PROBLEM TO BE SOLVED: To provide an energy efficient satellite maneuvering method.SOLUTION: The method includes maneuvering a satellite that is in an orbit around a planet 208, so that a principle sensitive axis 408 of the satellite is oriented to an orbit frame plane 404 to reduce gravity gradient torques acting upon the satellite. The orbit frame plane is based on an orbit frame vector 402.SELECTED DRAWING: Figure 4

    【課題】エネルギー効率に優れた衛星の操縦方法を提供する。【解決手段】惑星208の周りの軌道にある衛星を操縦し、それによって、衛星の主要な受感軸408が軌道フレーム平面404に方向付けられ、衛星に働く重力勾配トルクを低減させることを含む。軌道フレーム平面は、軌道フレームベクトル402に基づく。【選択図】図4


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    Title :

    ENERGY EFFICIENT SATELLITE MANEUVERING


    Additional title:

    エネルギー効率に優れた衛星の操縦


    Contributors:
    TIMOTHY S LUI (author) / LEE KANGSIK (author)

    Publication date :

    2017-08-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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