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dc.contributor.authorTantravahi, Santosh
dc.date.accessioned2026-02-17T21:34:57Z
dc.date.available2026-02-17T21:34:57Z
dc.date.copyright5/27/2025 12:00:00 AM
dc.date.issued2025
dc.identifier.issn2689-6117
dc.identifier.otheraldsc-24-1065.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4310310
dc.description.abstractThere has been an increasing attention toward the research of space manipulator systems for different applications like on-orbit servicing, debris removal, etc. from various institutions across the globe. This resulted in the trend of investigating simple methods to couple various manipulator and base/spacecraft pose control methodologies that already exist independently in the literature. One such scientific work in this direction proposed a control strategy for purely manipulator end-effector trajectory tracking control, while the base/spacecraft is station-kept. This article investigates the generalizability of the control strategy proposed by the scientific work for various space manipulation applications.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleOn the Simulations Concerning the Dynamics and Control of Space Manipulator Systems
dc.typeJournal Paper
dc.journal.volume5
dc.journal.issue3
dc.journal.titleASME Letters in Dynamic Systems and Control
dc.identifier.doi10.1115/1.4068538
dc.journal.fristpage31002-1
dc.journal.lastpage31002-13
dc.page13
dc.treeASME Letters in Dynamic Systems and Control:;2025:;volume( 005 ):;issue: 003
dc.contenttypeFulltext


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