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