2011 8th International Conference on Electrical Engineering, Computing Science and Automatic Control 2011
DOI: 10.1109/iceee.2011.6106610
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Design and implementation of an Attitude and Heading Reference System (AHRS)

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Cited by 19 publications
(7 citation statements)
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“…Apart from that, the system demonstrated dependency to methods of initialization. Adaptive Kalman filter (AKF) [6], extended Kalman filter (EKF) [7], and dual Kalman filter (DKF) methods [8] have been performed for orientation estimation with a basic model of the system. A precise stable Kalman-based AHRS was designed as an approach of the simultaneous localization and mapping (SLAM) applications by the authors of [9].…”
Section: Related Workmentioning
confidence: 99%
“…Apart from that, the system demonstrated dependency to methods of initialization. Adaptive Kalman filter (AKF) [6], extended Kalman filter (EKF) [7], and dual Kalman filter (DKF) methods [8] have been performed for orientation estimation with a basic model of the system. A precise stable Kalman-based AHRS was designed as an approach of the simultaneous localization and mapping (SLAM) applications by the authors of [9].…”
Section: Related Workmentioning
confidence: 99%
“…Fig. 3 Diagram of AHRS The basic step of AHRS could be described as in paper [6,7] USV Mathematical Model.USV mathematical model was need for control. The USV movement can be represented by the following equation [8].…”
Section: Design Of the Usv Experiments Platformmentioning
confidence: 99%
“…In order to employ a non-singular attitude representation in the estimator, MEKFs formulate the attitude as a multiplication of an estimated attitude quaternion and an error quaternion representing the deviation between the above estimates and true attitude. Due to the advantages of the non-singularity representation, the MEKF method has been applied to the design of micro attitude and heading reference system (AHRS) [19], as well as the MAV velocity and attitude estimation problem [20]. Although EKFs have been successfully applied in a number of applications, they have several disadvantages in addressing the navigation problem of MAVs.…”
Section: Related Workmentioning
confidence: 99%