The present invention relates to an output pulse control system for a valve for satellite posture control and a control method thereof, and more specifically, to a system, which can control a valve in terms of fault management for a satellite posture and track operation stability when input of a time mark for control of an output pulse of a valve for satellite posture control is stopped or dissipated, and a control method thereof.

    본 발명은 인공위성 자세제어용 밸브의 출력 펄스 제어 시스템 및 그 제어 방법에 관한 것으로서, 더욱 상세하게는, 인공위성 자세제어용 밸브의 출력 펄스의 제어를 위한 동기 신호(Time Mark)의 입력이 중단되거나 소실되는 경우, 위성 자세 및 궤도 운영 안정성을 위한 Fault management 측면에서 밸브를 제어할 수 있는 시스템 및 그 제어 방법에 관한 것이다.


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    Titel :

    Output fire pulse control system and method of satellite attitude controlling valve


    Weitere Titelangaben:

    인공위성 자세제어용 밸브의 출력 펄스 제어 시스템 및 그 제어 방법


    Beteiligte:
    KIM KYU DONG (Autor:in) / PARK SUNG WOO (Autor:in) / PARK HEE SUNG (Autor:in) / PARK JEONG EON (Autor:in) / YANG JEONG HWAN (Autor:in)

    Erscheinungsdatum :

    2020-01-06


    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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