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Recent flight-test results of optical airdata techniquesOptical techniques for measuring airdata parameters have been demonstrated with promising results on high-performance fighter aircraft. These systems can measure the airspeed vector, and some are not as dependent on special in-flight calibration processes as current systems. Optical concepts for measuring free stream static temperature and density are feasible for in-flight as applications. The best feature of these concepts is that the airdata measurements are obtained nonintrusively, and for the most part well into the freestream region of the flowfield about the aircraft. Current requirements for measuring airdata at high angle of attack, and future need to measure the same information at hypersonic flight conditions place strains on existing techniques. Optical technology advances show outstanding potential for application in future programs and promise to make common use of optical concepts a reality. This paper summarizes results from several flight-test programs and identifies the technology advances required to make optical airdata techniques practical.
Document ID
19930029268
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bogue, Rodney K.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Instrumentation
Report/Patent Number
AIAA PAPER 92-4086
Report Number: AIAA PAPER 92-4086
Meeting Information
Meeting: AIAA, Biennial Flight Test Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: AIAA
Accession Number
93A13265
Distribution Limits
Public
Copyright
Other

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