Rendezvous and Docking Control of Satellites Using Chaos Synchronization Method With Intuitionistic Fuzzy Sliding Mode Control

dc.authorscopusid 57210598822
dc.authorscopusid 57210605351
dc.authorscopusid 37030525400
dc.authorscopusid 7007101709
dc.contributor.author Silahtar, O.
dc.contributor.author Kutlu, F.
dc.contributor.author Atan, Ö.
dc.contributor.author Castillo, O.
dc.date.accessioned 2025-05-10T16:54:38Z
dc.date.available 2025-05-10T16:54:38Z
dc.date.issued 2023
dc.department T.C. Van Yüzüncü Yıl Üniversitesi en_US
dc.department-temp Silahtar O., Department of Electrical and Electronics Engineering, Faculty of Engineering, Van Yuzuncu Yil University, Van, 65080, Turkey; Kutlu F., Department of Mathematics, Faculty of Science, Van Yuzuncu Yil University, Van, 65080, Turkey; Atan Ö., Department of Electrical and Electronics Engineering, Faculty of Engineering, Van Yuzuncu Yil University, Van, 65080, Turkey; Castillo O., Division of Graduate Studies, Tijuana Institute of Technology, TecNM, Tijuana, Mexico en_US
dc.description.abstract In this study, two different controllers have been designed to perform the rendezvous and docking tasks of two nonidentical and noncooperative cubic satellites. Firstly, the motion of cubic satellites was modeled with chaotic equations. After selecting suitable chaotic models, fuzzy sliding mode controller (FSMC) and a new intuitionistic fuzzy sliding mode controller (IFSMC), which are applied to synchronization systems under the same initial conditions, have been designed. It has been observed that both synchronizations reach stability by applying the controllers designed by considering the Lyapunov stability criteria. After a while, a short-term and random disturbance was applied to the synchronization systems and the response of both controllers was observed. The numerical results showed that the synchronization system with both controllers was stable, robust, efficient, fast and chattering-free. However, synchronization system with IFSMC was found to be more robust, faster and more efficient than synchronization system with FSMC. © 2023, The Author(s), under exclusive license to Springer Nature Switzerland AG. en_US
dc.identifier.doi 10.1007/978-3-031-22042-5_10
dc.identifier.endpage 197 en_US
dc.identifier.issn 1860-949X
dc.identifier.scopus 2-s2.0-85152285836
dc.identifier.scopusquality Q3
dc.identifier.startpage 177 en_US
dc.identifier.uri https://doi.org/10.1007/978-3-031-22042-5_10
dc.identifier.uri https://hdl.handle.net/20.500.14720/3202
dc.identifier.volume 1061 en_US
dc.identifier.wosquality N/A
dc.language.iso en en_US
dc.publisher Springer Science and Business Media Deutschland GmbH en_US
dc.relation.ispartof Studies in Computational Intelligence en_US
dc.relation.publicationcategory Kitap Bölümü - Uluslararası en_US
dc.rights info:eu-repo/semantics/closedAccess en_US
dc.subject Chaos Synchronization en_US
dc.subject Fuzzy Sliding Mode Control en_US
dc.subject Intuitionistic Fuzzy Sliding Mode Control en_US
dc.subject Rendezvous And Docking Control en_US
dc.title Rendezvous and Docking Control of Satellites Using Chaos Synchronization Method With Intuitionistic Fuzzy Sliding Mode Control en_US
dc.type Book Part en_US
dspace.entity.type Publication
gdc.coar.access metadata only access
gdc.coar.type text::book::book part

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