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Space station attitude disturbance arising from internal motionsA source of space station attitude disturbances is identified. The attitude disturbance is driven by internal space station motions and is a direct result of conservation of angular momentum. Three examples are used to illustrate the effect: a planar three link system, a rigid carrier body with two moveable masses, and a nonplanar five link system. Simulation results are given to show the magnitude of the attitude change in each example. Factors which accentuate or attenuate this disturbance effect are discussed.
Document ID
19930020806
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcnally, Patrick J. (Michigan Univ. Ann Arbor, MI, United States)
Mcclamroch, N. Harris (Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
September 6, 2013
Publication Date
June 3, 1993
Publication Information
Publication: Efficient Reorientation Maneuvers for Spacecraft with Multiple Articulated Payloads
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: American Control Conference
Location: Ann Arbor, MI
Country: United States
Start Date: January 1, 1993
Accession Number
93N29995
Funding Number(s)
CONTRACT_GRANT: NSF MSS-91-14630
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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