Thanks to their enormous versatility, inertial platforms (IMUs) based on MEMS (Micro Electromechanical Systems) technology are now widely used in various fields. The strength of MEMS technology is the ability to miniaturize entire sensors within very small volumes. Inertial units play an important role in tracking an object in space and, therefore, in all the fields attached to it: self-driving vehicles, aerospace, and many others. The estimation of orientation in space is obtained using triaxial gyroscopes, accelerometers, and magnetometers. Raw data, output from inertial sensors, are commonly processed using different sensor fusion techniques and, on the base of their structure, may vary their sensitivity with respect to the acquired signals. A key aspect to consider in highly complex systems like these is noise components affecting measurements. The aim of the paper is to analyze the different noise components affecting low-cost IMU platforms to guide the selection of the particular sensor fusion technique to be employed.

Analysis of noise contributions in low-cost IMUs through Allan's variance / Catelani M.; Ciani L.; Patrizi G.; Singuaroli R.; Carratu M.; Sommella P.; Pietrosanto A.. - ELETTRONICO. - (2023), pp. 258-262. (Intervento presentato al convegno 10th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2023 tenutosi a Milano (Italy) nel 9 June 2023 through 21 June 2023) [10.1109/MetroAeroSpace57412.2023.10189971].

Analysis of noise contributions in low-cost IMUs through Allan's variance

Catelani M.;Ciani L.;Patrizi G.;Singuaroli R.;
2023

Abstract

Thanks to their enormous versatility, inertial platforms (IMUs) based on MEMS (Micro Electromechanical Systems) technology are now widely used in various fields. The strength of MEMS technology is the ability to miniaturize entire sensors within very small volumes. Inertial units play an important role in tracking an object in space and, therefore, in all the fields attached to it: self-driving vehicles, aerospace, and many others. The estimation of orientation in space is obtained using triaxial gyroscopes, accelerometers, and magnetometers. Raw data, output from inertial sensors, are commonly processed using different sensor fusion techniques and, on the base of their structure, may vary their sensitivity with respect to the acquired signals. A key aspect to consider in highly complex systems like these is noise components affecting measurements. The aim of the paper is to analyze the different noise components affecting low-cost IMU platforms to guide the selection of the particular sensor fusion technique to be employed.
2023
2023 IEEE 10th International Workshop on Metrology for AeroSpace, MetroAeroSpace 2023 - Proceedings
10th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2023
Milano (Italy)
9 June 2023 through 21 June 2023
Goal 9: Industry, Innovation, and Infrastructure
Catelani M.; Ciani L.; Patrizi G.; Singuaroli R.; Carratu M.; Sommella P.; Pietrosanto A.
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Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/1341871
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