A precision trajectory program has been developed to serve as a test bed for geocentric orbit raising steering laws. The steering laws to be evaluated have been developed using optimization methods employing averaging techniques. This program provides the capability of testing the steering laws in a precision simulation. The principal system models incorporated in the program are described, including the radiation environment, the solar array model, the thrusters and power processors, the geopotential, and the solar system. Steering and array orientation constraints are discussed, and the impact of these constraints on program design is considered.


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    Titel :

    Precision orbit raising trajectories


    Beteiligte:
    Flanagan, P. F. (Autor:in) / Horsewood, J. L. (Autor:in) / Pines, S. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Electric Propulsion Conference ; 1975 ; New Orleans, LA


    Erscheinungsdatum :

    01.03.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Precision orbit raising trajectories

    FLANAGAN, P. / HORSEWOOD, J. / PINES, S. | AIAA | 1975





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