DocumentCode :
3610916
Title :
Determination of an Attitude Estimation Unit with Inertial Sensors Modeled by Allan Variance
Author :
Carrasco, M.M. ; da Silva, A.L.
Author_Institution :
Univ. Fed. do ABC, Santo André, Brazil
Volume :
13
Issue :
8
fYear :
2015
Firstpage :
2500
Lastpage :
2505
Abstract :
This article deal with the identification, by Allan variance, of the associated noises in signals from microelectromechanical (MEMS) inertial sensors accelerometer and gyroscope, whose data are used in attitude calculus of rigid bodies. An Arduino Uno microprocessor was used to collect sensor data while the software MATLAB was applied for post processing. The results were used for building error models to improve simulators and also to refine attitude estimation with Kalman filter.
Keywords :
accelerometers; attitude measurement; gyroscopes; inertial navigation; mathematics computing; microprocessor chips; microsensors; Allan variance; Arduino Uno microprocessor; Kalman filter; MATLAB; accelerometer; attitude estimation unit; gyroscope; microelectromechanical inertial sensors; Estimation; Kalman filters; MATLAB; Mathematical model; Micromechanical devices; Position measurement; Sensors; Allan Variance; Attitude Determination; Attitude Sensors; Inertial Navigation;
fLanguage :
English
Journal_Title :
Latin America Transactions, IEEE (Revista IEEE America Latina)
Publisher :
ieee
ISSN :
1548-0992
Type :
jour
DOI :
10.1109/TLA.2015.7331904
Filename :
7331904
Link To Document :
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