Satellite, with inertia properties within specific range of values, is assumed to be in orbit of small eccentricity; cold-gas jets that are bounded in thrust level supply torques for attitude control; performance criterion in minimum-fuel consumption for reaching desired attitude in given time; Pontryagin's maximum principle is employed to determine characteristics of minimum-fuel, optimal control for linearized motion, and suboptimal, feedback, attitude-control system is developed that is simple and efficient.


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    Titel :

    Attitude control of satellite in elliptic orbit


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Busch, R.E. (Autor:in) / Fluegge-Lotz, I. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :