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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    Title :

    Guidance, flight mechanics and trajectory optimization -- 11


    Additional title:

    NASA CR


    Contributors:

    Published in:

    Publication date :

    1968


    Size :

    117 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Guidance, flight mechanics and trajectory optimization -- 16

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


    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 -- 6

    Allione, M.S. / Blackford, A.L. / Mendez, J.C. et al. | 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