Simulation of quadcopter flight altitude stabilization system

Authors

  • Mikhail Yu. Babich Department Main Specialist JSC Research and Production Enterprise
  • Mikhail M. Butaev Department Main Specialist JSC Research and Production Enterprise
  • Dmitry V. Pashchenko Penza State Technological University
  • Alexey I. Martyshkin Department of Computational Machines and Systems, Penza State Technological University
  • Dmitry A. Trokoz Penza State Technological University

DOI:

https://doi.org/10.5377/nexo.v33i02.10799

Keywords:

quadrocopter, flight altitude stabilization, unmanned aerial vehicle, modeling, multicopter, algorithm, implementation

Abstract

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.

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Published

2020-12-31

How to Cite

Yu. Babich, M., M. Butaev, M., Pashchenko, D. V., Martyshkin, A. I., & Trokoz, D. A. (2020). Simulation of quadcopter flight altitude stabilization system. Nexo Scientific Journal, 33(02), 638–650. https://doi.org/10.5377/nexo.v33i02.10799

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