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How to Choose Parameters of the On-Board System for a Quadcopter Control

  • AUTOMATION AND CONTROL IN ENGINEERING
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Abstract

The issue of how to simulate and choose parameters of the on-board system for controlling a quadcopter is examined in this paper. The examined system controls simultaneously the quadcopter’s rotation angles and its linear displacement. The procedure for calculating the orientation angles and torques of the drivers of the lifting propellers determining the orientation of the quadcopter and the thrust value and direction is presented. The initial equations for calculating the thrust and rotation torques are obtained. It is shown that control of the quadcopter is different from classical approach for motion of a solid considering the center of mass displacement and its required orientation. It is shown that the orientation angles are not independent coordinates and they are set by considering the condition for securing the thrust directions of lifting rotors aiming to secure the center of mass motion of the quadcopter along the given trajectory.

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REFERENCES

  1. Pyrkin, A.A., Mal’tseva, T.A., Labadin, D.V., Surov, M.O., and Bobtsov, A.A., Synthesis of control system for a quadcopter with the use of a simplified mathematical model, Izv. Vyssh. Uchebn. Zaved. Priborostr., 2013, vol. 56, no. 4, pp. 47–51.

    Google Scholar 

  2. Luukkonen, T., Modelling and control of quadcopter, Espoo: Aalto University, 2011. http://sal.aalto.fi/publications/pdf-files/eluu11_public.pdf.

    Google Scholar 

  3. Gur’yanov, A.E., Modeling of quadcopter control, Inzh. Vestn., 2014, no. 8, p. 4.

  4. Pavlovskii, V.E. and Savitskii, A.V., The solving of inverse problem for the computation of control action for quadrocopter, Preprint of the Keldysh Inst. of Applied Mathematics, Russ. Acad. Sci., 2017, no. 17. https://doi.org/10.20948/prepr-2017-17

  5. Tsokurova, I.G., Denisov, A.N., Samoilenko, S.A., and Ostapchuk, M.L., Application of quadcopter UAVs DJI Inspire 1V 2.0 in searching for persons on the ground, Nauka, Tekh. Obraz., 2018, no. 11, pp. 43–46.  https://doi.org/10.20861/2312-8267-2018-52-005

  6. Krasovskii, A.N. and Suslova, O.A., On the mathematical model of the controlled motion of a drone-quadrocopter, Agrar. Vestn. Urala, 2016, no. 4, pp. 55–59.

  7. Shilov, K.E., Development of automatic control system for rotor-type unmanned aerial vehicle, Tr. Mosk. Fiz.-Tekh. Inst., 2014, vol. 6, no. 4, pp. 139–152.

    Google Scholar 

  8. Kanatnikov, A.N., Plane motion control of quadcopter, Mat. Mat. Mod., 2015, no. 2, pp. 23–36.

  9. Gen, K.K. and Chulin, N.A., Stabilization algorithms for automated trajectory motion control of quadcopter, Nauka Obraz.: Nauchn. Izd. Mosk. Gos. Tekh. Univ. im. Baumana, 2015, no. 5, pp. 218–235.  https://doi.org/10.7463/0515.0771076

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Correspondence to V. L. Afonin or V. V. Sleptsov.

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The authors declare that they have no conflicts of interest.

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Translated by Yu.V. Zikeeva

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Afonin, V.L., Sleptsov, V.V. How to Choose Parameters of the On-Board System for a Quadcopter Control. J. Mach. Manuf. Reliab. 51, 659–667 (2022). https://doi.org/10.3103/S1052618822070020

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  • DOI: https://doi.org/10.3103/S1052618822070020

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