The invention provides a spaceflight launch condition control method and device based on state transition, and the method comprises the steps: determining a security recovery point closest to the current state of a spaceflight launch system when a launch program is interrupted due to the fault of a spaceflight launch task; matching a current condition in pre-formulated state transition conditions of the spaceflight launch task, and determining a path from the current state to the security recovery point; transferring the spaceflight launch task from the current state to the security recovery point along the path by implementing a pre-formulated state transfer measure; and taking the security recovery point as a reentry program point of the spaceflight launch task, and reentering the launch program when a reentry launch program condition is met. According to the method, the task can be transferred to the expected state when the system breaks down, and it is ensured that the spaceflight launching task is implemented according to the preset launching program.

    本申请提供了一种基于状态转移的航天发射条件控制方法及装置,其中的方法包括:当航天发射任务因故障发生导致发射程序中断时,确定航天发射系统的当前状态最邻近的安全恢复点;在预先制定的航天发射任务的状态转移条件中匹配当前的条件,确定从当前状态转移至安全恢复点的路径;通过实施预先制定的状态转移的措施,使航天发射任务从当前状态沿所述路径转移到安全恢复点;将所述安全恢复点作为航天发射任务的再入程序点,当再入发射程序条件满足则重新进入发射程序。本申请的方法能够使系统发生故障时任务向期望的状态转移,确保航天发射任务按预定的发射程序实施。


    Access

    Download


    Export, share and cite



    Title :

    Spaceflight launching condition control method and device based on state transition


    Additional title:

    一种基于状态转移的航天发射条件控制方法及装置


    Contributors:
    DONG XUEJUN (author) / ZHONG WENAN (author) / YAN ZHENG (author) / DU JIANZHOU (author) / FAN JIANBO (author) / CHEN SHAOJIANG (author) / YE XIN (author) / LI LIJIE (author) / ZHANG JUNXIN (author)

    Publication date :

    2024-09-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Spaceflight launching system pipeline based on vacuum pipeline acceleration and launching method

    ZHANG YAOPING / QING SHAN / ZHAO YONG | European Patent Office | 2020

    Free access

    Diversion trench device suitable for offshore spaceflight launching platform

    LIN TONG / WEI ZHIYUAN / ZHONG WEIDONG et al. | European Patent Office | 2022

    Free access

    Digital twin system of spaceflight launching site

    ZUO YUQIN / WANG SANQIANG | European Patent Office | 2023

    Free access

    Automatic locking device for rotary platform of spaceflight launching tower

    JIANG PENG / ZHAI JING / DONG QIANG et al. | European Patent Office | 2023

    Free access

    Vacuum pipeline spaceflight launching tail section air pressure balancing device and method

    ZHANG YAOPING / QING SHAN / ZHAO YONG | European Patent Office | 2020

    Free access