Multivariable Disturbance Observer-Based Finite-Time Sliding Mode Attitude Control for Fixed-Wing UAVs under Matched and Mismatched Disturbances
DC Field | Value | Language |
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dc.contributor.author | Nguyen, Ngo Phong | - |
dc.contributor.author | Oh, Hyondong | - |
dc.contributor.author | Moon, Jun | - |
dc.contributor.author | Kim, Yoonsoo | - |
dc.date.accessioned | 2023-11-24T05:18:18Z | - |
dc.date.available | 2023-11-24T05:18:18Z | - |
dc.date.issued | 2023-06 | - |
dc.identifier.issn | 2475-1456 | - |
dc.identifier.issn | 2475-1456 | - |
dc.identifier.uri | https://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/193094 | - |
dc.description.abstract | In this letter, we propose a multivariable disturbance observer-based finite-time sliding mode attitude control (MDOB-FT-SM-AC) for fixed-wing UAVs in the presence of both matched and mismatched disturbances. Compared with existing sliding mode attitude controllers, the significant improvements of the proposed MDOB-FT-SM-AC are the multivariable control structure, strong robustness, and high precision performance with continuous control input signal. In the proposed MDOB-FT-SM-AC, we first develop multivariable finite-time disturbance observers such that the precise estimation of both matched and mismatched disturbances is ensured. Next, a nonsingular terminal sliding manifold is designed such that the fixed-wing UAV is driven to track its desired attitude command in finite time. We finally present a multivariable super-twisting reaching law such that the finite-time convergence of the sliding variable and its derivative to zero is guaranteed. Attentive finite-time convergence analysis is derived based on the Lyapunov and homogeneity theories. Simulation results are given to illustrate the superiority of the proposed MDOB-FT-SM-AC. | - |
dc.format.extent | 6 | - |
dc.language | 영어 | - |
dc.language.iso | ENG | - |
dc.publisher | Institute of Electrical and Electronics Engineers Inc. | - |
dc.title | Multivariable Disturbance Observer-Based Finite-Time Sliding Mode Attitude Control for Fixed-Wing UAVs under Matched and Mismatched Disturbances | - |
dc.type | Article | - |
dc.publisher.location | 미국 | - |
dc.identifier.doi | 10.1109/LCSYS.2023.3283390 | - |
dc.identifier.scopusid | 2-s2.0-85161615246 | - |
dc.identifier.wosid | 001017367300014 | - |
dc.identifier.bibliographicCitation | IEEE Control Systems Letters, v.7, pp 1999 - 2004 | - |
dc.citation.title | IEEE Control Systems Letters | - |
dc.citation.volume | 7 | - |
dc.citation.startPage | 1999 | - |
dc.citation.endPage | 2004 | - |
dc.type.docType | Article | - |
dc.description.isOpenAccess | N | - |
dc.description.journalRegisteredClass | scopus | - |
dc.description.journalRegisteredClass | esci | - |
dc.relation.journalResearchArea | Automation & Control Systems | - |
dc.relation.journalWebOfScienceCategory | Automation & Control Systems | - |
dc.subject.keywordPlus | Aircraft control | - |
dc.subject.keywordPlus | Antennas | - |
dc.subject.keywordPlus | Fixed wings | - |
dc.subject.keywordPlus | Flight control systems | - |
dc.subject.keywordPlus | Perturbation techniques | - |
dc.subject.keywordPlus | Riccati equations | - |
dc.subject.keywordPlus | Unmanned aerial vehicles (UAV) | - |
dc.subject.keywordAuthor | Flight control | - |
dc.subject.keywordAuthor | uncertain systems | - |
dc.subject.keywordAuthor | variable-structure/sliding-mode control | - |
dc.identifier.url | https://ieeexplore.ieee.org/document/10144581 | - |
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