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dc.contributor.authorKao, C. F.en_US
dc.contributor.authorChen, T. L.en_US
dc.date.accessioned2014-12-08T15:11:21Z-
dc.date.available2014-12-08T15:11:21Z-
dc.date.issued2008-06-15en_US
dc.identifier.issn0924-4247en_US
dc.identifier.urihttp://dx.doi.org/10.1016/j.sna.2008.02.008en_US
dc.identifier.urihttp://hdl.handle.net/11536/8715-
dc.description.abstractConventionally, there are two ways to determine the orientation angles of an object. One uses 3-axis accelerometers and 3-axis magnetic sensors, while the other one uses additional 3-axis gyroscopes to achieve a higher sensing accuracy than the first one. This paper presents a novel orientation estimation system that uses seven single-axis linear accelerometers and 3-axis magnetic sensors. These seven linear accelerometers are deployed in a way to form a "coplanar" gyro-free inertial measurement unit (IMU). As such, they can perform the integrated measurements of gravity force and angular velocity for the subsequent sensor fusion algorithms. With the information of the angular velocity, this novel design achieves a comparable performance with the one that includes 3-axis gyroscopes. The analysis of the system observability indicates that the angular velocity measurements can improve the observability of the angle estimation under certain circumstances. This result suggests the possibility of using fewer sensors in an orientation estimation system. Simulation results indicate that the proposed design achieve a sensing accuracy of 0.11 degrees, 0.09 degrees, and 0.2 degrees for the roll, pitch, and yaw angle; this leads to the improvement of 540%, 632%, and 754% over the one that does not include the measurement of the angular velocity. (C) 2008 Elsevier B.V. All rights reserved.en_US
dc.language.isoen_USen_US
dc.subjectaccelerometersen_US
dc.subjectgyroscopesen_US
dc.subjectgyro-free inertial measurement uniten_US
dc.subjectEuler anglesen_US
dc.subjectsensor fusionen_US
dc.subjectsystem observabilityen_US
dc.titleDesign and analysis of an orientation estimation system using coplanar gyro-free inertial measurement unit and magnetic sensorsen_US
dc.typeArticleen_US
dc.identifier.doi10.1016/j.sna.2008.02.008en_US
dc.identifier.journalSENSORS AND ACTUATORS A-PHYSICALen_US
dc.citation.volume144en_US
dc.citation.issue2en_US
dc.citation.spage251en_US
dc.citation.epage262en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000256896700003-
dc.citation.woscount12-
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