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Gravity Measurement Method Of Solid Rocket Drive Based On Switched Reluctance Motor System

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dc.contributor.author Dongyi, Jia
dc.contributor.author Zhuo, Li
dc.contributor.author Farooq, Haq
dc.contributor.author Mohammed, Yousuf
dc.date.accessioned 2021-11-04T07:17:58Z
dc.date.available 2021-11-04T07:17:58Z
dc.date.copyright © 2021
dc.date.issued 2021
dc.identifier.citation Jia, D., Li, Z., Haqi, F., & Yousuf, M. (2021). Gravity measurement method of solid rocket drive based on switched reluctance motor system. Thermal Science, 26(6 Part A), 4011-4018. https://doi.org/10.2298/TSCI2106011J en_US
dc.identifier.issn 03549836
dc.identifier.uri https://doi.org/10.2298/TSCI2106011J
dc.identifier.uri http://hdl.handle.net/20.500.12519/460
dc.description This article is not available at CUD collection. The version of scholarly record of this article is published in Thermal Science (2021), available online at: https://doi.org/10.2298/TSCI2106011J en_US
dc.description.abstract Solid rocket drive system based on switched reluctance motor is established through the working principle of switched reluctance motor, and the closed-loop precise control of solid rocket drive system digitization is realized by the control method of pulse width modulation technology. The gravity value of solid rocket drive system is measured by the vertical deviation measurement method based on attitude error observation. The attitude datum of solid rocket drive system is ob-tained by the relationship between the vertical deviation and the attitude error of solid rocket drive system. The state space of solid rocket drive system is estab-lished by the attitude datum obtained. The horizontal gravity component estima-tion model of the real gravity value of the solid rocket drive system is established by the state space model, and the accurate gravity value of the solid rocket drive system is obtained by the estimation model. The simulation results show that the method can effectively measure the gravity value of solid rocket driving system, and the errors of measuring the gravity of solid rocket driving system are less than 1%. © 2021. Society of Thermal Engineers of Serbia en_US
dc.language.iso en en_US
dc.publisher Serbian Society of Heat Transfer Engineers en_US
dc.relation Authors Affiliations : Jia, D., Department of Mechanical and Electrical Engineering, Hetao College, Bayannur, China, College of Science, Inner Mongolia University of Technology, Hohhot, China; Li, Z., College of Science, Inner Mongolia University of Technology, Hohhot, China; Haqi, F., Department of Marketing, Canadian University of Dubai, Dubai, United Arab Emirates; Yousuf, M., Department of Bussines Administration, Applied Science University, Al Eker, Bahrain
dc.relation.ispartofseries Thermal Science;Volume 26, Issue 6 Part A
dc.rights Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) License
dc.rights.uri https://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject driving coefficient en_US
dc.subject gravity value en_US
dc.subject rocket engine en_US
dc.subject switched reluctance motor system en_US
dc.title Gravity Measurement Method Of Solid Rocket Drive Based On Switched Reluctance Motor System en_US
dc.type Article en_US
dc.rights.holder Copyright : © 2021. Society of Thermal Engineers of Serbia


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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) License Except where otherwise noted, this item's license is described as Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) License

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