The invention discloses a space station large-scale flexible solar wing unfolding and folding and sun orientation comprehensive type driving control device, and aims at the unfolding and folding and sun orientation driving functions of a space station large-scale flexible solar wing. Driving circuits of a lifting mechanism, a box body unfolding and folding mechanism, a restraining and releasing mechanism, a stretching mechanism and a sun orientation driving mechanism which are used for achieving multi-step unfolding of the large flexible solar wing are integrated in the same comprehensive driving control device, and the high-integration-level design of aerospace products is achieved. The flexible working mode that the large flexible solar wing of the space station is fully automatically unfolded according to a program or independently unfolded and folded in a time-sharing and single-step mode is achieved; according to the technical scheme, high-reliability multi-type instruction interface design including 1553B bus communication and redundant OC hard wire instructions is achieved, under the high-priority OC hard wire instruction execution working condition, a drive control task can be completed in a minimum function circuit in a single machine in an isolated mode, and the high reliability requirement of the drive control device is met.

    一种空间站大型柔性太阳翼展收及对日定向综合型驱动控制装置,针对空间站大型柔性太阳翼展收及对日定驱动功能,将实现大型柔性太阳翼多步展开的抬升机构、箱体展收机构、约束释放机构、伸展机构以及对日定向驱动机构的驱动电路集成在同一综合型驱动控制装置内部,实现了航天产品的高集成度设计;具备空间站大型柔性太阳翼按程序全自动展开或分时单步独立展收的灵活工作模式;具备高可靠的多类型指令接口设计,包括1553B总线通信以及冗余设计的OC硬线指令,在高优先级的OC硬线指令执行工况下,驱动控制任务可以隔离在单机内部最小化功能电路中完成,确保了驱动控制装置的高可靠性要求。


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    Titel :

    Flexible solar wing unfolding and folding and sun orientation comprehensive driving control device for space station


    Weitere Titelangaben:

    一种空间站柔性太阳翼展收及对日定向综合驱动控制装置


    Beteiligte:
    JIANG FANMING (Autor:in) / ZHOU WEIXING (Autor:in) / WANG JUN (Autor:in) / LI XUE (Autor:in) / ZHENG YUE (Autor:in) / QU CHUANKUN (Autor:in) / YAO WEILIN (Autor:in) / HOU CHAO (Autor:in) / WANG TAO (Autor:in) / LI HAO (Autor:in)

    Erscheinungsdatum :

    10.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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