Fuel optimal control conditions in attitude correction of satellite in circular orbit determined using maximum principle, solving resulting boundary value problem


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    Title :

    Attitude Control of a Satellite in Circular Orbit


    Contributors:
    Athans, M. (author) / Gray, D. L. (author)

    Publication date :

    1967-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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