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Performance Evaluation Of Two Altimeters Intended For Euler Angles Measurement

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F13%3A00208418" target="_blank" >RIV/68407700:21230/13:00208418 - isvavai.cz</a>

  • Result on the web

    <a href="http://dx.doi.org/10.1109/DASC.2013.6712653" target="_blank" >http://dx.doi.org/10.1109/DASC.2013.6712653</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1109/DASC.2013.6712653" target="_blank" >10.1109/DASC.2013.6712653</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Performance Evaluation Of Two Altimeters Intended For Euler Angles Measurement

  • Original language description

    This paper describes usage of two pressure altimeters to measure an airplane position angle, e.g. pitch or roll. The measurement relates to the properties of the standard atmosphere where the pressure descends with increasing altitude. The altitudes measured by two altimeters allow us to determine their mutual vertical difference. While we know the shortest distance between these two altimeters we can calculate the required positional angle of an airplane. There are multiple ways how to compose a measurement system using this principle. One possible solution is based on two absolute sensors. In this case the precision of the pressure sensors is the crucial parameter. In this article we describe sensor modules with wireless interface using two types ofsensors and we evaluate their performance for the proposed position angle measurement application. There are two types of sensors compared in the article. First of them is a cheap MEMS sensor LPS001DL provided by ST microelectronics with

  • 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

    2013

  • 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 2013 - 32nd Digital Avionics Systems Conference 2013

  • ISBN

    978-1-4799-1538-5

  • ISSN

    2155-7195

  • e-ISSN

  • Number of pages

    11

  • Pages from-to

    "8C31"-"8C312"

  • Publisher name

    AIAA

  • Place of publication

    Reston, VA

  • Event location

    Syracuse

  • Event date

    Oct 6, 2013

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000350222202039