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This paper considers the comparative analysis of the physical and mathematical methods of the optimal operation of aviation objects’ automatic control systems, which is an urgent scientific and technical task. The paper also represents the corresponding stability criteria, depending on the operating conditions, and the influence of external factors that allows ensuring the automatic control systems’ reliable operation not only in normal circumstances, but also in the presence of probable disagreements. The scientific novelty of the research lies in developing new stability criteria by means of synthesising the influence of different factors and also the ability to ensure optimal functioning of the automatic control systems. Corresponding mathematical and computer models have been developed. The use of these models allows to determine the optimal stability criteria for control systems with parameters of a different physical nature and ensure reliable operation of electromechanical systems for general and special applications based on the current analysis. The research results are illustrated by corresponding mathematical models, engineering calculations and modelling of the optimal control limits depending on the influence of various factors. The simulation results coincide with the theoretical calculations, which indicates the consistency between the microprocessor-based and software of automatic control systems.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
45--70
Opis fizyczny
Bibliogr. 17 poz., fot., rys., wzory
Twórcy
autor
- Electrical Engineering Department National University of Zaporizhzhya Polytechnic Zaporizhzhya, 64 Zhukovsky Street, Zaporizhzhya, 69063, Ukraine
autor
- Electrical Engineering Department National University of Zaporizhzhya Polytechnic Zaporizhzhya, 64 Zhukovsky Street, Zaporizhzhya, 69063, Ukraine
autor
- Electrical Engineering Department National University of Zaporizhzhya Polytechnic Zaporizhzhya, 64 Zhukovsky Street, Zaporizhzhya, 69063, Ukraine
autor
- PJSC «Titanium Institute», 180 Sobornyi Avenue, Zaporizhzhya, 69035, Ukraine
Bibliografia
- [1] Delas N., Kasyanov V. Extremely hyperbolic law of distribution [Predelno giperbolicheskiy zakon raspredeleniya]. In: Sbornik nauchnykh trudov Mezhdunarodnoy nauchnoy konferentsii «Intellektualnye sistemy prinyatiya resheniy i problemy vychislitelnogo intellekta» (International Conference «Intellectual Systems for Decision Making and Problems of Computational Intelligence»); Evpatoria; 2012. p. 67-8.
- [2] Loh R., Bian Y., Roe T. UAVs in civil airspace: safety requirements. IEEE Aerosp Electron Syst Mag. 2009 Jan;24:5-17.
- [3] Shanyavskiy A. Bezopasnoe ustalostnoe razrushenie elementov aviakonstruktsiy. Sinergetika v inzhenernykh prilozheniyakh [Safe fatigue failure of elements of aircraft structures. Synergetics in engineering applications]. [place unknown]: Ufa; 2003. 803 p.
- [4] Steinberg M. A historical overview of research in reconfigurable flight control. Proc Inst Mech Eng G. 2005 Apr;219:267-75.
- [5] Lin X., Fulton N., Horn M. Quantification of high level safety criteria for civil unmanned aircraft systems. Proc IEEE Aerosp Conf [Internet]. 2014:1-13. Available from: https://doi.org/10.1109/AERO.2014.6836463
- [6] Zinovkin V. Zbirnyk tez dopovidej Vseukrai'ns'koi' naukovoi' konferencii' «Elektroenergetyka, elektrotehnika ta elektromehanika: zastosuvannja, doslidzhennja, osvita». Odesa: Ministerstvo oborony Ukrai'ny. Vijs'kova akademija; 2021. Umovy optymal'nogo funkcionuvannja bagatoparametrychnyh tehnologichnyh ob’jektiv. [conditions for optimal functioning of multi-parameter technological objects.]; p. 53-5.
- [7] Zinovkin V., Antonov M., Krysan I. Multi-Parameter technological proces optimization functional similarity criteria. In: 2021 IEEE 2nd KhPI Week on Advanced Technology (KhPIWeek) [Internet]; 2021 Sep 13-17; Kharkiv, Ukraine. [place unknown: publisher unknown]; 2021. p. 490-5. Available from: https://doi.org/10.1109/KhPIWeek53812.2021.9570014
- [8] Kozak V., Shevchuk D., Vovk V., Levchenko M. Automation of aircraft control reconfiguration in flight special situations. In: Proceedings of IEEE 3rd International Conference on Methods and Systems of Navigation and Motion Control [Internet]; 2014 Oct 14-17; Kiev, Ukraine. [place unknown: publisher unknown]; 2014. p. 14-7. Available from: https://doi.org/10.1109/MSNMC.2014.6979759
- [9] Yang Z., Hua S., Hongzhuan Q., Chengrui L. Control reconfigurability of nonlinear system based on control redundancy. In: 10th IEEE International Conference on Industrial Informatics (INDIN) [Internet]; 2012 Jul 25-27; Beijing, China. Available from: https://doi.org/10.1109/INDIN.2012.6301366
- [10] Bannikov M., Terekhina A., Plekhov O. Experimental studies of the generation of heat in the top of the fatigue crack [Eksperimentalnoe issledovani osobennostey protsessa generatsii tepla v vershine ustalostnoy treschiny]. Vestnik PGTU Mekhanika. 2011;2:14-27.
- [11] Zugaj M., Narkiewicz J. Autopilot for reconfigurable flight control system. ASCE J Aerosp Eng. 2009 Jan;22:78-84.
- [12] Goraj Z. A specialized UAV for surveillance in windy, turbulent environment of the antarctic coast. Proc 29th Congr Int Counc Aeronaut Sci. 2014;I-VI:1-13.
- [13] Kuo B. Teorija i praktika cifrovyh sistem upravlenija [Theory and practice of digital control systems]. Moscow: Mashinostroenie; 1986. 448 p.
- [14] Zinovkin V. Rizkozminni navantazhennja ta i'h vplyv na elektrotehnichne obladnannja i metody doslidzhennja: navchal'nyj posibnyk. [Sharp load fluctuations and their impact on electrical equipment and research methods: textbook.]. Zaporizhzhja: ZNTU; 2017. 374 p.
- [15] Zinovkin V., Antonov M., Krysan I. Research of electromagnetic parameters of complex electromechanical system under hardly varying loads variable load. In: 2020 IEEE 7th International Conference on Energy Smart Systems (ESS) [Internet]; 2020 May 12-14; Kiev, Ukraine. p. 267-72. Available from: https://doi.org/10.1109/ESS50319.2020.9160022
- [16] Zinovkin V., Blyzniakov O. Research of the non-sinusoidal loads impact on the operability of tap-changers contacts. Electr Eng Power Eng [Internet]. 2020 Dec 24;2:17-23. Available from: https://doi.org/10.15588/1607-6761-2020-2-2
- [17] Dyakonov V. MATLAB 6/6.1/6.5+Simulink 4/5 v matematike i modelirovanii. Polnoe rukovodstvo pol'zovatelja [MATLAB 6/6.1/6.5 + Simulink 4/5 in Mathematics and Simulation. Complete user manual]. Moscow: SOLON - Press; 2003.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa nr POPUL/SP/0154/2024/02 w ramach programu "Społeczna odpowiedzialność nauki II" - moduł: Popularyzacja nauki (2025)
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-6f7630ea-c24a-4e1c-b985-f94dc5d93cf7
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