Influence of vibration on gravitational acceleration vector measurement
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F18%3A00534559" target="_blank" >RIV/60162694:G43__/18:00534559 - isvavai.cz</a>
Výsledek na webu
<a href="https://www.crcpress.com/New-Trends-in-Civil-Aviation-Proceedings-of-the-19th-International-Conference/Svitek/p/book/9780815376026" target="_blank" >https://www.crcpress.com/New-Trends-in-Civil-Aviation-Proceedings-of-the-19th-International-Conference/Svitek/p/book/9780815376026</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1201/9781351238649-42" target="_blank" >10.1201/9781351238649-42</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Influence of vibration on gravitational acceleration vector measurement
Popis výsledku v původním jazyce
The paper is focused on the measurement of gravitational acceleration vector using COTS accelerometers and the influence of vibration. Determination of gravitational acceleration vector is a fundamental task of all inertial navigation systems and attitude and heading reference systems. Utilization of COTS acceleration sensors is a domain especially of small unmanned aerial systems. Measurement accuracy is dependent on ambient conditions, i.e. temperature and vibrations. The paper is aimed at the evaluation of the influence of vibration on the measurement accuracy. This effect was verified experimentally using laboratory vibration generator and several 6DOF sensors. These sensors were exposed to vibrations of various frequencies, while the accuracy of gravitational acceleration vector measurement was observed. As a device under test two different categories of sensors were used—general purpose accelerometers and accelerometers intended for drones.
Název v anglickém jazyce
Influence of vibration on gravitational acceleration vector measurement
Popis výsledku anglicky
The paper is focused on the measurement of gravitational acceleration vector using COTS accelerometers and the influence of vibration. Determination of gravitational acceleration vector is a fundamental task of all inertial navigation systems and attitude and heading reference systems. Utilization of COTS acceleration sensors is a domain especially of small unmanned aerial systems. Measurement accuracy is dependent on ambient conditions, i.e. temperature and vibrations. The paper is aimed at the evaluation of the influence of vibration on the measurement accuracy. This effect was verified experimentally using laboratory vibration generator and several 6DOF sensors. These sensors were exposed to vibrations of various frequencies, while the accuracy of gravitational acceleration vector measurement was observed. As a device under test two different categories of sensors were used—general purpose accelerometers and accelerometers intended for drones.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
—
OECD FORD obor
20201 - Electrical and electronic engineering
Návaznosti výsledku
Projekt
—
Návaznosti
S - Specificky vyzkum na vysokych skolach<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2018
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
New Trends in Civil Aviation - Proceedings of the 19th International Conference on New Trends in Civil Aviation, NTCA 2017
ISBN
978-0-8153-7602-6
ISSN
—
e-ISSN
—
Počet stran výsledku
6
Strana od-do
249-254
Název nakladatele
CRC Press/Balkema
Místo vydání
Praha
Místo konání akce
Prague, the Czech Republic
Datum konání akce
7. 12. 2017
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
—