One or more embodiments of the present disclosure include features and functionality that reduce size, weight, and power (SWaP) specifications for an unmanned aerial vehicle (UAV) by combining flight control functionality with mission processing functionality within common hardware. By implementing flight control and mission processing functionality using common hardware, systems and methods described herein decrease costs associated with developing, producing, servicing, and operating UAVs. Moreover, the systems and methods described herein include features that reduce the SWaP for the UAV while providing further redundancies that maintain reliability of the UAV.


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    Titel :

    Unified and redundant flight and mission control for an unmanned aerial vehicle


    Beteiligte:

    Erscheinungsdatum :

    26.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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