References
- Y. Song, B. Song,B.Seanor,and M.Napolitano,"OnLineAircraft Parameter Using Fourier Transform Regression With an Application to NASA F/A-18 HARV Flight Data," KSME International Journal, vol. 16, no.3, pp. 327-337, 2002
- www.eecs.berkeley.edul
- B. Mettler, M. B. Tishler, and T. Kanade, "System identification modeling of a small-scale unmanned rotorcraft for flight control design," Journal of the American Helicopter Society, vol. 47, no. 1, pp. 50-63, 2002
- M. B. Tischler and R K. Remple, Aircraft andRotorcraft System Identification, AIAA, 2006
- V. Klein and E. A. Morelli, Aircraft System Identifica-tion : Theory and Practice, AIAA, 2006
- P. G. Hamel (ed.), RotorcraJt System Identification,AGARD-AR-280, 1991
- M. B. Tischler, "System Identification Requirements for High-Bandwidth Rotorcraft Flight Control System Design," J of Guidance, Control, and Dynamics, vol.13, no. 5, pp. 835-841, 1990
- J Lucas, B. Martin, L. Ericsson, C. Catterall, and M.Cole, "Combining Static Analyses and Frequency Domain System Identification to Enhance the Accuracy of a Fixed-Wing UAV Simulation," AIAA Aerospace Sciences Meeting, AIAA 2006-640, Jan. 2006