DocumentCode
888569
Title
Use of Malkin´s theorem for satellite stability in the presence of light pressure
Author
Anand, D.
Volume
55
Issue
3
fYear
1967
fDate
3/1/1967 12:00:00 AM
Firstpage
444
Lastpage
445
Abstract
Stability of satellites subjected to persistent perturbations is examined using Malkin´s theorem. Expressions are presented for distrubing torqnes about all three spacecraft axes due to light pressure. Malkin´s theorem is shown to be a valuable design tool for satellite attitude control.
Keywords
Capacitance measurement; Cutoff frequency; Diodes; Frequency measurement; Impedance matching; Joining processes; Satellites; Silicon; Stability; Varactors;
fLanguage
English
Journal_Title
Proceedings of the IEEE
Publisher
ieee
ISSN
0018-9219
Type
jour
DOI
10.1109/PROC.1967.5531
Filename
1447461
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