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 :
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