@inproceedings{SisLab88,
       booktitle = {4th International Conference on Communications and Electronics (ICCE 2012)},
           title = {Application of Extended and Linear Kalman Filters for an Integrated Navigation System},
          author = {Tan Tran Duc},
            year = {2012},
             url = {https://eprints.uet.vnu.edu.vn/eprints/id/eprint/88/},
        abstract = {Inertial 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.}
}