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NASA TN D-6579, 1972. [12] Ili! KW, Maine RE. Practical aspects of using a maximum likelihood estimation method to extract stability and control derivatives from #ight data. NASA TN D-8209, 1976. [13] Maine RE, Ili! KW. Identi"cation of dynamic systems: theory and formulation. NASA RF 1168, June 1986. [14] Mendel JM. Discrete techniques of parameter estimation. New York, NY: Marcel Dekker, 1973. [15] Ljung L. System identi"cation: theory for the user. s, NJ: Prentice-Hall, 1987. [16] Bodson M. An information-dependent data forgetting adaptive algorithm.

High accuracy evaluation of the "nite Fourier transform using sampled data. NASA TM 110340, June 1997. [23] Klein V. Aircraft parameter estimation in frequency domain. Proceedings of the 1978 AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 78-1344, Palo Alto, CA, August 1978. [24] Roskam J. Airplane #ight dynamics and automatic #ight controls: Part I. Roskam Aviation and Engineering Coorporation, Ottawa, KA, 1994. R. Napolitano et al. / Aircraft Design 4 (2001) 19}50 [25] Hoak DE, Finck RD.

4] Calise AJ, Lee S, Sharma M. Direct adpative recon"gurable control of a tailless "ghter aircraft. Proceedings of the 1998 AIAA Guidance Navigation and Control Conference, AIAA Paper 98-4108, Boston, MA, August 1998. [5] Totah J. Adaptive #ight control and on-line learning. Proceedings of the 1997 AIAA Guidance Navigation and Control Conference, AIAA Paper 97-3537, New Orleans, LA, August 1997. [6] Jorgensen CC. Direct adaptive aircraft control using dynamic cell structure neural networks. NASA TM 112198, May 1997.

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Battle Over the Reich: The Strategic Bomber Offensive Against Germany, 1939-1943 by Dr Alfred Price


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