The invention discloses a satellite magnetic torquer control capability analysis method, and belongs to the technical field of satellite attitude and orbit control. The method comprises the following steps: firstly, acquiring triaxial magnetic field intensity data under a satellite body system; then, traversing all specified torque directions, for each specified torque direction, firstly calculating the average value of the maximum magnetic torques under different magnetic field intensities, and then calculating the corresponding magnetic torquer control capability; and finally, based on the control capability of the magnetic torquer in each specified torque direction, analyzing whether the magnetic torquer meets the control requirement or not. According to the method, the control capability of the magnetic torquer can be accurately obtained, and a decision basis is provided for configuration selection of the magnetic torquer.

    本发明公开了一种卫星磁力矩器控制能力分析方法,属于卫星姿态与轨道控制技术领域。该方法首先获取卫星本体系下的三轴磁场强度数据;接着,遍历所有指定力矩方向,对于每一个指定力矩方向,先计算不同磁场强度下最大磁力矩的平均值,再计算对应的磁力矩器控制能力;最后基于各指定力矩方向的磁力矩器控制能力,分析磁力矩器是否满足控制需求。本发明能够准确得到磁力矩器的控制能力,为磁力矩器配置选取提供决策依据。


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    Title :

    Satellite magnetic torquer control capability analysis method


    Additional title:

    一种卫星磁力矩器控制能力分析方法


    Contributors:
    ZHANG KAICHENG (author) / ZHAI XINGHUI (author) / SUN SHANG (author) / NIU WENTING (author) / YANG YULONG (author) / ZHU WENSHAN (author)

    Publication date :

    2025-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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