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dc.contributor.authorLi, Dongjin
dc.contributor.authorLi, Huayang
dc.contributor.authorQi, Chenkun
dc.contributor.authorHu, Yan
dc.contributor.authorGao, Feng
dc.contributor.authorZhao, Xianchao
dc.date.accessioned2026-08-20T21:15:33Z
dc.date.available2026-08-20T21:15:33Z
dc.date.copyright2026/02/25
dc.date.issued2026
dc.identifier.otherJAEEEZ.ASENG-6727.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314193
dc.description.abstractAbstractA space contact hardware-in-the-loop (HIL) simulator is a key facility for ground testing of space contact processes. It must faithfully reproduce the dynamics in space. Force delay is known to induce instability. To suppress velocity drift from ...
dc.publisherAmerican Society of Civil Engineers
dc.titleDistortion Analysis and Compensation for a Space Contact HIL Simulator with Force Delay and Dead Zone
dc.typeJournal Article
dc.journal.volume39
dc.journal.issue3
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-6727
dc.journal.fristpage04026012-1
dc.journal.lastpage04026012-11
dc.page11
dc.treeJournal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 003
dc.contenttypeFulltext


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