Design of an Inertial Reference Unit with Mixed Gravitaional and Magnetic Correction of Gyroscopic Drift

Result code in 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>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Design of an Inertial Reference Unit with Mixed Gravitaional and Magnetic Correction of Gyroscopic Drift
Original language description
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.
Czech name
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Czech description
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Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Transport Means 2010 (Proceedings of the 14th International Conference)
ISBN
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ISSN
1822-296X
e-ISSN
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Number of pages
4
Pages from-to
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Publisher name
Kaunas University of Technology
Place of publication
Litevská republika
Event location
Kaunas
Event date
Jan 1, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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