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http://dx.doi.org/10.5139/JKSAS.2008.36.5.462

Research on the Method of a Composite Navigation Algorithm Using Aircraft Recorder Data  

Kim, Jae-Hyung (대한항공 한국항공기술연구원)
Lyou, Joon (충남대학교 전자공학과)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.36, no.5, 2008 , pp. 462-471 More about this Journal
Abstract
Flight recoder is used to analyze the accident factors and prevent the accident. In the analysis of the flight recorder, the most important factor is how to estimate the precise location of the flight. Traditional aviation navigation is based on stable sensors such as DME and VOR. In order to enhance the precision of the location estimation, the integrated navigation algorithm is designed to incorporate DME, Air data sensors and INS(Inertial Navigation System). The results demonstrate that the proposed algorithm can achieve better accuracy, comparing with the traditional navigation schemes, in flight location estimation.
Keywords
QAR; DME; Air Data; INS; GPS; Composite Navigation;
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  • Reference
1 Jennings, Randle G., "Avionics Standard Communication Bus-Its Implementation And Usage", Proceedings of the IEEE/AIAA 7th Digital Avionics Systems Conference, Institute of Electronical and Electronics Engineers, New Yorkm NY, 1986
2 L. Hogle, K. Markin. and S. Toth, "Evaluation of various navigation system concepts", FAA Rep. FAA-EM-82-1s. Mar. 1982
3 Robert B. Merrick, "A simplified kalman estimation for an aircraft landing display", J. Aircraft 1978
4 Gebre-Egziabher, D. Powell, J.D. Enge, P., "A DME based area navigation systems for GPS/WAAS interferencemitigation in general aviation applications", Position Location and Navigation Symposium, IEEE 2000
5 Daniel Murdin and Predrag Pucar, "Integrated INS and DME navigation wit Fault Detection, in the SAAB Gripprn Aircraft", Proceedings of the 24th JSDE Symposium, Anahiem, CA. JSDE, 1998
6 H.K. Lee, J.G. Lee, C.G. Park and Y.K. Rho, "Modeling quaternion errors in SDINS: computer frame approach", IEEE Transactions on Aerospace and Electronic Systems, Vol. 34, No. 1, pp. 289-299, 1988   DOI   ScienceOn
7 Johdnsen H., "A SURVEY OF GENERAL COVERAGE NAVAIDS FOR V/STOL AIRCRAFT A VOR/DME ERROR MODEL", NASA CR-1588, 1970
8 Demoz, Gebre-Egziabher Design and Performance Analysis of a Low-Cost Aided Dead Reckoning Navigator, A Dissertation submitted to the Department of Aeronautics and Astronautics and the committee on graduate studies of Stanford University, Stanford University 2004
9 Myron Kayton and Walter R. Fried., "Avionics Navigation Systems", John Wiley and Sons, Inc., New York, New York, 2nd edition, 1997
10 Albert Helfrick, "Principles of Avionics Data Buses", Avionics Commuication Inc., 3th edition, 2004
11 R. Dorobantu, C. Gerlach, "Investigation of a navigation-Grade RLG SIMU type iNAV-RQH", Schriftenreihe IAPG/FESG (in print), Technische Universitat Munchen, 2004
12 A. Weinred and I.Y. Bar-Itzhack, "The Psi-Angle Error Equation in Strapdown Inertial Navigation Systems", Aerospace and Electronic Systems, IEEE Transactions on Aerospace and Electronic Systems, Vol. 14, No.3, pp. 539-542, 1978   DOI   ScienceOn