一种阵列式卫星智能姿控组件,包括:箱体(1)、反作用飞轮(2)、磁力矩器(3)、磁力矩器线圈(4)、控制板(5)、陀螺仪(6),箱体的每个侧壁设置四组定位孔,左右侧壁的定位孔上布置八个X轴反作用飞轮(21),前后侧壁的定位孔上布置八个Y轴反作用飞轮(22);控制板安装在箱体的底壁的中心处,在控制板上布置八个Z轴反作用飞轮(23);磁力矩器对反作用飞轮进行磁卸载,安装在箱体的底壁上,且包括X轴磁力矩器(31)、Y轴磁力矩器(32);磁力矩器线圈安装在磁力矩器和控制板之间,且为Z轴方向;陀螺仪数量为三个且集中在一起安装在控制板的中心处。还有工作方法。

    An array type satellite intelligent attitude control assembly comprises a box body (1), reaction flywheels (2), a magnetic torquer (3), a magnetic torquer coil (4), a control panel (5) and a gyroscope (6), four sets of positioning holes are formed in each side wall of the box body, eight X-axis reaction flywheels (21) are arranged on the positioning holes in the left side wall and the right side wall, and eight Y-axis reaction flywheels (22) are arranged on the positioning holes in the front side wall and the rear side wall; the control panel is installed at the center of the bottom wall of the box body, and eight Z-axis reaction flywheels (23) are arranged on the control panel; the magnetic torquer is used for performing magnetic unloading on the reaction flywheel, is mounted on the bottom wall of the box body, and comprises an X-axis magnetic torquer (31) and a Y-axis magnetic torquer (32); the magnetic torquer coil is installed between the magnetic torquer and the control panel and is in the Z-axis direction. The number of the gyroscopes is three, and the gyroscopes are concentrated together and installed at the center of the control panel. A working method is also provided.


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    Titel :

    一种阵列式卫星智能姿控组件及其工作方法


    Erscheinungsdatum :

    2024-07-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS