{"id":3519,"date":"2025-08-06T13:27:51","date_gmt":"2025-08-06T12:27:51","guid":{"rendered":"https:\/\/izvestiyakbncran.ru\/?page_id=3519"},"modified":"2026-04-13T10:00:14","modified_gmt":"2026-04-13T09:00:14","slug":"27-3-4-en","status":"publish","type":"page","link":"https:\/\/izvestiyakbncran.ru\/index.php\/en\/27-3-4-en\/","title":{"rendered":"27.3.4 En"},"content":{"rendered":"\n<h1 class=\"wp-block-heading has-lora-font-family\" style=\"font-size:24px\"><strong>The effect of electromagnetic processes on gyroscope readings in BLDC motors<\/strong><\/h1>\n\n\n\n<p class=\"has-foreground-color has-text-color has-link-color has-lora-font-family has-extra-small-font-size wp-elements-077918335f8aa9ba44b3a36f06b145ab\" style=\"margin-top:0;margin-bottom:0;padding-top:0;padding-bottom:0\"><strong><strong><strong><strong><strong><strong><strong><strong><strong><strong><strong><strong>H. Pham Trong, A.A. Shilin, M.T. Nguyen<\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/strong><\/p>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity is-style-wide\" style=\"margin-top:var(--wp--preset--spacing--20);margin-bottom:var(--wp--preset--spacing--20)\"\/>\n\n\n\n<div class=\"wp-block-group is-nowrap is-layout-flex wp-container-core-group-is-layout-24a27e19 wp-block-group-is-layout-flex\" style=\"margin-top:0;margin-bottom:0;padding-top:0;padding-bottom:0\">\n<p class=\"has-text-color has-link-color has-lora-font-family has-extra-small-font-size wp-elements-fa99f84d8051eb763ab85c3007cdb1c2\" style=\"color:#5b1919;text-decoration:underline\"><strong><strong>Upload the full text<\/strong><\/strong><\/p>\n\n\n\n<div class=\"wp-block-group is-vertical is-layout-flex wp-container-core-group-is-layout-9151b400 wp-block-group-is-layout-flex\" style=\"min-height:0px;margin-top:0;margin-bottom:0;padding-top:0;padding-bottom:0\">\n<div class=\"wp-block-buttons is-content-justification-left is-layout-flex wp-container-core-buttons-is-layout-15bf754d wp-block-buttons-is-layout-flex\" style=\"margin-top:0;margin-bottom:0;padding-top:0;padding-right:0;padding-bottom:0;padding-left:0\">\n<div class=\"wp-block-button has-custom-width wp-block-button__width-100 is-style-outline is-style-outline--1\"><a class=\"wp-block-button__link has-background-background-color has-text-color has-background has-link-color has-border-color has-small-font-size has-custom-font-size wp-element-button\" href=\"http:\/\/izvestiyakbncran.ru\/wp-content\/uploads\/2025\/07\/fam-chong-shilin-nguen-4.pdf\" style=\"border-color:#5b1919;border-style:solid;border-width:2px;border-radius:8px;color:#5b1919;padding-top:0.4rem;padding-right:var(--wp--preset--spacing--40);padding-bottom:0.4rem;padding-left:var(--wp--preset--spacing--40)\">PDF<\/a><\/div>\n<\/div>\n\n\n\n<div style=\"height:0px;width:0px\" aria-hidden=\"true\" class=\"wp-block-spacer wp-container-content-273e683f\"><\/div>\n<\/div>\n<\/div>\n\n\n\n<p class=\"has-foreground-color has-text-color has-link-color has-lora-font-family has-extra-small-font-size wp-elements-68c557e6f216aaa91cba7dfee47c26e8\" style=\"line-height:1.4\"><em><strong><strong>Abstract<\/strong>.<\/strong> <\/em>The relevance of the work lies in the fact that vibration interference due to the operation of quadrocopter engines remains one of the key reasons for the deterioration in accuracy and stability of drone control systems. This interference, caused by a flux switching motor, can significantly affect the accuracy of accelerometer and gyroscope readings, reducing the overall navigation and stabilisation performance. Therefore, studying the properties of such disturbances and their influence on quadrocopter dynamics is an important and practical task. The objective of this paper is to determine vibration properties caused by flux switching motor, as well as their effect on quadrocopter