Integration of Low-cost Inertial Navigation Unit with Secondary Navigation Systems

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F10%3A00165631" target="_blank" >RIV/68407700:21230/10:00165631 - 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
Integration of Low-cost Inertial Navigation Unit with Secondary Navigation Systems
Original language description
This paper concerns the development of a system that consists of a low-cost inertial navigation unit and the 3-axial magnetometer, which will be used as a secondary navigation system. The development includes measuring and testing of inertial sensors anda magnetometer, and the calibration of navigation sensors used for the following data fusion via Kalman Filter. As a primary system for integration the Inertial Navigation System (INS) will be used. The INS consists of 3-axial accelerometer and 3-axialangular rate sensor. Tri-axial magnetometer will be used as the secondary system. All of these sensor outputs are disturbed by errors which are a decisive factor for their implementation and verification of their performance. The deterministic sensor error analyses of accelerometers, angular rate sensors, and magnetometers are presented.
Czech name
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Czech description
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Project
<a href="/en/project/GD102%2F09%2FH082" target="_blank" >GD102/09/H082: Sensors and intelligent sensor systems</a><br>
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)<br>V - Vyzkumna aktivita podporovana z jinych verejnych zdroju

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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