The results are reported of work on an appropriate approach to the solution of the optimum two-impulse transfer problem between orbits of specified inclination. The task included a literature search to identify the current state of the art and a definition of the suggested approach for the specific application of a lunar orbit trim. The applications of the results to the problem are included. The formulation for a computer program developed under this task following a more conventional approach is also included.


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    Title :

    Two impulse trajectory optimization for the RAE-B orbit trim problem


    Contributors:
    Payne, M. H. (author) / Pines, S. (author) / Horsewood, J. L. (author)

    Publication date :

    1972-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


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