performance. <strong>Methods<\/strong>. The methods of mathematical modelling, spectral analysis and experimental investigations are used in this work. <strong>Results<\/strong>. This paper proposes a modification to the quadrocopter model that considers these interferences. Modelling and experimental results confirm that vibration frequency is related to engine control and is present in the thrust force spectrum, which in turn is reflected in the readings from the gyroscope and accelerometer. The necessity of taking vibration noise into account for qualitative synthesis of quadrocopter control systems, as well as the development of new noise-tolerant algorithms is emphasized. <strong>Conclusions<\/strong>. Further research could focus on optimising the control architecture to account for the identified spectral interference. It could also involve developing more efficient filters that could deliver high performance and accuracy when noise interference is included<\/p>\n\n\n\n<p class=\"has-foreground-color has-text-color has-link-color has-lora-font-family has-extra-small-font-size wp-elements-c9fdaf32b1204355dd841a1521687608\" style=\"line-height:1.4\"><strong><em><strong>Keywords<\/strong>:<\/em><\/strong> BLDC motor, spectral component, disturbances, mathematical expectation, quadcopter, variance<\/p>\n\n\n\n<p class=\"has-foreground-color has-text-color has-link-color has-lora-font-family wp-elements-a2e09714524b503813bcbe10bfb9ffce\" style=\"font-size:12px;line-height:1.4\"><strong><strong>For citation<\/strong>.<\/strong> H. Pham Trong, Shilin A.A., Nguyen M.T The effect of electromagnetic processes on gyroscope readings in BLDC motors. <em>News of the Kabardino-Balkarian Scientific Center of RAS.<\/em> 2025. Vol. 27. No. 3. Pp. 55\u201372. DOI: 10.35330\/1991-6639-2025-27-3-55-72<\/p>\n\n\n\n<details class=\"wp-block-details has-foreground-color has-text-color has-link-color has-lora-font-family has-extra-small-font-size wp-elements-f382e56a95e533d1154718778307e6c9 is-layout-flow wp-container-core-details-is-layout-0ab540ad wp-block-details-is-layout-flow\" style=\"font-style:normal;font-weight:700;line-height:1.5\"><summary><strong>R<\/strong>eferences<\/summary>\n<ol style=\"margin-top:0;margin-bottom:0\" class=\"wp-block-list\">\n<li style=\"font-style:normal;font-weight:400\">Kurak S., Migdat H. Control and estimation of a quadcopter dynamical model. Periodicals of Engineering and Natural Sciences (PEN). 2018. Vol. 6. No. 1. Pp. 63\u201375. DOI: 10.21533\/pen.v6i1.164<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Cao N., Alan F.L. Inner\u2013outer loop control for quadrotor UAVs with input and state constraints. IEEE Transactions on Control Systems Technology. 2015. Vol. 2. No. 5. Pp. 1797\u20131804. 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DOI: 10.3390\/app13063464<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Belov N.V., Boris B.Ya. Building a mathematical model for controlling UAV altitude and angles of motion. Telecommunications and Information Technologies. 2018. Vol. 5. No. 1. Pp. 100\u2013111. EDN: UROPEO. (In Russian)<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Oloo J.O. Design of extended kalman filter optimized fuzzy PID controller for a quadcopter in the event of one rotor failure: Dis. JKUAT-COETEC. 2021. 71 p.<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Kalachev Yu.N. SimInTech: modeling in electric drive. Moscow: DMK Press, 2022. Pp. 26\u201333. (In Russian)<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Bahari N.B., Jidin A.B., Abdullah M.N. et al. Modeling and simulation of torque hysteresis controller for brushless DC motor drives. IEEE Symposium on Industrial Electronics and Applications. Bandung, Indonesia. 2012. Pp. 152\u2013155.