The present invention extends to methods, systems, devices, and apparatus for failover navigation for remotely operated aerial vehicles. During flight, a primary guidance system uses a higher resolution map for an area to guide a remotely operated aerial vehicle around obstacles (e.g., buildings) in the area. Failure of the primary guidance system is detected during flight. The remotely operated aerial vehicle switches over to a secondary guidance system in response to detecting the failure. The secondary guidance system formulates a flight path to a safer location based on a lower resolution map of the area. The formulated flight path minimizes crossings between different boundaries represented in the lower resolution map. The formulated flight path is biased towards safety over efficiency.


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    Titel :

    Failover navigation for remotely operated aerial vehicles


    Beteiligte:

    Erscheinungsdatum :

    27.08.2019


    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 / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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