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.


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    Title :

    A note on satellite dynamics


    Additional title:

    Eine Notiz ueber Satelliten-Dynamiken


    Contributors:
    Guibord, A.F. (author) / Ahmed, N.U. (author)

    Published in:

    Publication date :

    1976


    Size :

    4 Seiten, 2 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    A Note on Satellite Dynamics

    Guibord, A. F. / Ahmed, N. U. | IEEE | 1976


    Comments on 'A note on satellite dynamics'

    Sen, A.K. | Tema Archive | 1977



    Authors' reply to "Comments on' a Note on Satellite Dynamics'"

    Guibord, A. F. / Ahmed, N. U. | IEEE | 1977