Accelerometers and their Usage in an Aircraft Attitude Evaluation
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F05%3A03109366" target="_blank" >RIV/68407700:21230/05:03109366 - 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
Accelerometers and their Usage in an Aircraft Attitude Evaluation
Original language description
The paper describes a method that enables a usage of low-cost angular rate sensors in an aircraft attitude evaluation. The method depicts a suitability of using accelerometers to restrict an influence of angular rate integration on a precision of the attitude assessment. The method was verified with a simulation in MATLAB-Simulink environment. The method principle and its simulation results are presented.
Czech name
Akcelerometry a jejich použití při určení polohy letadla
Czech description
Není k dispozici
Classification
Type
D - Article in proceedings
CEP classification
JB - Sensors, detecting elements, measurement and regulation
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
2005
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Applied Electronics 2005 - International Conference Pilsen
ISBN
80-7043-369-8
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
285-288
Publisher name
Západočeská universita
Place of publication
Plzeň
Event location
Pilsen
Event date
Sep 7, 2005
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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