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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    Title :

    Satellite module for attitude determination


    Contributors:

    Publication date :

    2022-02-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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