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A Methodology for Determining Statistical Performance Compliance for Airborne Doppler Radar with Forward-Looking Turbulence Detection CapabilityThe objective of the research developed and presented in this document was to statistically assess turbulence hazard detection performance employing airborne pulse Doppler radar systems. The FAA certification methodology for forward looking airborne turbulence radars will require estimating the probabilities of missed and false hazard indications under operational conditions. Analytical approaches must be used due to the near impossibility of obtaining sufficient statistics experimentally. This report describes an end-to-end analytical technique for estimating these probabilities for Enhanced Turbulence (E-Turb) Radar systems under noise-limited conditions, for a variety of aircraft types, as defined in FAA TSO-C134. This technique provides for one means, but not the only means, by which an applicant can demonstrate compliance to the FAA directed ATDS Working Group performance requirements. Turbulence hazard algorithms were developed that derived predictive estimates of aircraft hazards from basic radar observables. These algorithms were designed to prevent false turbulence indications while accurately predicting areas of elevated turbulence risks to aircraft, passengers, and crew; and were successfully flight tested on a NASA B757-200 and a Delta Air Lines B737-800. Application of this defined methodology for calculating the probability of missed and false hazard indications taking into account the effect of the various algorithms used, is demonstrated for representative transport aircraft and radar performance characteristics.
Document ID
20090025483
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Bowles, Roland L.
(AeroTech Research, Inc. Newport News, VA, United States)
Buck, Bill K.
(AeroTech Research, Inc. Newport News, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2009
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/CR-2009-215769
NF1676L-10742
LF99-8937
ATR-2009-12038
Report Number: NASA/CR-2009-215769
Report Number: NF1676L-10742
Report Number: LF99-8937
Report Number: ATR-2009-12038
Funding Number(s)
CONTRACT_GRANT: NNL06AA03B
TASK: NNL08AC16T
TASK: NNL07AE19T
Distribution Limits
Public
Copyright
Public Use Permitted.
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