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contributor authorWood, R.
contributor authorStromberg, I. M.
contributor authorJonas, P. R.
contributor authorMill, C. S.
date accessioned2017-06-09T14:08:03Z
date available2017-06-09T14:08:03Z
date copyright1997/08/01
date issued1997
identifier issn0739-0572
identifier otherams-1305.pdf
identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4148457
description abstractA system has been developed for use on a light aircraft for the measurement of the turbulent wind vector components that does not rely on the use of either an inertial navigation system (INS) or Doppler radar. The system described here uses a five-hole probe to measure the wind vector relative to the aircraft. A GPS system, a vertical gyroscope for aircraft pitch and roll angles, a gyrocompass system, and a strap-down three-axis accelerometer system are used to obtain aircraft motion. Flight tests and results of an intercomparison with the United Kingdom Meteorological Office C-130 are presented. Under conditions of straight and level flight, the estimated rms errors are 0.3 m s?1 for the vertical wind component and 2 m s?1 for the horizontal components.
publisherAmerican Meteorological Society
titleAnalysis of an Air Motion System on a Light Aircraft for Boundary Layer Research
typeJournal Paper
journal volume14
journal issue4
journal titleJournal of Atmospheric and Oceanic Technology
identifier doi10.1175/1520-0426(1997)014<0960:AOAAMS>2.0.CO;2
journal fristpage960
journal lastpage968
treeJournal of Atmospheric and Oceanic Technology:;1997:;volume( 014 ):;issue: 004
contenttypeFulltext


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