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 (see Analysis and Design of Space Vehicle Flight Control Systems. New York; Spactan Books, 1970, p.385-94) and contradict Sen's results (see ibid., vol.12, no.5, p.290-91 (1976)) by indicating a basic error in his derivation. However, Sen's step 1 is correct.
A note on satellite dynamics
Eine Notiz ueber Satelliten-Dynamiken
IEEE Transactions on Aerospace and Electronic Systems ; AES-12 , 6. ; 819-822
1976
4 Seiten, 2 Quellen
Aufsatz (Zeitschrift)
Englisch
IEEE | 1976
|Comments on 'A note on satellite dynamics'
Tema Archiv | 1977
|Comments on "A Note on Satellite Dynamics"
IEEE | 1977
|TECHNICAL NOTE - Dynamics and Orbit Determination of Tethered Satellite Systems
Online Contents | 1998
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