Guidance equations for orbital operations; development of mathematical formulations of maneuver in orbit problem and solutions that can be utilized in analysis of space missions and associated guidance process; factors affecting vehicle motion are isolated and optimum sequence of events required to produce desired motion is defined.


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    Titel :

    Guidance, flight mechanics and trajectory optimization -- 11


    Weitere Titelangaben:

    NASA CR


    Beteiligte:
    Townsend, G.E. (Autor:in) / Grier, D.R. (Autor:in) / Blackford, A.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    117 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Guidance, flight mechanics and trajectory optimization -- 5

    Townsend, G.E. / Grier, D.R. / Palmer, R.R. et al. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 16

    Robertson, R.L. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 17

    Grier, D.R. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 3

    Townsend, G.E. / Tamburro, M.B. | Engineering Index Backfile | 1968


    Guidance, flight mechanics and trajectory optimization -- 15

    Abbott, A.S. / Blackford, A.L. | Engineering Index Backfile | 1968