The invention relates to an in-orbit autonomous rotation starting control method for a control moment gyroscope, which can autonomously complete rotation starting of the control moment gyroscope without relying on the ground after injection into an orbit, can diagnose and recover a faulted control moment gyroscope in the process, does not generate extra disturbance moment to a star body, and can be quickly accessed to carry out attitude control. During steady-state control, according to the state of a current control moment gyroscope access system, when the access number is greater than 3, the position of a theoretical frame of the control moment gyroscope is planned, zero-motion maneuvering rate control is added, and instruction resolving is performed by taking the position of the theoretical frame as a target, so that the control moment gyroscope is prevented from staying near a certain fixed position in an on-orbit frame.

    一种控制力矩陀螺在轨自主起旋控制方法,能够在入轨后不依靠地面,自主完成控制力矩陀螺的起旋,在此过程中能够对故障的控制力拒陀螺进行诊断与恢复,不对星体产生额外干扰力矩,使其能够快速接入以进行姿态控制。稳态控制时,根据当前控制力矩陀螺接入系统的状态,当接入个数大于3时对控制力拒陀螺理论框架位置进行规划,加入零运动操纵率控制,以理论框架位置为目标进行指令解算,避免控制力矩陀螺在轨框架停留在某一固定位置附近。


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    Titel :

    In-orbit autonomous rotation starting control method for control moment gyroscope


    Weitere Titelangaben:

    一种控制力矩陀螺在轨自主起旋控制方法


    Beteiligte:
    CHEN HUA (Autor:in) / DU YAOKE (Autor:in) / KANBI (Autor:in) / WANG YU (Autor:in) / WANG JIAYI (Autor:in) / YUE YANG (Autor:in) / LIU MEISHI (Autor:in)

    Erscheinungsdatum :

    25.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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