Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System
Abo el-Soud, M., el-Dakiky, M., el-Khayat, M. (2003). Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System. EKB Journal Management System, 10(10th International Conference On Aerospace Sciences & Aviation Technology), 805-817. doi: 10.21608/asat.2013.24701
M Samy Abo el-Soud; M. el-Dakiky; M. el-Khayat. "Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System". EKB Journal Management System, 10, 10th International Conference On Aerospace Sciences & Aviation Technology, 2003, 805-817. doi: 10.21608/asat.2013.24701
Abo el-Soud, M., el-Dakiky, M., el-Khayat, M. (2003). 'Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System', EKB Journal Management System, 10(10th International Conference On Aerospace Sciences & Aviation Technology), pp. 805-817. doi: 10.21608/asat.2013.24701
Abo el-Soud, M., el-Dakiky, M., el-Khayat, M. Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System. EKB Journal Management System, 2003; 10(10th International Conference On Aerospace Sciences & Aviation Technology): 805-817. doi: 10.21608/asat.2013.24701

Improving The Positioning Accuracy of High speed Aircraft By using Integrated GPS/INS Navigation System

International Conference on Aerospace Sciences and Aviation Technology
Article 54, Volume 10, 10th International Conference On Aerospace Sciences & Aviation Technology, May 2003, Page 805-817  XML PDF (2.23 MB)
Document Type: Original Article
DOI: 10.21608/asat.2013.24701
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Authors
M Samy Abo el-Soud; M. el-Dakiky; M. el-Khayat
Electrical Engineering Department, Faculty of Engineering At Port Said, Suez Canal University.
Abstract
Military avionics navigation systems are constantly demanding for exploding system performance and minimizing system size. They require higher accuracy, reliability, and robustness against jamming. This drives the system-integrators towards a generation based upon satellite navigation (GPS) and inertial navigation system (INS). This paper presents the solution of GPS navigation equations operating in a stand-alone configuration in a general environment. On the other hand, the solution of INS equations operating in a stand-alone configuration in the same environment. And finally, the solution of integrated GPS/INS navigation system, which will provide improvements in navigation performance are presented.
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