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

1 Cita (Scopus)

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
Publicado de forma externa
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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