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

dc.contributor.authorDongyi, Jia
dc.contributor.authorZhuo, Li
dc.contributor.authorFarooq, Haq
dc.contributor.authorMohammed, Yousuf
dc.date.accessioned2021-11-04T07:17:58Z
dc.date.available2021-11-04T07:17:58Z
dc.date.copyright© 2021
dc.date.issued2021
dc.descriptionThis 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/TSCI2106011Jen_US
dc.description.abstractSolid 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 Serbiaen_US
dc.identifier.citationJia, 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/TSCI2106011Jen_US
dc.identifier.issn03549836
dc.identifier.urihttps://doi.org/10.2298/TSCI2106011J
dc.identifier.urihttp://hdl.handle.net/20.500.12519/460
dc.language.isoenen_US
dc.publisherSerbian Society of Heat Transfer Engineersen_US
dc.relationAuthors 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.ispartofseriesThermal Science;Volume 26, Issue 6 Part A
dc.rightsCreative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) License
dc.rights.holderCopyright : © 2021. Society of Thermal Engineers of Serbia
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subjectdriving coefficienten_US
dc.subjectgravity valueen_US
dc.subjectrocket engineen_US
dc.subjectswitched reluctance motor systemen_US
dc.titleGravity Measurement Method Of Solid Rocket Drive Based On Switched Reluctance Motor Systemen_US
dc.typeArticleen_US
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