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
Link To Document :
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