<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Myasishchev A.A. Programming ESC controllers with SimonK and BLHeli firmware via Arduino and a flight controller. Electronic resource. 2019. Available at: https:\/\/www.researchgate.net publication\/332381105. (In Russian)<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Yadav P.M., Gadgune S.Y. Position and speed control of brushless DC motors using sensorless techniques: A review. International Journal of Engineering Research &amp; Technology. Vol. 8. No. 1. Pp. 62\u201369.<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Dasari M., Reddy A.S., Kumar M.V. Modeling of a commercial BLDC motor and control using GA-ANFIS tuned PID controller. International Conference on Innovative Research In Electrical Sciences (IICIRES). Nagapattinam, India. 2017. Pp. 1\u20136. DOI: 10.1109\/IICIRES.2017.8078305<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Yamashita R.Y., Silva L.M., Santiciolli F.M. et al. Comparison between two models of BLDC motor, simulation and data acquisition. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2018. Vol. 40. ID: 63. DOI: 10.1007\/s40430-018-1020-0<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Ascorti L. An application of the extended Kalman filter to the attitude control of a quadrotor: Dis. Biblioteche e Archivi. 2012. Pp. 45\u201349.<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Kiruthika A., Rajan A.A., Rajalakshmi P. Mathematical modelling and speed control of a sensored brushless DC motor using intelligent controller. IEEE International Conference ON Emerging Trends in Computing, Communication and Nanotechnology (ICECCN). Tirunelveli, India. 2013. Pp. 211\u2013216. DOI: 10.1109\/ICE-CCN.2013.6528495<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Hai P.T. Reasearh data for this article. URL: https:\/\/github.com\/tronghai180598\/1_articles (accessed: 30.05.2025).<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">John B. Quadcopter Simulation and Control. Dynamics generated with PyDy. Available at: https:\/\/github.com\/bobzwik\/Quadcopter_SimCon (accessed: 05.10.2024).<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">C\u00e1rdenas R.C., Morales C.A.C., Ospina J.P. et al. Mathematical modeling and identification of a quadrotor. Computational Science and Its Applications \u2013 ICCSA 2020: 20th International Conference. Cagliari, Italy, July 1\u20134, 2020, Proceedings, Part I 20. Springer International Publishing. 2020. Pp. 261\u2013275. DOI: 10.1007\/978-3-030-58799-4_19<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Abdelhay S., Alia Z. Modeling of a quadcopter trajectory tracking system using PID controller. Procedia Manufacturing. 2019. Vol. 32. Pp. 564\u2013571. DOI: 10.1016\/j.promfg.2019.02.253<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Nguyen N.P., Ming N.X., Thanh H.l.N.N. et al. Adaptive sliding mode control for attitude and altitude system of a quadcopter UAV via neural network. IEEE Access. 2021. Vol. 9. Pp. 40076\u201340085. DOI: 10.1109\/ACCESS.2021.3064883<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Hoffmann F., Niklas G., Torsten B. Attitude estimation and control of a quadrocopter. IEEE \/ RSJ International Conference on Intelligent Robots and Systems. 2010. P. 10721077.<br>DOI: 10.1109\/IROS.2010.5649111<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Kalachev O. How I developed a quadcopter on ESP32 from scratch, Khabr. Available at: https:\/\/github.com\/okalachev\/flix. (In Russian)<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Open Source Autopilot For Drone Developers \/\/ PX4. URL: https:\/\/github.com\/px4\/px4-autopilot\/ (accessed: 25.06.2024).<\/li>\n\n\n\n<li style=\"font-style:normal;font-weight:400\">Zhmud V.A., Kuznetsov K.A., Kondratyev N.O. et al. Accelerometer and gyroscope MPU6050: first inclusion on STM32 and study of readings in statics. Avtomatizatsiya i programmnaya inzheneriya [Automation and software engineering]. 