DocumentCode
3211714
Title
Nonlinear observer for real-time attitude estimation
Author
Guerrero-Sánchez, W.F. ; Guerrero-Castellanos, J.F. ; Juárez-Salazar, R. ; Salmerón-Quiroz, B.B.
Author_Institution
Fac. de Cienc. Fisico-Mat., Benemerita Univ. Autonoma de Puebla (BUAP), Puebla, Mexico
fYear
2009
fDate
10-13 Jan. 2009
Firstpage
1
Lastpage
6
Abstract
This paper deals with the attitude estimation of a rigid body equipped with a module of GAM sensors (rate gyros, accelerometers and magnetometers). A quaternion-based nonlinear observer is proposed in order to fuse all information sources and to obtain an accurate estimation of the attitude. It is shown that the error dynamics can break up into two passive subsystems connected in ¿feedback¿. This property is a first and crucial result that could be used to show that the error dynamics is input-to-state stable (ISS) when the measurement disturbance is seen as an input and the error state as the state. The effectiveness of the observer is confirmed in a real-time application.
Keywords
accelerometers; aircraft; attitude measurement; magnetometers; observers; real-time systems; GAM sensors; accelerometers; error dynamics; input-to-state stable; magnetometers; quaternion-based nonlinear observer; rate gyros; realtime attitude estimation; Accelerometers; Fuses; Gravity; Magnetic sensors; Magnetometers; Micromechanical devices; Observers; Quaternions; Robot kinematics; Robot sensing systems; Aerial Robotics; Attitude; MEMS sensors; Nonlinear Observer; SVD;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical Engineering, Computing Science and Automatic Control,CCE,2009 6th International Conference on
Conference_Location
Toluca
Print_ISBN
978-1-4244-4688-9
Electronic_ISBN
978-1-4244-4689-6
Type
conf
DOI
10.1109/ICEEE.2009.5393399
Filename
5393399
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