Development of a Low-cost Inertial Navigation Unit and a Testing of Filters for Inertial Navigation
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F09%3A00153607" target="_blank" >RIV/68407700:21230/09:00153607 - isvavai.cz</a>
Výsledek na webu
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DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Development of a Low-cost Inertial Navigation Unit and a Testing of Filters for Inertial Navigation
Popis výsledku v původním jazyce
This document concerns the development of a low-cost inertial navigation unit. This includes a testing of inertial sensors, implementation of a navigation algorithm (enhanced by sensor output data de-noising) and the design of a filter for sensors outputdata fusion based on Kalman filtering. Over the last decades there was a remarkable increase in demand for low-cost inertial navigation systems (INS) to serve as car navigation, personal navigation or navigation for unmanned aerial vehicles and aviationin general. A rapid technological advance in the precision and reliability of micro-electro-mechanical sensors is a promising key factor in the area of low-cost INS. Although the precision and reliability increases, the low-cost sensors still exhibit large long-term errors, giving the opportunity to seek for solutions. Such a solution was sought by introducing innovations into the hardware concept [1] as well as into the conventional signal processing algorithms.
Název v anglickém jazyce
Development of a Low-cost Inertial Navigation Unit and a Testing of Filters for Inertial Navigation
Popis výsledku anglicky
This document concerns the development of a low-cost inertial navigation unit. This includes a testing of inertial sensors, implementation of a navigation algorithm (enhanced by sensor output data de-noising) and the design of a filter for sensors outputdata fusion based on Kalman filtering. Over the last decades there was a remarkable increase in demand for low-cost inertial navigation systems (INS) to serve as car navigation, personal navigation or navigation for unmanned aerial vehicles and aviationin general. A rapid technological advance in the precision and reliability of micro-electro-mechanical sensors is a promising key factor in the area of low-cost INS. Although the precision and reliability increases, the low-cost sensors still exhibit large long-term errors, giving the opportunity to seek for solutions. Such a solution was sought by introducing innovations into the hardware concept [1] as well as into the conventional signal processing algorithms.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
JU - Aeronautika, aerodynamika, letadla
OECD FORD obor
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Návaznosti výsledku
Projekt
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Návaznosti
Z - Vyzkumny zamer (s odkazem do CEZ)
Ostatní
Rok uplatnění
2009
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
Workshop 09
ISBN
978-80-01-04286-1
ISSN
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e-ISSN
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Počet stran výsledku
2
Strana od-do
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Název nakladatele
ČVUT
Místo vydání
Praha
Místo konání akce
Praha
Datum konání akce
16. 2. 2009
Typ akce podle státní příslušnosti
EUR - Evropská akce
Kód UT WoS článku
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