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A method of wind shear detection for powered-lift STOL aircraftA new wind shear warning system for powered-lift STOL aircraft was evaluated by using a flight simulator. Wind shear warning systems for CTOL aircraft have been designed to detect horizontal shear only. Because the approach air speed of STOL aircraft is lower than that for CTOL aircraft, STOL aircraft are more vulnerable to vertical wind due to (1) a gradient of horizontal shear that is smaller for STOL than for CTOL aircraft because of slower airspeed; (2) STOL aircraft spend longer time in a downdraft; and (3) vertical wind causes a more radical change in the STOL aircraft's flight path because of its lower airspeed. In order to detect the vertical wind, the wind shear warning system proposed calculates the difference between potential flight path measured on-board during shear traversal and trimmed flight path estimated from aircraft status. The most characteristic feature of this new system is that it utilizes only inertial information and pitot-static airspeed data; this yields a convenient means of on-board implementation. Simulation test results confirm that the new system can detect the vertical shear.
Document ID
19930064348
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Funabiki, Kohei
(NASA Ames Research Center Moffett Field, CA, United States)
Bando, Toshio
(NASA Ames Research Center Moffett Field, CA, United States)
Tanaka, Keiji
(National Aerospace Lab. Tokyo, Japan)
Hynes, Charles S.
(NASA Ames Research Center Moffett Field, CA, United States)
Hardy, Gordon H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Atmospheric Flight Mechanics Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers (A93-48301 20-08)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aircraft Instrumentation
Report/Patent Number
AIAA PAPER 93-3667
Accession Number
93A48345
Distribution Limits
Public
Copyright
Other

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