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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    Title :

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


    Additional title:

    一种控制力矩陀螺在轨自主起旋控制方法


    Contributors:
    CHEN HUA (author) / DU YAOKE (author) / KANBI (author) / WANG YU (author) / WANG JIAYI (author) / YUE YANG (author) / LIU MEISHI (author)

    Publication date :

    2025-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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