Aerodynamic Derivatives Identification Using a Non-Conservative Robust Kalman Filter
![]() ![]() |
Lee, Han-Sung
(School of Electrical Engineering, Seoul National University)
Ra, Won-Sang (School of Mechanical and Control Engineering, Handong Global University) Lee, Jang-Gyu (School of Electrical Engineering, Seoul National University) Song, Yong-Kyu (School of Aerospace and Mechanical Engineering, Korea Aerospace University) Whang, Ick-Ho (Department of Guidance and Control, Agency for Defense Development) |
1 | W. S. Ra, Non conservative Robust Kalman Filtering Using Noise Corrupted Measurement Matrix, Ph.D. Dissertation, Department of Electrical and Electronic Engineering and The Graduate School of Younsei University, December 2008. |
2 | I. H. Whang, W. S. Ra, and J. Y. Ahn, "A modified weighted least squares range estimator for ASM (anti-ship missile) application," Int. Journal of Control, Automation, and Systems, 2005, 3, (3), pp. 486-492. |
3 | Robert C. Nelson, Flight Stability and Automatic Control, 2nd Ed., McGraw Hill, 1998. |
4 | Simon Haykin, Adaptive filter theory, Prentice Hall, Upper Saddle River, New Jersey 070458, 2002. |
5 | A. Gelb (ed.), Applied optimal estimation, Cambridge, MA: MIT press, 1974. |
6 | F. L. Lewis, Optimal estimation: with an introduction to stochastic control theory, New York: John Wiley & Sons, 1986. |
7 | Y. Song and B. Song, "A Comparative Study of Real-Time Aircraft Parameter Identification Schemes Applied to NASA F/A-18 HARV Flight Data," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 45, No. 149, 2002. |
8 | Y. Song, B. Seanor, M. Napolitano, G. Campa, "Online Parameter Estimation Techniques Comparison Within a Fault Tolerant Flight Control System," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 3, 2002 |
9 | H. Y. Yang, Aerodynamic Parameter Identification of a Missile using Maximum Likelihood Method and Extended Kalman Filter, MS. Dissertation, Department of Electrical Engineering and The Graduate School of Seoul National University, 1984. |
10 | J.G. Lee and D. H. Lee, "Aerodynamic Parameter Identification of a Tactical Missile Utilizing Post flight Telemetry Data," AIAA 12th Atmospheric Flight Mechanics Conference, Snowmass, Colorado, August 1985. |
11 | T. G. Sung, Missile Aerodynamic Parameter Identification under Uncertain Model Structure, MS. Dissertation, Department of Electrical Engineering and The Graduate School of Seoul National University, 1986. |
12 | D. H. Lee, Comparison of Parameter Identification Algorithms for an Aircraft, Ph.D. Dissertation, Department of Electrical Engineering and The Graduate School of Seoul National University, 1992. |
13 | S. T. Park, J.G. Lee and G. Chen, "Comments on 'Modified Extended Kalman Filtering and a Real-Time Parallel Algorithm for System Parameter Identification," IEEE Transactions on Automatic Control, Vol. 40, No. 9, September 1995, pp. 1661-1662. DOI ScienceOn |
14 | Y. Song and M.S. Hwang, "A Study on the Aircraft Parameter Estimation form Flight Test Data," Journal of the KSAS, Vol. 26, No. 6, October, 1998, pp. 1-12. |
15 | W. S. Ra, I. H. Whang, and J. B. Park, "Non-conservative robust Kalman filtering using a noise corrupted measurement matrix", IET Control Theory and Applications, 2009, Vol. 3, Iss. 9, pp. 1226-1236. DOI ScienceOn |
16 | T. J. Sooy, "Aerodynamic Predictions, Comparisons, and Validations Using Missile DATCOM (97) and Aeroprediction 98 (AP98) ," AIAA Paper 04-1246, January, 2004. |
17 | Brain L. Stevens, Frank L. Lewis, Aircraft Control and Simulation. John Wiley and Sons, Inc., 2003, ch. 2. |
18 | P. G. Hamel and R. Jategaonkar, "Evolution of flight vehicle system identification," J. Aircraft, 1996, 33, (1), pp. 9-28. DOI |
19 | M. R. Ananthasayanam, "Parameter Estimation of a Flight Vehicle Using MMLE/BFGS Estimator Under Limited Measurements," AIAA Paper 02-4624, August, 2002. |
20 | G. Chowdhary, "Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman Filter," AIAA Paper 06-6146, August, 2006. |
21 | S. Singh, "Parameter Estimation from Flight Data of a missile using Maximum Likelihood and Neural Network Method," AIAA Paper 06-6284, August, 2006. |
![]() |