Unmanned aerial vehicle takeoff, navigation and landing support system. The invention relates to a location support system that can be used in the take-off, navigation and landing stages of unmanned aerial vehicles (1) in environments where GNSS signals are inhibited/not available. To do this, there are prisms (2) attached to the unmanned aerial vehicle (1), capable of 360-degree retroreflective reflection, attached to each other at a 45-degree angle. The theodolite (7), which is a part of the azimuth and position measurement system (3), is optically oriented towards the prisms (2) of the unmanned aerial vehicle (1) and tracks the unmanned aerial vehicle (1), Instantly measures its distance to the UAV (1) and sends it to the processor along with the azimuth and elevation angles of the line of sight relative to its axis. The processor calculates the absolute position of the unmanned aerial vehicle (1) using the data from the theodolite (7) and the inertial navigation system (8). The ground measurement system (3) instantly sends the calculated position information to the unmanned aerial vehicle (1). (Machine-translation by Google Translate, not legally binding)


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    Titel :

    SISTEMA DE APOYO AL DESPEGUE, NAVEGACION Y ATERRIZAJE DE VEHICULOS AEREOS NO TRIPULADOS


    Beteiligte:

    Erscheinungsdatum :

    27.09.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Spanisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / G01S RADIO DIRECTION-FINDING , Funkpeilung



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