Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/118404
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dc.contributorDepartment of Aeronautical and Aviation Engineering-
dc.creatorYang, R-
dc.creatorWen, W-
dc.creatorYang, P-
dc.creatorZhao, Z-
dc.creatorHuang, F-
dc.date.accessioned2026-04-14T03:09:40Z-
dc.date.available2026-04-14T03:09:40Z-
dc.identifier.issn0018-9251-
dc.identifier.urihttp://hdl.handle.net/10397/118404-
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineersen_US
dc.rights© 2025 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.en_US
dc.rightsThe following publication R. Yang, W. Wen, P. Yang, Z. Zhao and F. Huang, 'Unified Sufficient Conditions for Exact Convex Relaxation of Nonconvex Optimal Control Problems,' in IEEE Transactions on Aerospace and Electronic Systems, vol. 61, no. 6, pp. 17924-17937, Dec. 2025 is available at https://doi.org/10.1109/TAES.2025.3607718.en_US
dc.subjectConvex optimizationen_US
dc.subjectConvex relaxationen_US
dc.subjectMars landingen_US
dc.subjectOptimal controlen_US
dc.titleUnified sufficient conditions for exact convex relaxation of nonconvex optimal control problemsen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage17924-
dc.identifier.epage17937-
dc.identifier.volume61-
dc.identifier.issue6-
dc.identifier.doi10.1109/TAES.2025.3607718-
dcterms.abstractThis article focuses on achieving exact convex relaxation of optimal control problems characterized by nonconvex control constraints and convex state constraints. By employing the convex hull of the original nonconvex control constraint set, the constraints are relaxed, thereby transforming the original problem into a convex problem. The article introduces two unified sufficient conditions to ensure the relaxation’s exactness, guaranteeing that the solution derived from the relaxed problem remains globally optimal for the original nonconvex problem. Although one of the proposed sufficient conditions is abstract and nontrivial, we prove that it can be transformed into standard controllability, normality, and strong observability conditions proposed by the previous work about exact convex relaxation, if the control and state constraint sets have certain properties. Furthermore, approximation methods are developed to modify the cost function, control constraints, and system dynamics to ensure that the sufficient conditions are satisfied in certain scenarios. The results of this article are applied to Mars landing problems, demonstrating that under glide-slope constraints, the exact convex can be realized.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationIEEE transactions on aerospace and electronic systems, Dec. 2025, v. 61, no. 6, p. 17924-17937-
dcterms.isPartOfIEEE transactions on aerospace and electronic systems-
dcterms.issued2025-12-
dc.identifier.scopus2-s2.0-105016235044-
dc.identifier.eissn1557-9603-
dc.description.validate202604 bcjz-
dc.description.oaAccepted Manuscripten_US
dc.identifier.SubFormIDG001445/2026-03en_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextThis work was supported by the Research Center of Deep Space Exploration (RCDSE), The Hong Kong Polytechnic University, under project “Multi-robot Collaborative Operations in Lunar Areas for Regolith Processing (BBDW).”en_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryGreen (AAM)en_US
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