Expand this Topic clickable element to expand a topic
Skip to content
Optica Publishing Group

Distributed Fiber-optic Sensing, Structural Monitoring and Control System for Aircraft

Not Accessible

Your library or personal account may give you access

Abstract

A concept of distributed fiber-optic sensing, monitoring and control for smart aircraft is introduced. In-flight sensing results are shown with comparison to aeroelastic analysis. Aerodynamic load identification is also conducted.

© 2022 The Author(s)

PDF Article
More Like This
Distributed Fiber Optic Sensing for Aircraft Towards In- Flight Structural Control

Daichi Wada and Hirotaka Igawa
W2B.1 Optical Fiber Sensors (OFS) 2020

Development of Fiber Optic Distributed Sensing System for Aircraft Wing and its On-board Monitoring during Flight Tests

Daichi Wada, Hirotaka Igawa, Masato Tamayama, Tokio Kasai, Hitoshi Arizono, and Hideaki Murayama
WF98 Optical Fiber Sensors (OFS) 2018

Adaptive Load Control of Flexible Aircraft Wings Using Fiber Optic Sensing

Francisco Pena, Benjamin Martins, and W. Lance Richards
WF101 Optical Fiber Sensors (OFS) 2018

Select as filters


Select Topics Cancel
© Copyright 2024 | Optica Publishing Group. All rights reserved, including rights for text and data mining and training of artificial technologies or similar technologies.