Digital twin concept for aircraft system failure detection and correction

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

Digital twin concept for aircraft system failure detection and correction

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

Producción científica: Capítulo del libro/informe/acta de congreso › Ponencia publicada en las memorias del evento con ISBN › revisión exhaustiva

2 Citas (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 original	Inglés
Título de la publicación alojada	AIAA Aviation 2019 Forum
Editorial	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (versión impresa)	9781624105890
Estado	Publicada - 2019
Evento	AIAA Aviation 2019 Forum - Dallas, Estados Unidos Duración: 17 jun. 2019 → 21 jun. 2019

Serie de la publicación

Nombre	AIAA Aviation 2019 Forum

Conferencia

Conferencia	AIAA Aviation 2019 Forum
País/Territorio	Estados Unidos
Ciudad	Dallas
Período	17/06/19 → 21/06/19

Nota bibliográfica

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

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title = "Digital twin concept for aircraft system failure detection and correction",

abstract = "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.",

author = "Alvarez, {Omar Hazbon} and {Gutierrez Zea}, {Luis B.} and Cees Bil and Fravolini, {Mario L.} and Marcello Napolitano",

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Digital twin concept for aircraft system failure detection and correction. / Alvarez, Omar Hazbon; Gutierrez Zea, Luis B.; Bil, Cees et al.
AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (AIAA Aviation 2019 Forum).

Producción científica: Capítulo del libro/informe/acta de congreso › Ponencia publicada en las memorias del evento con ISBN › revisión exhaustiva

TY - GEN

T1 - Digital twin concept for aircraft system failure detection and correction

AU - Alvarez, Omar Hazbon

AU - Gutierrez Zea, Luis B.

AU - Bil, Cees

AU - Fravolini, Mario L.

AU - Napolitano, Marcello

PY - 2019

Y1 - 2019

N2 - 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.

AB - 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.

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M3 - Ponencia publicada en las memorias del evento con ISBN

AN - SCOPUS:85098261575

SN - 9781624105890

T3 - AIAA Aviation 2019 Forum

BT - AIAA Aviation 2019 Forum

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - AIAA Aviation 2019 Forum

Y2 - 17 June 2019 through 21 June 2019

ER -

Digital twin concept for aircraft system failure detection and correction

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