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Backstepping Sliding Mode Control of Quadrotor UAV Trajectory

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dc.contributor.authorMulualem, Yohannes Lisanewerk-
dc.contributor.authorJin, Gang Gyoo-
dc.contributor.authorKwon, Jaesung-
dc.contributor.authorAhn, Jongkap-
dc.date.accessioned2025-11-05T03:00:06Z-
dc.date.available2025-11-05T03:00:06Z-
dc.date.issued2025-10-
dc.identifier.issn2227-7390-
dc.identifier.issn2227-7390-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/80641-
dc.description.abstractUnmanned Aerial Vehicles (UAVs), commonly known as drones, have become widely used in many fields, ranging from agriculture to military operations, due to recent advances in technology and decreases in costs. Quadrotors are particularly important UAVs, but their complex, coupled dynamics and sensitivity to outside disturbances make them challenging to control. This paper introduces a new control method for quadrotors called Backstepping Sliding Mode Control (BSMC), which combines the strengths of two established techniques: Backstepping Control (BC) and Sliding Mode Control (SMC). Its primary goal is to improve trajectory tracking while also reducing chattering, a common problem with SMC that causes rapid, high-frequency oscillations. The BSMC method achieves this by integrating the SMC switching gain directly into the BC through a process of differential iteration. Herein, a Lyapunov stability analysis confirms the system's asymptotic stability; a genetic algorithm is used to optimize controller parameters; and the proposed control strategy is evaluated under diverse payload conditions and dynamic wind disturbances. The simulation results demonstrated its capability to handle payload variations ranging from 0.5 kg to 18 kg in normal environments, and up to 12 kg during gusty wind scenarios. Furthermore, the BSMC effectively minimized chattering and achieved a superior performance in tracking accuracy and robustness compared to the traditional SMC and BC.-
dc.language영어-
dc.language.isoENG-
dc.publisherMDPI AG-
dc.titleBackstepping Sliding Mode Control of Quadrotor UAV Trajectory-
dc.typeArticle-
dc.publisher.location스위스-
dc.identifier.doi10.3390/math13193205-
dc.identifier.scopusid2-s2.0-105018948558-
dc.identifier.wosid001593734800001-
dc.identifier.bibliographicCitationMathematics, v.13, no.19-
dc.citation.titleMathematics-
dc.citation.volume13-
dc.citation.number19-
dc.type.docTypeArticle-
dc.description.isOpenAccessY-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.relation.journalResearchAreaMathematics-
dc.relation.journalWebOfScienceCategoryMathematics-
dc.subject.keywordAuthorquadrotor-
dc.subject.keywordAuthorbackstepping control-
dc.subject.keywordAuthorsliding mode control-
dc.subject.keywordAuthorbackstepping sliding mode control-
dc.subject.keywordAuthorLyapunov stability-
dc.subject.keywordAuthorgenetic algorithm-
dc.subject.keywordAuthor93-10-
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해양과학대학 (기계시스템공학과)
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