Filtering Methods of the Inertial Position Measuring System
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F11%3A00181631" target="_blank" >RIV/68407700:21230/11:00181631 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Filtering Methods of the Inertial Position Measuring System
Original language description
This paper describes a part of experimental project focused on inertial position measurement. Paper aims to filtering process of position and attitude estimation. In addition, the position evaluation process contains three filtering steps. Those steps are described separately. Inertial measuring unit (IMU) use a MEMS (Microelectromechanical Systems) technology sensors in specific application. This application is a tracking of the aerobatic aircraft flight path. Measurement by MEMS inertial sensors in this application is influenced by many types of noise. Described three step filtering process is trying to remove position and attitude error as much as possible.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JA - Electronics and optoelectronics
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Proceedings of the 2011 International Conference on Telecommunication Systems Management
ISBN
978-0-9820958-4-3
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
35-38
Publisher name
American Telecommunications Systems Management Association Inc.
Place of publication
Dallas, TX
Event location
Praha
Event date
May 26, 2011
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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