Accelerometers and 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%3A03117923" target="_blank" >RIV/68407700:21230/05:03117923 - 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 an Aircraft Attitude Evaluation
Original language description
The paper describes a method that enables a usage of low-cost inertial sensors, such as angular rate sensors and accelerometers, in a system of aircraft attitude evaluation. The method depicts a suitability of using accelerometers to restrict an influence of angular rates’ integration on a precision of the attitude assessment. The method was verified with a simulation in MATLAB-Simulink environment and with various measurements. The method principles, simulation and measurement results are presented.
Czech name
Akcelerometry a měření výšky letu
Czech description
V příspěvku je popsána metoda použití cenově dostupných inerciálních senzorů jako akcelerometrů.
Classification
Type
A - Audiovisual production
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
ISBN
0-7803-9057-1
Place of publication
Irvine, CA
Publisher/client name
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Version
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Carrier ID
neuvedeno