The invention provides an on-orbit working method of a ground remote sensing microsatellite. The on-orbit working method comprises a locking wired mode and an unlocking wired mode between a platform cabin and a load cabin. The locking wired mode comprises a sun-facing locking mode, a ground-facing locking mode and a sun-facing safety mode; the unlocking wired mode comprises a sun-facing unlockingmode and a ground-facing unlocking mode. The efficiency of the ground remote sensing microsatellite platform can be fully exerted so as to meet the requirements of ground remote sensing microsatelliteobservation tasks.

    本发明提供了一种对地遥感微小卫星在轨工作方法,包括:平台舱与载荷舱间的锁紧有线与解锁有线模式。锁紧有线模式包括对日锁紧模式、对地锁紧模式、对日安全模式;解锁有线模式包括对日解锁模式、对地解锁模式。本发明可充分发挥对地遥感微小卫星平台的效能,以满足对地遥感微小卫星观测任务需求。


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    Titel :

    On-orbit working method of ground remote sensing microsatellite


    Weitere Titelangaben:

    一种对地遥感微小卫星在轨工作方法


    Beteiligte:
    HUANG QINGLONG (Autor:in) / XU JUN (Autor:in) / CHEN XIAO (Autor:in) / ZHANG WEI (Autor:in) / SHI WEIHUANG (Autor:in) / ZHANG XIAOKE (Autor:in) / ZHENG YONG'AI (Autor:in)

    Erscheinungsdatum :

    14.07.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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