce the time during research, as well as avoid the quadrocopter damage, reducing the number of launches.
ISSN:1818-6742
1995-9516
DOI:10.5377/nexo.v33i02.10799