Dynamic analysis of flexible space shuttle remote manipulator system with large payloads

Wiedemann, Simon M.; Kirk, Colin L.

dc.contributor.author	Wiedemann, Simon M.	en_UK
dc.contributor.author	Kirk, Colin L.	en_UK
dc.date.accessioned	2005-11-22T13:33:57Z
dc.date.available	2005-11-22T13:33:57Z
dc.date.issued	2005-06-27T15:48:00Z	en_UK
dc.identifier.uri	http://hdl.handle.net/1826/878
dc.description	Paper given at Dynamics and Control of Systems and Structures in Space (DCSSS), 5th conference, Kings College, Cambridge, July 2002	en_UK
dc.description.abstract	This paper presents a new approach for determination of vibration response of the triply articulated Space Shuttle Remote Manipulator System (SRMS) with large rigid overhanging payloads. In contrast to other researchers dynamic modelling is based on the exact eigenvalue analysis of the two main flexible links with a rigid end effector and payload, including the effect of interaction of the Shuttle. A wide range of SRMS configurations and payloads with joints free and locked is examined for bang-bang slews and with all joints locked for payload positioning using Shuttle thruster firing.	en_UK
dc.format.extent	1944 bytes
dc.format.extent	229027 bytes
dc.format.mimetype	text/plain
dc.format.mimetype	application/pdf
dc.language.iso	en_UK
dc.publisher	Cranfield University; School of Engineering	en_UK
dc.title	Dynamic analysis of flexible space shuttle remote manipulator system with large payloads	en_UK
dc.type	Presentation	en_UK