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dc.contributor.authorZhang, Yuan
dc.contributor.authorZhang, Ran
dc.contributor.authorLi, Huifeng
dc.date.accessioned2026-08-20T21:14:46Z
dc.date.available2026-08-20T21:14:46Z
dc.date.copyright2025/10/06
dc.date.issued2026
dc.identifier.otherJAEEEZ.ASENG-6502.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314174
dc.description.abstractAbstractIn hypersonic vehicle entry guidance, trajectory prediction is widely used, and its accuracy directly affects the performance of the flight mission. To fast predict the trajectory, existing methods mainly focus on deriving analytical solutions of ...
dc.publisherAmerican Society of Civil Engineers
dc.titleHigh-Accuracy Entry Guidance with Analytical Trajectory Prediction for Large-Maneuver Gliding
dc.typeJournal Article
dc.journal.volume39
dc.journal.issue1
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6502
dc.journal.fristpage04025111-1
dc.journal.lastpage04025111-12
dc.page12
dc.treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 001
dc.contenttypeFulltext


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