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Standalone Trailing Probe for Aero metrical Measurements

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F12%3A00196767" target="_blank" >RIV/68407700:21230/12:00196767 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Standalone Trailing Probe for Aero metrical Measurements

  • Original language description

    This article describes a design of a probe intended for aero metrical instrument testing which is being hanged under an airplane. The probe collects data in an undisturbed airfield and compares them with data provided by dashboard instruments. The differences reveal quality of an airplane prototype design during maiden flights. The most important flight instruments are an altimeter and an air speed indicator. These instruments can be tested by comparison with data from a trailing bomb probe. While commonly used probes fed pressure from the probe entry points up to the airplane cabin by pipes, the prototype described in this paper uses wireless data link to transfer data to a data acquisition unit. Beside the altitude and speed the probe also measures its angle of attack and angle of sideslip which are used onboard to compensate for errors caused by probe alignment within the airfield. The designed system consists of two parts: the probe itself and a winch mechanism. Because the probe s

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/TA01030651" target="_blank" >TA01030651: Safety Improvement of Flight, Crew and Other Participants of Flight Transport in Normal and Emergency Situations by Assistive Technologies</a><br>

  • Continuities

    S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2012

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    DASC 2012 - 31th Digital Avionics System Conference - Proceedings

  • ISBN

    978-1-4673-1698-9

  • ISSN

    2155-7195

  • e-ISSN

  • Number of pages

    12

  • Pages from-to

    1-12

  • Publisher name

    IEEE Operations Center

  • Place of publication

    Piscataway

  • Event location

    Williamsburg

  • Event date

    Oct 14, 2012

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000316917202015