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