DocumentCode :
3613031
Title :
Attitude estimation and sensor identification utilizing nonlinear filters based on a low-cost MEMS magnetometer and sun sensor
Author :
Teshnizi, Masoud Mirzaei ; Shirazi, Abolfazl
Author_Institution :
Sharif Univ. of Technol., Tehran, Iran
Volume :
30
Issue :
12
fYear :
2015
fDate :
12/1/2015 12:00:00 AM
Firstpage :
20
Lastpage :
33
Abstract :
A combination of low-cost micro-electoro-mechanical sensors (MEMSs) and nonlinear attitude estimation algorithm techniques can provide an inexpensive and accurate system for navigation and attitude determination. The features of MEMSs are their light weight and small size; hence, the MEMSs have found significant attention in low-cost navigation and control systems. A common disadvantage of these sensors is the significant errors that accompany the corresponding measurements. The accuracy obtained using MEMSs depends on a number of factors, such as scale factor, bias, and random noise corrections. However, these low-cost sensors suffer from large noise and errors, making calibration and error identification of critical importance.
Keywords :
attitude measurement; calibration; magnetometers; microsensors; navigation; nonlinear filters; sun sensors; MEMS magnetometer; attitude determination; calibration; control system; error identification; microelectromechanical sensor; navigation; nonlinear attitude estimation algorithm; nonlinear filter; random noise correction; scale factor; sensor identification; sun sensor; Electromechanical devices; Magnetic field measurement; Magnetometers; Microelectoromechanical sensors; Nonlinear attitude estimation; Quaternions; Satellites; Sensors;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/MAES.2015.150069
Filename :
7381287
Link To Document :
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