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dc.contributor.authorTran, Duc Tan-
dc.date.accessioned2016-08-11T07:57:35Z-
dc.date.available2016-08-11T07:57:35Z-
dc.date.issued2012-
dc.identifier.urihttp://repository.vnu.edu.vn/handle/VNU_123/13036-
dc.description.abstractInertial navigation, integrated with other navigation aids such as Global Positioning System (GPS), has gained significance in recent years. The integrated navigation system can be used to determine attitude, velocity and position of the moving objects. This paper presents an approach to designing an INS/GPS based navigation system using a combination of an Extended Kalman Filter (EKF) and a Linear Kalman Filter (LKF). These include a first-stage eight-state EKF for the GPS data and a second-stage eight-state LKF for the INS/GPS integration. The advantage of this design is that we can utilize the simplicity of the LKF but keep the high performance of the EKF. Comparison and analysis of the new scheme is carried out, and it is demonstrated that the proposed configuration is useful technique.en_US
dc.language.isoenen_US
dc.publisherĐHCNen_US
dc.subjectIntegrated Navigation Systemen_US
dc.subjectCommunications and Electronicsen_US
dc.titleApplication of Extended and Linear Kalman Filters for an Integrated Navigation Systemen_US
dc.typeArticleen_US
Appears in Collections:Bài đăng tạp chí (LIC)


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  • Full metadata record
    DC FieldValueLanguage
    dc.contributor.authorTran, Duc Tan-
    dc.date.accessioned2016-08-11T07:57:35Z-
    dc.date.available2016-08-11T07:57:35Z-
    dc.date.issued2012-
    dc.identifier.urihttp://repository.vnu.edu.vn/handle/VNU_123/13036-
    dc.description.abstractInertial navigation, integrated with other navigation aids such as Global Positioning System (GPS), has gained significance in recent years. The integrated navigation system can be used to determine attitude, velocity and position of the moving objects. This paper presents an approach to designing an INS/GPS based navigation system using a combination of an Extended Kalman Filter (EKF) and a Linear Kalman Filter (LKF). These include a first-stage eight-state EKF for the GPS data and a second-stage eight-state LKF for the INS/GPS integration. The advantage of this design is that we can utilize the simplicity of the LKF but keep the high performance of the EKF. Comparison and analysis of the new scheme is carried out, and it is demonstrated that the proposed configuration is useful technique.en_US
    dc.language.isoenen_US
    dc.publisherĐHCNen_US
    dc.subjectIntegrated Navigation Systemen_US
    dc.subjectCommunications and Electronicsen_US
    dc.titleApplication of Extended and Linear Kalman Filters for an Integrated Navigation Systemen_US
    dc.typeArticleen_US
    Appears in Collections:Bài đăng tạp chí (LIC)


  • paper.PDF
    • Size : 822,78 kB

    • Format : Adobe PDF

    • View : 
    • Download :