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


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    Titel :

    Satellite module for attitude determination


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

    Erscheinungsdatum :

    10.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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