Aircraft Positioning with INS/GNSS Integrated System

• Autorzy: Kaniewski P.
• Języki publikacji: EN

Abstrakty

EN

The paper describes methods of INS/GNSS integration and rules of designing Kalman filters. An example of INS/GPS positioning system is presented. The system employs a Complementary Linearized Kalman Filter, estimating INS position, velocity and attitude errors, as well as GPS clock bias and drift. Chosen simulation results, comparing accuracy of INS, GPS and INS/GPS are included.

Słowa kluczowe

EN

INS; GNSS; GPS; Kalman filter; integrated positioning system

• Wydawca: Silesian Division of Polish Acoustical Society
• Czasopismo: Molecular and Quantum Acoustics
• Rocznik: 2006
• Tom: Vol. 27
• Strony: 149--168
• Opis fizyczny: Bibliogr. 8 poz., rys.

Twórcy

autor

Kaniewski P.

• Military University of Technology, 2, Gen. S. Kaliski St., 00-908 Warsaw, Poland,

Bibliografia

• 1.R.G. Brown, P.Y.C. Hwang, Introduction to random signals and applied Kalman filtering, John Wiley & Sons, Inc., USA, 1997.
• 2.M.S. Grewal, L.R. Weill, A.P. Andrews, Global Positioning Systems, Inertial Navigation and Integration, John Wiley & Sons, Inc., USA, 2001.
• 3.G. Minkler, J. Minkler, Theory and Application of Kalman Filtering, Magellan Book Company, USA, 1993.
• 4.P.J. Nordlund, Sequential Monte Carlo filters and integrated navigation, PhD thesis, Linkping University, Sweden, 2002.
• 5.O. Salychev, Inertial Systems in Navigation and Geophysics, Bauman MSTU Press, Russia, 1998.
• 6.Sinpyo Hong, Man Hyung Lee, Ho-Hwan Chun, Sun-Hong Kwon, J.L. Speyer, IEEE Transactions on Vehicular Technology, Vol. 54, No. 2, 731-743 (2005).
• 7.J. Spilker, B. Parkinson, Eds., Global Positioning System: Theory and Applications, Vol. I and Vol. II, American Institute of Aeronautics and Astronautics, 1996.
• 8.D.H. Titterton, J.L. Weston, Strapdown Inertial Navigation Technology - 2nd Edition, American Institute of Aeronautics and Astronautics, 2004.