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AGARD-RTO-AG-160-V22

AGARD-RTO-AG-160-V22
  • Version
  • 258 Downloads
  • 3.47 MB File Size
  • 1 File Count
  • April 28, 2016 Create Date
  • April 28, 2016 Last Updated
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Application of Fiber Optic Instrumentation
AGARD-RTO-AG-160-V22 Application of Fiber Optic Instrumentation
This AGARDograph presents an introduction to fiber optic systems and is intended to provide a basic
understanding of the utilization of these systems for aircraft instrumentation. It documents the current state
of the art and provides references for users of this technology to track the rapid advances expected in fiber
optic technology in the coming years.
Revolutionary advances in fiber optic technology, as applied to flight-test instrumentation, have been
achieved over the last decade and are expected to continue at a rapid pace for the foreseeable future. There
has been significant maturation in both the manufacturing of fibers and the miniaturization of hardware,
which has enabled movement of this technology from controlled laboratory environments to realistic aircraft
operations. The ability to closely space sensors on the fibers has improved by orders of magnitude and the
capability for continuous sensors is rapidly becoming feasible. Fiber optic systems will revolutionize flight-
test instrumentation for all of the NATO members, potentially eliminating strain gages and their associated
wiring while collecting more accurate and densely spaced measurements at a significantly reduced system
weight. Fiber optic instrumentation provides the ability to capture system—wide stress, strain, and temperature
measurements far beyond classic aircraft flight-test instrumentation applications. The technology also
enables the determination of many other derived engineering parameters such as structural shape, and applied
loads; information that has not been available before with conventional aircraft sensors systems.
This AGARDograph documents the current state of the art for this technology and provides references for
users to track the rapid advances expected in fiber optics in the coming years. One application for this
technology could be to a wide range of NATO aircraft systems in order to establish a comprehensive set of
data for aging aircraft. Other future applications could entail embedding fiber optic systems in composite
structures as they are manufactured, allowing extremely light-weight flexible structures to be actively
controlled, giving enhanced capability to air, surface, and ground—based NATO systems.

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AGARD-RTO-AG-160-V22

AGARD-RTO-AG-160-V22
  • Version
  • 258 Downloads
  • 3.47 MB File Size
  • 1 File Count
  • April 28, 2016 Create Date
  • April 28, 2016 Last Updated
Scroll for Details

Application of Fiber Optic Instrumentation
AGARD-RTO-AG-160-V22 Application of Fiber Optic Instrumentation
This AGARDograph presents an introduction to fiber optic systems and is intended to provide a basic
understanding of the utilization of these systems for aircraft instrumentation. It documents the current state
of the art and provides references for users of this technology to track the rapid advances expected in fiber
optic technology in the coming years.
Revolutionary advances in fiber optic technology, as applied to flight-test instrumentation, have been
achieved over the last decade and are expected to continue at a rapid pace for the foreseeable future. There
has been significant maturation in both the manufacturing of fibers and the miniaturization of hardware,
which has enabled movement of this technology from controlled laboratory environments to realistic aircraft
operations. The ability to closely space sensors on the fibers has improved by orders of magnitude and the
capability for continuous sensors is rapidly becoming feasible. Fiber optic systems will revolutionize flight-
test instrumentation for all of the NATO members, potentially eliminating strain gages and their associated
wiring while collecting more accurate and densely spaced measurements at a significantly reduced system
weight. Fiber optic instrumentation provides the ability to capture system—wide stress, strain, and temperature
measurements far beyond classic aircraft flight-test instrumentation applications. The technology also
enables the determination of many other derived engineering parameters such as structural shape, and applied
loads; information that has not been available before with conventional aircraft sensors systems.
This AGARDograph documents the current state of the art for this technology and provides references for
users to track the rapid advances expected in fiber optics in the coming years. One application for this
technology could be to a wide range of NATO aircraft systems in order to establish a comprehensive set of
data for aging aircraft. Other future applications could entail embedding fiber optic systems in composite
structures as they are manufactured, allowing extremely light-weight flexible structures to be actively
controlled, giving enhanced capability to air, surface, and ground—based NATO systems.

FileAction
AGARD-RTO-AG-160-V22 Application of Fiber Optic Instrumentation.pdfDownload 
17,005 Documents in our Technical Library
3180460 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...