Number of approaches were applied to final satellite decay problem, but only few theories were developed for case of predicting ahead fraction or few revolutions; latter problem is attacked for orbits of small eccentricity taking into account not only reference density but also scale height; by linearization of dynamical equations analytical expressions are developed for perturbation due to drag; being in closed form, expressions can be used in various ways to study influence of small eccentricity and drag on other quantities.


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    Titel :

    Linearized drag analysis and orbit determination


    Weitere Titelangaben:

    Progress Astronautics Aeronautics -- Celestial Mechanics Astrodynamics


    Beteiligte:
    Forster, K. (Autor:in) / Baker, Jr., R.M.L. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    ORBIT DETERMINATION BY LINEARIZED DRAG ANALYSIS

    FORSTER, KURT / BAKER, ROBERT / KURT, FORSTER | AIAA | 1963


    Linearized Drag Analysis and Orbit Determination

    Szebehely, Victor G. | AIAA | 1964


    Drag Coefficient Estimation in Orbit Determination

    McLaughlin, Craig A. | Online Contents | 2011


    Drag Coefficient Estimation in Orbit Determination

    McLaughlin, Craig A | Online Contents | 2011


    Drag Coefficient Estimation in Orbit Determination

    McLaughlin, Craig A. / Mance, Steve / Lichtenberg, Travis | Springer Verlag | 2011