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Six-degree-of-freedom simulation of an astronaut detumble systemThe problem of stabilizing the attitude of an untethered astronaut in a three-axis tumble is addressed. A simple six thruster detumbling system mounted on the astronaut's Portable Life Support System backpack is analyzed as a possible solution. A six-degree-of-freedom dynamical model is constructed using the Clohessy-Wiltshire equations, Euler's moment equations, and quaternions. The six thruster system produces both moments and forces when activated. However, it is shown that the thrust forces acting on the body during detumbling do not significantly affect the translational motion.
Document ID
19910049047
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Fowler, W. T.
(Texas, University Austin, United States)
Neff, J. M.
(Texas Univ. Austin, TX, United States)
Date Acquired
August 14, 2013
Publication Date
March 1, 1991
Publication Information
Publication: Journal of the Astronautical Sciences
Volume: 39
ISSN: 0021-9142
Subject Category
Man/System Technology And Life Support
Accession Number
91A33670
Funding Number(s)
CONTRACT_GRANT: NGT-50222
Distribution Limits
Public
Copyright
Other

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