DocumentCode
2015382
Title
An Attitude and Heading Reference System (AHRS) based in a dual filter
Author
Munguia, Rodrigo ; Grau, Antoni
Author_Institution
Dept. of Autom. Control, UPC, Barcelona, Spain
fYear
2011
fDate
5-9 Sept. 2011
Firstpage
1
Lastpage
8
Abstract
This paper describes the design, analysis, and experimental results of an Attitude and Heading System based on a Dual Kalman Filtering technique. The presented scheme is suitable for implementation using low cost sensors. Attitude determination systems are essential for real time vehicle navigation, guidance and control applications. When low cost sensors are used, efficient and robust algorithms become necessary for an acceptable performance. For the proposed approach, a low cost Inertial Measurement Unit (IMU), formed by 3-axis gyroscope, 3-axis accelerometer, and 3-axis magnetometer, provides the input measurements. Experimental results with real data show that the proposed algorithm is able to maintain an accurate and drift-free attitude and heading estimation.
Keywords
Kalman filters; accelerometers; aircraft instrumentation; attitude measurement; gyroscopes; inertial navigation; magnetometers; 3-axis accelerometer; 3-axis gyroscope; 3-axis magnetometer; attitude determination system; attitude reference system; dual Kalman filtering technique; heading reference system; inertial measurement unit; real time vehicle control; real time vehicle guidance; real time vehicle navigation; sensor; Accelerometers; Covariance matrix; Estimation; Kinematics; Magnetometers; Quaternions; Sensors;
fLanguage
English
Publisher
ieee
Conference_Titel
Emerging Technologies & Factory Automation (ETFA), 2011 IEEE 16th Conference on
Conference_Location
Toulouse
ISSN
1946-0740
Print_ISBN
978-1-4577-0017-0
Electronic_ISBN
1946-0740
Type
conf
DOI
10.1109/ETFA.2011.6059089
Filename
6059089
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