2018. Vol. 3. No. 25. Pp. 9\u201322. EDN: YALYRF. (In Russian)<\/li>\n<\/ol>\n<\/details>\n\n\n\n<details class=\"wp-block-details has-foreground-color has-text-color has-link-color has-lora-font-family has-extra-small-font-size wp-elements-a6e3ecb54e8a726458f80f94e0653d3a is-layout-flow wp-container-core-details-is-layout-5dafc681 wp-block-details-is-layout-flow\" style=\"font-style:normal;font-weight:700;line-height:1.5\"><summary><strong>Information about the authors<\/strong><\/summary>\n<div class=\"wp-block-group is-vertical is-layout-flex wp-container-core-group-is-layout-b291ae12 wp-block-group-is-layout-flex\" style=\"min-height:0px;margin-top:0;margin-bottom:0;padding-top:var(--wp--preset--spacing--20);padding-right:var(--wp--preset--spacing--40);padding-bottom:var(--wp--preset--spacing--20);padding-left:var(--wp--preset--spacing--40)\">\n<p style=\"font-style:normal;font-weight:400\"><strong>Hai Pham Trong<\/strong>, Graduate student in the Electrical power Engineering Department of the School<br>of Energy Engineering, Tomsk Polytechnic University;<br>634050, Russia, Tomsk, 7 Usova street;<br>tronghai180598@gmail.ru, ORCID: https:\/\/orcid.org\/0009-0004-6272-890X<br><strong>Alexander A. Shilin<\/strong>, Doctor of Technical Sciences, Associate Professor, Professor of the Department,<br>Electrical power Engineering Department of the School of Energy Engineering, Tomsk Polytechnic University;<br>634050, Russia, Tomsk, 7 Usova street;<br>shilin@tpu.ru; ORCID: https:\/\/orcid.org\/0000-0002-4761-7249, SPIN-code: 2790-9730<br><strong>Minh Tuong Nguyen<\/strong>, Candidate of Engineering Sciences, Associate Professor of the Department of<br>Informatics, MIREA \u2013 Russian Technological University;<br>119454, Russia, Moscow, 78 Vernadsky avenue;<br>nguen_m@mirea.ru, ORCID: https:\/\/orcid.org\/0009-0002-7267-1121, SPIN-code: 5480-9970<\/p>\n\n\n\n<p style=\"font-style:normal;font-weight:400\"><\/p>\n\n\n\n<p style=\"font-style:normal;font-weight:400\"><\/p>\n<\/div>\n<\/details>\n","protected":false},"excerpt":{"rendered":"<p>The effect of electromagnetic processes on gyroscope readings in BLDC motors H. Pham Trong, A.A. Shilin, M.T. Nguyen Upload the full text Abstract. The relevance of the work lies in the fact that vibration interference due to the operation of quadrocopter engines remains one of the key reasons for the deterioration in accuracy and stability [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"wp-custom-template-home","meta":{"footnotes":""},"class_list":["post-3519","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.5 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>27.3.4 En - \u0418\u0417\u0412\u0415\u0421\u0422\u0418\u042f \u041a\u0410\u0411\u0410\u0420\u0414\u0418\u041d\u041e-\u0411\u0410\u041b\u041a\u0410\u0420\u0421\u041a\u041e\u0413\u041e \u041d\u0410\u0423\u0427\u041d\u041e\u0413\u041e \u0426\u0415\u041d\u0422\u0420\u0410 \u0420\u0410\u041d\u00bb<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/izvestiyakbncran.ru\/index.php\/en\/27-3-4-en\/\" \/>\n<meta property=\"og:locale\" content=\"ru_RU\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"27.3.4 En - \u0418\u0417\u0412\u0415\u0421\u0422\u0418\u042f \u041a\u0410\u0411\u0410\u0420\u0414\u0418\u041d\u041e-\u0411\u0410\u041b\u041a\u0410\u0420\u0421\u041a\u041e\u0413\u041e \u041d\u0410\u0423\u0427\u041d\u041e\u0413\u041e \u0426\u0415\u041d\u0422\u0420\u0410 \u0420\u0410\u041d\u00bb\" \/>\n<meta property=\"og:description\" content=\"The effect of electromagnetic processes on gyroscope readings in BLDC motors H. 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Pham Trong, A.A. Shilin, M.T. Nguyen Upload the full text Abstract. 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