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2008 | 114 | 6A | A-133-A-138
Article title

Closed-Loop INS/TACAN/ALT Positioning System

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Languages of publication
EN
Abstracts
EN
The paper presents a design of aircraft integrated positioning system, composed of INS, TACAN and altimeter (ALT). This paper describes a modified, closed-loop version of INS/TACAN/ALT system and compares it to the previous design. The system is integrated according to the scheme of compensation with feed-backward INS correction and it employs a complementary extended Kalman filter. The paper includes chosen results of simulations obtained for the open-loop and closed-loop INS/TACAN/ALT systems and discusses advantages of the new design.
Keywords
Contributors
author
  • Military University of Technology, Gen. S. Kaliskiego 2, 00-908 Warsaw, Poland
References
  • 1. P. Kaniewski, Mol. Quant. Acoust. 28, 165 (2007)
  • 2. P. Kaniewski, in: ENC-GNSS 2008 - The European Navigation Conf., Toulouse (France) 2008, DVD
  • 3. R.G. Brown, P.Y.C. Hwang, Introduction to Random Signals and Applied Kalman Filtering, Wiley, USA 1997
  • 4. M.S. Grewal, L.R. Weill, A.P. Andrews, Global Positioning Systems, Inertial Navigation and Integration, Wiley, USA 2001
  • 5. M. Kayton, W.R. Fried, Avionics Navigation Systems, Wiley, USA 1997
  • 6. P. Kaniewski, Mol. Quant. Acoust. 28, 151 (2007)
  • 7. D.H. Titterton, J.L. Weston, Strapdown Inertial Navigation Technology, 2nd ed. AIAA, 2004
Document Type
Publication order reference
YADDA identifier
bwmeta1.element.bwnjournal-article-appv114n6a22kz
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