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Typical Errors, Accuracy Classes and Currently Expected Accuracy of Inertial Measurement Units
Author(s) -
Attila Varga,
Tamás Jancsó,
Péter Udvardy
Publication year - 2021
Publication title -
acta avionica
Language(s) - English
Resource type - Journals
eISSN - 1339-9853
pISSN - 1335-9479
DOI - 10.35116/aa.2021.0002
Subject(s) - units of measurement , gyroscope , accelerometer , inertial measurement unit , inertial frame of reference , accuracy and precision , range (aeronautics) , computer science , inertial navigation system , measurement uncertainty , aviation , engineering , aerospace engineering , artificial intelligence , mathematics , physics , statistics , quantum mechanics , operating system
Inertial measurement units can nowadays be found in a wide range of applications, from consumer electronics to precision surveying systems requiring high accuracy. IMUs are also widely used in aviation, especially for UAVs. The gyroscopes and accelerometers in IMUs have specific operating modes that would result in specific errors typical of such instruments. This paper reviews the typical errors of IMUs and the accuracy that can be achieved with these instruments today in each application area.

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