Biomimetic Optical Sensor for Real-Time Aircraft Wing Deflection MeasurementReducing the environmental impact of aviation is a primary goal of NASA aeronautics research. One approach to achieve this goal is to build lighter weight aircraft, which presents complex challenges due to a corresponding increase in structural flexibility. Wing flexibility can adversely affect aircraft performance from the perspective of aerodynamic efficiency and safety. Knowledge of the wing position during flight can aid active control methods designed to mitigate problems due to increased wing flexibility. Current approaches to measuring wing deflection, including strain measurement devices, accelerometers, or GPS solutions, and new technologies such as fiber optic strain sensors, have limitations for their practical application to flexible aircraft control. Hence, it was proposed to use a bio-mimetic optical sensor based on the fly-eye to track wing deflection in real-time. The fly-eye sensor has several advantages over conventional sensors used for this application, including light weight, low power requirements, fast computation, and a small form factor. This paper reports on the fly-eye sensor development and its application to real-time wing deflection measurement.
Document ID
20190001122
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Frost, Susan A. (NASA Ames Research Center Moffett Field, CA, United States)
Wright, Cameron H. G. (Wyoming Univ. Laramie, WY, United States)
Khan, Md. Arif (Wyoming Univ. Laramie, WY, United States)
Date Acquired
March 4, 2019
Publication Date
January 5, 2015
Subject Category
Instrumentation And PhotographyAircraft Stability And ControlElectronics And Electrical Engineering
Report/Patent Number
ARC-E-DAA-TN19511Report Number: ARC-E-DAA-TN19511
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)