DocumentCode
1126599
Title
A Note on Satellite Dynamics
Author
Guibord, A.F. ; Ahmed, N.U.
Author_Institution
Ottawa University, Ottawa, Ont., Canada
Issue
6
fYear
1976
Firstpage
819
Lastpage
822
Abstract
It is demonstrated here that inertial differentiation of angular momentum-is independent of the choice of the moving reference coordinate system. The results agree with Greensite [1] and contradict Sen´s results [2] by indicating a basic error in his derivation. However, Sen´s step [2] is correct.
Keywords
Argon; Circuit theory; Councils; Flywheels; Markov processes; Satellites;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1976.308364
Filename
4101745
Link To Document