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dc.contributor.authorZheng, Bochen
dc.contributor.authorZhang, Hehong
dc.contributor.authorWang, Xin
dc.contributor.authorZhai, Chao
dc.contributor.authorLin, Hongyu
dc.contributor.authorLi, Xin
dc.date.accessioned2026-08-20T21:15:31Z
dc.date.available2026-08-20T21:15:31Z
dc.date.copyright2026/02/24
dc.date.issued2026
dc.identifier.otherJAEEEZ.ASENG-6702.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314192
dc.description.abstractAbstractThe intake system of high-altitude simulation chambers is characterized by strong nonlinearities, high coupling effects, and significant external disturbances, posing substantial challenges for achieving precise temperature and pressure ...Practical ApplicationsHigh-altitude simulation chambers are essential ground-based facilities designed to replicate the pressure and temperature conditions experienced by aircraft engines during high-altitude flight. However, their control systems often ...
dc.publisherAmerican Society of Civil Engineers
dc.titleESO-MPC and Differential Flatness-Based Multivariable Control of High-Altitude Chamber Intake Systems
dc.typeJournal Article
dc.journal.volume39
dc.journal.issue3
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6702
dc.journal.fristpage04026010-1
dc.journal.lastpage04026010-15
dc.page15
dc.treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 003
dc.contenttypeFulltext


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