Design of an Inertial Reference Unit with Mixed Gravitaional and Magnetic Correction of Gyroscopic Drift
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F10%3A00423180" target="_blank" >RIV/60162694:G43__/10:00423180 - 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
Design of an Inertial Reference Unit with Mixed Gravitaional and Magnetic Correction of Gyroscopic Drift
Popis výsledku v původním jazyce
The Department of Aerospace Electrical Systems (Faculty of Military Technology, University of Defence) is traditionally interested in the field of development and design of the aircraft instruments. The developed Inertial Reference Unit (IRU) was originally based on the MEMS sensorial technology and designed to measure the position angles on the board of small or ultra-light aircraft, airships, unmanned aerial vehicles, but also on the board of different unmanned ground vehicles and robots. The measurement circuits of pitch and roll of the IRU were equipped only with gravitational correction, which is nevertheless sensitive to the motion acceleration. Recently it was decided to improve the precision of the IRU by means of mixed gravitational and magnetic correction of the gyroscopic drift, as the measurement of geomagnetic field components is not affected by the disturbing acceleration.
Název v anglickém jazyce
Design of an Inertial Reference Unit with Mixed Gravitaional and Magnetic Correction of Gyroscopic Drift
Popis výsledku anglicky
The Department of Aerospace Electrical Systems (Faculty of Military Technology, University of Defence) is traditionally interested in the field of development and design of the aircraft instruments. The developed Inertial Reference Unit (IRU) was originally based on the MEMS sensorial technology and designed to measure the position angles on the board of small or ultra-light aircraft, airships, unmanned aerial vehicles, but also on the board of different unmanned ground vehicles and robots. The measurement circuits of pitch and roll of the IRU were equipped only with gravitational correction, which is nevertheless sensitive to the motion acceleration. Recently it was decided to improve the precision of the IRU by means of mixed gravitational and magnetic correction of the gyroscopic drift, as the measurement of geomagnetic field components is not affected by the disturbing acceleration.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
KA - Vojenství
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
2010
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
Transport Means 2010 (Proceedings of the 14th International Conference)
ISBN
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ISSN
1822-296X
e-ISSN
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Počet stran výsledku
4
Strana od-do
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Název nakladatele
Kaunas University of Technology
Místo vydání
Litevská republika
Místo konání akce
Kaunas
Datum konání akce
1. 1. 2010
Typ akce podle státní příslušnosti
EUR - Evropská akce
Kód UT WoS článku
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