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dc.contributor.authorTang, Chun
dc.contributor.otherQueen's University (Kingston, Ont.). Theses (Queen's University (Kingston, Ont.))en
dc.date2012-01-06 12:29:00.941en
dc.date2012-01-12 16:00:47.983en
dc.date2012-01-13 14:46:45.44en
dc.date.accessioned2012-01-13T20:11:32Z
dc.date.available2012-01-13T20:11:32Z
dc.date.issued2012-01-13
dc.identifier.urihttp://hdl.handle.net/1974/6956
dc.descriptionThesis (Master, Electrical & Computer Engineering) -- Queen's University, 2012-01-13 14:46:45.44en
dc.description.abstractWireless sensor network technology has now been widely adopted. In many applications, distributed sensor nodes collect data at different locations and the location information of each node is required. The Global Positioning System is commonly used to identify the location of the nodes in such networks. Although GPS localization has consistent long-term accuracy, it is limited by the inherent dependency on a direct line of sight to 4 or more external satellites. The increasing demand for an embedded system providing reliable navigation solutions regardless of its operational environment has motivated investigations into the use of integrated systems that combine inertial sensors with GPS receivers. This research proposes a hardware architecture for location-based wireless sensor networks. In this architecture, each sensor node consists of a GPS receiver, a reduced set of low cost micro-electro-mechanical-system-based INS and a wireless transceiver. Sensor nodes in WSN are often equipped with irreplaceable batteries, which makes the power consumption crucial. To reduce the energy consumption, a microcontroller is used to control the power supply. Besides, a motion detection scheme is proposed by taking advantage of the ultra low-power wake-up function of the microcontroller. A low-power featured digital signal processor is used to accomplish the navigation computation using the Kalman filter for GPS/INS data fusion. Non-Holonomic Constraints derived velocity updates are applied to reduce the position errors. Field tests are conducted to verify the real-time performance of the proposed system with a positioning update rate of 20 Hz. The first test shows that the 2D INS/GPS integration can maintain the average system position error within 5 meters during a 60-second GPS outage. The second test used low cost inertial sensors. The average position error was 10.17 meters during a 20-second outage. The largest RMS value of position errors among these outages was within 14.5 meters. Furthermore, additional accuracy improvements of approximately 1.4 meters were achieved by utilizing NHC during GPS outages. The third test shows that the average error during a 30-second outage is approximately 20.6 meters for the on-foot scenario and 26.7 meters for the in-vehicle scenario.en_US
dc.languageenen
dc.language.isoenen_US
dc.relation.ispartofseriesCanadian thesesen
dc.rightsThis publication is made available by the authority of the copyright owner solely for the purpose of private study and research and may not be copied or reproduced except as permitted by the copyright laws without written authority from the copyright owner.en
dc.subjectEmbedded Systemsen_US
dc.subjectGPS/INS Integrationen_US
dc.subjectWSNen_US
dc.subjectDSPen_US
dc.titleA HARDWARE ARCHITECTURE FOR GPS/INS-ENABLED WIRELESS SENSOR NETWORKSen_US
dc.typeThesisen_US
dc.description.degreeMasteren
dc.contributor.supervisorIbnkahla, Mohameden
dc.contributor.departmentElectrical and Computer Engineeringen


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