Abstract
A control system of permanent magnet synchronous motor ensuring its fail-safety at the expense of switchover between several scalar control modes, is proposed. A computer simulation model is realized. The operation of such a system is analyzed in terms of the electric pump unit of space application.
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ACKNOWLEDGEMENTS
The research was carried out in the framework of the project “Creation of high-tech import-substituting production of damage tolerant elements of executive automation systems transport and aerospace engineering, ensuring the development and use of the World Ocean, Arctic, and Antarctic” with the financial support of the Ministry of Science and Higher Education of the Russian Federation (Agreement no. 075-11-2019-077 of 13.12.2019) following the decree of the RF Government of 09.04.2010 No. 218.
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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 2, pp. 37 - 44.
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Matveev, S.A., Testoedov, N.A., Slobodzyan, N.S. et al. Fail-Safe Control System for an Electric Pump Unit of Space Application. Russ. Aeronaut. 64, 210–218 (2021). https://doi.org/10.3103/S1068799821020069
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DOI: https://doi.org/10.3103/S1068799821020069