DocumentCode
487887
Title
Attitude Oscillation Damping for Space Station Freedom Alternative Assembly Configurations
Author
Wade, James W.
Author_Institution
Engineering and Science Program, Lockheed Engineering & Sciences Company, P.O.Box 58561, Houston, Texas 77258-8561
fYear
1989
fDate
21-23 June 1989
Firstpage
1573
Lastpage
1578
Abstract
Studies were conducted to investigate passive magnetic dampers as alternative stabilization methods for the United States Space Station Freedom. Achievement of a fully functioning vehicle with communication, control, and reboost capability after the first flight is constrained by the space shuttle size and lift capabilities. Magnetic dampers have been built by General Electric since the 1960´s and have been used with several gravity-gradient stable spacecraft Magnetic dampers require no power or communication ability to operate. When used on properly manifested spacecraft, magnetic dampers provide a lightweight, inexpensive, proven effective method of passively damping attitude oscillations. This paper contains some of the results of a study conducted by Lockheed Engineering and Sciences Company for NASA-JSC to determine the possibility of using magnetic dampers on alternative assembly configurations for Freedom. The work was performed under contract number NAS 9-17900.
Keywords
Aerospace engineering; Assembly; Communication system control; Damping; Shock absorbers; Size control; Space shuttles; Space stations; Space vehicles; State-space methods;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1989
Conference_Location
Pittsburgh, PA, USA
Type
conf
Filename
4790438
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