A system (100) includes a signal generator (102) that is configured to generate a first electrical signal (130). The system (100) also includes a light source (104) configured to generate a light beam (132) based on the first electrical signal (130). The light source (104) is also configured to direct the light beam (132) towards a structural member (108) of an aircraft (300). The system (100) also includes a photoelectric sensor (112) configured to receive a reflected light beam (134) and convert the reflected light beam (134) to a second electrical signal (136). The reflected light beam (134) corresponds to a portion of the light beam (132) that is reflected from one or more optical reflectors (110) coupled to the structural member (108). The system (100) also includes circuitry (190) configured to estimate a location of a center-of-gravity (X) of the aircraft (300) based on a timing difference between the first electrical signal (130) and the second electrical signal (136).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    METHOD AND DEVICE TO ESTIMATE AIRCRAFT INFORMATION


    Weitere Titelangaben:

    VERFAHREN UND VORRICHTUNG ZUR SCHÄTZUNG VON FLUGZEUGINFORMATIONEN
    DISPOSITIF D'ESTIMATION D'INFORMATIONS D'AÉRONEFS ET PROCÉDÉ POUR UNE TELLE ESTIMATION


    Beteiligte:

    Erscheinungsdatum :

    2021-02-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Semiempirical Estimate of Aircraft Wing Weight

    York, P. / Labell, R. W. | NTRS | 1983



    Aircraft landing method, aircraft, information processing device, and program

    SUZUKI YOUICHI | Europäisches Patentamt | 2023

    Freier Zugriff

    A Neural Network Model to Estimate Aircraft Fuel Consumption

    Trani, Antonio / Wing-Ho, F. / Schilling, Glen et al. | AIAA | 2004