An unmanned aerial vehicle is provided, including a primary operation system in communication with a primary state estimator. The primary operation system is configured to operate the unmanned aerial vehicle based in part on the primary state estimator. The vehicle includes a flight failure recovery system in communication with a recovery state estimator and the primary operation system. The flight failure recovery system is configured to determine, at a first time, that flight failure has occurred. The flight failure recovery system is configured to determine a suitable second time to generate a deploy signal for a parachute based at least in part on one or more signals from the recovery state estimator. There is a delay between the first time and the suitable second time. An intelligent emergency parachute deployment system for, and a method for flight failure recovery of an unmanned aerial vehicle are also provided.


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    Titel :

    UNMANNED AERIAL VEHICLE RECOVERY SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    2018-12-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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