<> "The repository administrator has not yet configured an RDF license."^^ . <> . . . "Designing Kalman filters for integration of inertial navigation system and global positioning system"^^ . "Due to the strong growth of MEMS technology, the Inertial Navigation System (INS) is wi del y applie d to navi gati on and g ui dan ce of aircraft movements. However, there are existing errors in the accelerometer and gyroscope signals that cause unacceptable drifts. To minimize these effect s on the INS syste m, a GPS is u sually employed simultaneously with an INS in order to increase the dimension of the system; the desired parameters are estimated by the Kalman filtering technique applied to the enlarged system. In this paper, we prese nt a st ruct ure con sistin g of a Kal man Filter (KF) of whi ch t he input is the difference between the noisy INS output and the noisy GPS output; the output of KF is finally introduced into the unaided INS system. In this structure, INS errors are compensated by a feedforward and a feedback loop. The overall performance of the system is analyzed by simulation; and results show that this technique substantially improves the quality of the navigation and guidance systems."^^ . "2006" . . . . . . . . . . . . . . . . . . . . "Thang Long"^^ . "Nguyen"^^ . "Thang Long Nguyen"^^ . . "Phu Thuy"^^ . "Nguyen"^^ . "Phu Thuy Nguyen"^^ . . "Huu Tue"^^ . "Huynh"^^ . "Huu Tue Huynh"^^ . . "Duc Tan"^^ . "Tran"^^ . "Duc Tan Tran"^^ . . "Van Chuc"^^ . "Nguyen"^^ . "Van Chuc Nguyen"^^ . . . . "REV: the 10th biennial Vietnam Conference on Radio & Electronics"^^ . . . . . "Hanoi, Vietnam"^^ . . . . . . "Designing Kalman filters for integration of inertial navigation system and global positioning system (PDF)"^^ . . . "paper2_GPS_INS.pdf"^^ . . "HTML Summary of #1732 \n\nDesigning Kalman filters for integration of inertial navigation system and global positioning system\n\n" . "text/html" . . . "Electronics and Communications"@en . . . "Electronics and Computer Engineering"@en . .