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    Inertial Drift Correction for Aircraft-Derived Wind Fields

    Source: Journal of Atmospheric and Oceanic Technology:;1988:;volume( 005 ):;issue: 006::page 774
    Author:
    Shaw, William J.
    DOI: 10.1175/1520-0426(1988)005<0774:IDCFAD>2.0.CO;2
    Publisher: American Meteorological Society
    Abstract: During the last three decades, aircraft have assumed an increasingly important role as platforms for atmospheric measurement. Because of the nature of the wind measurement process, however, low-frequency winds remain susceptible to significant errors, which have their origin in the inertial navigation system (INS) of the aircraft. Computations are presented showing that the Electra, a state-of-the-art aircraft for meteorological measurements, experiences low-frequency wind measurement errors typically as large as 3 m s?1 in each component of the horizontal wind. Errors of this magnitude can produce can produce line-integral divergence errors of 10?4 s?1 in typical flight geometries. Use of the LORAN-C navigational information now received on the aircraft offers an order-of-magnitude reduction of errors from the INS.
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      Inertial Drift Correction for Aircraft-Derived Wind Fields

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4180400
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    contributor authorShaw, William J.
    date accessioned2017-06-09T15:22:10Z
    date available2017-06-09T15:22:10Z
    date copyright1988/12/01
    date issued1988
    identifier issn0739-0572
    identifier otherams-418.pdf
    identifier urihttp://onlinelibrary.yabesh.ir/handle/yetl/4180400
    description abstractDuring the last three decades, aircraft have assumed an increasingly important role as platforms for atmospheric measurement. Because of the nature of the wind measurement process, however, low-frequency winds remain susceptible to significant errors, which have their origin in the inertial navigation system (INS) of the aircraft. Computations are presented showing that the Electra, a state-of-the-art aircraft for meteorological measurements, experiences low-frequency wind measurement errors typically as large as 3 m s?1 in each component of the horizontal wind. Errors of this magnitude can produce can produce line-integral divergence errors of 10?4 s?1 in typical flight geometries. Use of the LORAN-C navigational information now received on the aircraft offers an order-of-magnitude reduction of errors from the INS.
    publisherAmerican Meteorological Society
    titleInertial Drift Correction for Aircraft-Derived Wind Fields
    typeJournal Paper
    journal volume5
    journal issue6
    journal titleJournal of Atmospheric and Oceanic Technology
    identifier doi10.1175/1520-0426(1988)005<0774:IDCFAD>2.0.CO;2
    journal fristpage774
    journal lastpage782
    treeJournal of Atmospheric and Oceanic Technology:;1988:;volume( 005 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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