The proposed technology relates to a small satellite focus control apparatus and a focus control method using the same, and more specifically, utilizes a flexor hinge and a single motor. The small satellite focus control apparatus of the present invention comprises: a motor; a linear screw; an actuation body; and a reflector.

    제안기술은 소형 위성용 포커스 조절 장치 및 이를 이용한 포커스 조절 방법에 관한 것으로, 더욱 상세하게는 플렉서 힌지와 단일 모터를 이용한 소형 위성용 포커스 조절 장치 및 이를 이용한 포커스 조절 방법에 관한 발명이다.


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    Titel :

    Focus adjustment device for small satellite and focus adjustment method using the same


    Weitere Titelangaben:

    소형 위성용 포커스 조절 장치 및 이를 이용한 포커스 조절 방법


    Beteiligte:
    HWANG JAI HYUK (Autor:in) / KIM BYUNG KYU (Autor:in) / LEE DONG KYU (Autor:in) / JUNG JIN WON (Autor:in) / JOE SEONG GUN (Autor:in) / CHOI JUN WOO (Autor:in)

    Erscheinungsdatum :

    12.12.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    G02B Optische Elemente, Systeme oder Geräte , OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS / B64G Raumfahrt , COSMONAUTICS



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