Integration of INS with TACAN and altimeter

• Autorzy: Kaniewski, P.
• Języki publikacji: EN

Abstrakty

EN

The paper presents a design of integrated positioning system for aircraft. The system is composed of INS, TACAN and altimeter. It employs a Complementary Extended Kalman Filter, estimating INS position, velocity and attitude errors. Chosen simulation results, comparing accuracy of INS, TACAN/ALT subsystem and integrated INS/TACAN/ALT positioning system are included.

Słowa kluczowe

EN

INS; TACAN; altimeter; EKF; integrated positioning system

• Czasopismo: Molecular and Quantum Acoustics
• Rocznik: 2007
• Tom: Vol. 28
• Strony: 165-177
• Opis fizyczny: Bibliogr. 13 poz., rys.

Twórcy

autor

Kaniewski, P.

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

Bibliografia

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• 5. M. Kayton, W.R. Fried, Avionics Navigation Systems, John Wiley & Sons, USA, 1997.
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• 7. O. Salychev, Inertial Systems in Navigation and Geophysics, Bauman MSTU Press, Russia, 1998.
• 8. D.H. Titterton, J.L. Weston, Strapdown Inertial Navigation Technology - 2nd Edition, American Institute of Aeronautics and Astronautics, 2004.
• 9. A. Kawalec, W. Komorniczak, Molecular and Quantum Acoustics 26, 159-164 (2005).
• 10. A. Kawalec, A. Pieniezny, Molecular and Quantum Acoustics 26, 175-182 (2005).
• 11. A. Kawalec, Molecular and Quantum Acoustics 26, 129-148 (2005).
• 12. U.S. Department of Transportation, U.S. Department of Defense, 2001 Federal Radionavigation Plan, DOT-VNTSC-RSPA-01-3/DoD-4650.5, USA, 2001.
• 13. U.S. Department of Transportation, U.S. Department of Defense, 2001 Federal Radionavigation Systems, DOT-VNTSC-RSPA-01-3.1/DOD-4650.5, USA, 2001