A compact SFS may can be deployed in small space vehicles. The SFS may have a small size, weight, and low power requirements. The hardware, software, catalogs, and calibration algorithm of the SFS provide highly accurate attitude information that can be used for pointing. For instance, accurate attitude determination may be provided that supports pointing of a deployable high gain helical antenna. A full “lost in space” attitude solution, accurate to about an arcminute, may be accomplished in under a minute. The SFS may be fully reprogrammable on orbit, allowing continued algorithm development and deployment after launch.


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    Titel :

    Compact star-field sensor (SFS)


    Beteiligte:
    DALLMANN NICHOLAS (Autor:in) / WREN JAMES (Autor:in) / PROICOU MICHAEL (Autor:in) / MOHR HANNAH (Autor:in) / DELAPP JERRY (Autor:in) / KATKO KIMBERLY (Autor:in) / MARTINEZ JOHN (Autor:in) / ORTEGA DONATHAN (Autor:in) / SEITZ DANIEL (Autor:in) / STEIN PAUL (Autor:in) ... [mehr]

    Erscheinungsdatum :

    29.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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