A satellite module (10) for attitude determination comprises a housing body (11) comprising at least one data acquisition board (17) and a connection interface (14); at least one first type of sensor (12) in communication with the data acquisition board (17), the first type of sensor (12) being selected from a sun sensor, an earth sensor, a star sensor, a horizon sensor; and at least one second type of sensor (13) in communication with the data acquisition board (17), the second type of sensor (13) being different from the first type of sensor (12), the second type of sensor (13) being selected from the sun sensor, the earth sensor, the star sensor, the horizon sensor. The connection interface (14) is mounted on a first face (19) of the receiving body (11), the first type sensor (12) is mounted on a second face (20) of the receiving body (11), and the second type sensor (13) is mounted on a third face (21) of the receiving body (11).

    一种用于姿态确定的卫星模块(10)包括容纳体(11),所述容纳体(11)包括至少一个数据采集板(17)和连接接口(14);与所述数据采集板(17)通信的至少一个第一类型传感器(12),所述第一类型传感器(12)从太阳传感器、地球传感器、恒星传感器、地平线传感器中选择;和与所述数据采集板(17)通信的至少一个第二类型传感器(13),所述第二类型传感器(13)与所述第一类型传感器(12)不同,所述第二类型传感器(13)从太阳传感器、地球传感器、恒星传感器、地平线传感器中选择。所述连接接口(14)安装在所述容纳体(11)的第一面(19)上,所述第一类型传感器(12)安装在所述容纳体(11)的第二面(20)上,所述第二类型传感器(13)安装在所述容纳体(11)的第三面(21)上。


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    Titel :

    Satellite module for attitude determination


    Weitere Titelangaben:

    用于姿态确定的卫星模块


    Beteiligte:
    FERRARIO LORENZO (Autor:in) / BEVILACQUA MARCO (Autor:in) / ZORZI LUCA (Autor:in) / GRIMOLDI GIORGIO (Autor:in)

    Erscheinungsdatum :

    01.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G01S RADIO DIRECTION-FINDING , Funkpeilung



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