The invention relates to a multi-momentum wheel angular momentum maximum envelope calculation in-orbit implementation method, and belongs to the technical field of satellite attitude control. According to the analytical calculation method, the maximum envelope of the angular momentum under any momentum wheel combination can be rapidly and conveniently obtained through one-time calculation so that a momentum wheel output torque can be distributed according to the maximum envelope surface, the angular momentum output capacity of a wheel train is fully utilized, and finally the rapid maneuvering capacity of the whole satellite is effectively improved.

    本发明涉及一种多动量轮角动量最大包络计算在轨实现方法,属于卫星姿态控制技术领域。本发明解析计算方法,通过一次计算即可快速便捷地获得任意动量轮组合下的角动量最大包络,从而可根据其最大包络面分配动量轮输出力矩,以充分利用轮系的角动量输出能力,最终有效提升整星快速机动能力。


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    Title :

    Multi-momentum wheel angular momentum maximum envelope calculation in-orbit implementation method


    Additional title:

    一种多动量轮角动量最大包络计算在轨实现方法


    Contributors:
    LU DONGNING (author) / LEI YONGJUN (author) / WANG SHUYI (author) / CHEN CHAO (author) / WANG JINPENG (author) / LIU JIE (author) / GUAN HONG (author) / XIE MINGYU (author) / QI YANXIA (author) / LI JINGXIN (author)

    Publication date :

    2021-08-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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