In this study, the integration of two navigation systems Air Data System (ADS) and Global Positioning System (GPS) was aimed. ADS is a widely used navigation system which measures static and total air pressure and the air temperature. ADS has high sampling frequency and poor accuracy, on the other hand, another navigation system GPS has high accuracy compared to ADS but lower sampling frequency.Kalman Filter is used to integrate and minimize the errors of the two navigation systems. By this integration a navigation system with high sampling frequency and high accuracy is aimed. Another object is to calculate the wind speed with high accuracy.
References
[1]
R. M. Rogers, “Applied Mathematics in Integrated Nnavigation Systems,” American Institute of Aeronautics and Astronautics, 2000.
[2]
W. Zuo and F. Song, “Autonomous Navigation Scheme for Small Satellites GPS/Geomagnetics Integration,” Mechanical Engineering Institute, Part G: Aerospace Engineering journal Vol. 214, No. 4, 2000, pp. 207-215.
[3]
Zh. Feizhou, , et al. “Application of GPS/INU/DM Integrated Position and Navigation Technologies in Smart Systems,” Beijing Hangkong Hangtian Daxue Xue- bao/Journal of Beijing University of Aeronautics and Astronautics, Vol. 26, No. 3, 2000, pp. 299-302.
[4]
R. Zaibel, et al., “Conference on Lasers and Electro-Optics Europe—Technical Digest 2000,” IEEE Pits- cataway, NJ, USA, 00TH8505. p. 66.
[5]
D. Brinkman, “Jane’s Avionics,” Jane’s Information Group. UK, 1999.
[6]
R. P. G. Collinson , “Introduction to Avionics,”London : Chapman & Hall, 1996.
[7]
Gri?in, P. Yu., Kazarinov and M.Yu, “Fault Tolerant Dynamical Systems,” Radio i svyaz, Moskow，Russian , 1985.
[8]
M. Kayton and W. R. Fried, “Avionics and Navigation Systems,” John Wiley & Sons Ltd., New York, 1997.
doi:10.1002/9780470172704
[9]
D. McLean, “Automatic Flight Control Systems,” Prentice Hall Inc. Englewood Cliffs, N. J. , 1990.
[10]
Ch. Hajiyev, “Radio Navigation, ” Istanbul : ITU, 1999.
