The present invention provides a control apparatus for sensing a change in a yaw angle of a moving satellite and calculating a ground sample distance in accordance with the yaw angle. The apparatus for controlling a moving satellite comprises: a sensing unit sensing the yaw angle corresponding to yaw steering of the moving satellite; and a processor calculating the ground sample distance where the length of a pixel captured by the moving satellite is projected on the ground surface in accordance with the yaw angle.

    이동 위성체의 요우 각 변화를 센싱하고, 요우 각에 따른 그라운드 샘플 거리를 계산하는 제어 장치가 제공된다. 상기 이동 위성체의 제어 장치는 상기 이동 위성체의 요우 스티어링에 상응하는 요우 각을 센싱하는 센싱부 및 상기 이동 위성체에 의해 촬영된 픽셀의 길이가 상기 요우 각에 따라 지표면에 사영된 그라운드 샘플 거리를 계산하는 프로세서를 포함할 수 있다.


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    Titel :

    APPARATUS AND METHOD FOR CONTROLLING A SATELLITE


    Weitere Titelangaben:

    위성체 제어 장치 및 그 방법


    Beteiligte:
    JEON MOON JIN (Autor:in) / LEE SANG ROK (Autor:in) / KIM HUI KYUNG (Autor:in) / KIM EUNG HYUN (Autor:in) / LIM SEONG BIN (Autor:in) / CHOI SEOK WEON (Autor:in)

    Erscheinungsdatum :

    20.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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