A spacecraft includes a body having a motor, a lander interface, a sensor and a power source for powering the motor and the sensor, and the power source being mounted thereon. An integrated avionics unit has a module and an integrated circuit with the module having a central computer and a motor controller for controlling the motor and the integrated circuit having a temperature monitoring system for monitoring the temperature of the spacecraft and a power regulator having a cell balancer for regulating the power of the power source. The module and the integrated circuit are connected to one another for constant communication therebetween. The central computer communicates with the sensor.


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    Titel :

    INTEGRATED AVIONICS UNIT


    Beteiligte:
    CORPA DE LA FUENTE CEDRIC (Autor:in) / ARBUCKLE TROY (Autor:in) / QUINN KERRY (Autor:in) / DAVIS ANDREA (Autor:in) / PROVENZANO MIKE (Autor:in) / ZIMO JOSEPH (Autor:in) / LNU UPASANA (Autor:in) / SHAPIRO JOSHUA (Autor:in) / GASPARRO NOAH (Autor:in)

    Erscheinungsdatum :

    17.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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