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dc.contributor.authorCai, Guangbin
dc.contributor.authorZheng, Hui
dc.contributor.authorWang, Yongchao
dc.contributor.authorZhang, Shiyuan
dc.date.accessioned2026-08-20T21:12:38Z
dc.date.available2026-08-20T21:12:38Z
dc.date.copyright2025/12/09
dc.date.issued2026
dc.identifier.otherJAEEEZ.ASENG-6043.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314121
dc.description.abstractAbstractIn this article, an incremental model predictive attitude control for morphing aircraft with variable wingspans and sweepback angles is proposed. This method does not require a concrete mathematical model of the system, thus reducing the ...
dc.publisherAmerican Society of Civil Engineers
dc.titleIncremental Model Predictive Attitude Control for Morphing Aircraft: A Weak Model-Dependent Control Method
dc.typeJournal Article
dc.journal.volume39
dc.journal.issue2
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6043
dc.journal.fristpage04025137-1
dc.journal.lastpage04025137-19
dc.page19
dc.treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002
dc.contenttypeFulltext


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