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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    Title :

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


    Additional title:

    소형 위성용 포커스 조절 장치 및 이를 이용한 포커스 조절 방법


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

    Publication date :

    2019-12-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

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



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