Digital twin concept for aircraft system failure detection and correction

Omar Hazbon Alvarez, Luis B. Gutierrez Zea, Cees Bil, Mario L. Fravolini, Marcello Napolitano

    Resultado de la investigación: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

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    Resumen

    The air data system estimates vital flight parameters for correct and safe aircraft operation. One of the main components in this system is the Pitot tube sensor for measuring the total pressure and static pressure to estimate altitude, air speed, vertical speed and Mach number. The Pitot tube can supply incorrect measurement readings when its orifices are blocked by ice, dust or even insects. This paper describes the results of an ongoing research project to develop a solution to aircraft loss of control caused by an unreliable airspeed indication by incorporating the concept of an aircraft digital twin.

    Idioma originalInglés
    Título de la publicación alojadaAIAA Aviation 2019 Forum
    EditorialAmerican Institute of Aeronautics and Astronautics Inc, AIAA
    ISBN (versión impresa)9781624105890
    EstadoPublicada - 2019
    EventoAIAA Aviation 2019 Forum - Dallas, Estados Unidos
    Duración: 17 jun. 201921 jun. 2019

    Serie de la publicación

    NombreAIAA Aviation 2019 Forum

    Conferencia

    ConferenciaAIAA Aviation 2019 Forum
    País/TerritorioEstados Unidos
    CiudadDallas
    Período17/06/1921/06/19

    Nota bibliográfica

    Publisher Copyright:
    © 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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