Parameter identification for inflight detection and characterization of aircraft icing

Åström, 1995 Bragg, M. B. (1996). Aircraft aerodynamic effects due to large droplet ice accretions. Proceedings of the 34th AIAA aerospace sciences meeting and exhibit, number AIAA-96-0932. Reno, NV. Bragg, M. B., Perkins, W. R., Sarter, N. B., Başar, T., Voulgaris, P. G., Gurbacki, H. M., Melody, J. W., & McCray, S. A. (1998). An interdisciplinary approach to inflight aircraft icing safety. Proceedings of the 36th AIAA aerospace sciences meeting and exhibit, number AIAA-98-0095. Reno, NV. Chandler, 1995, System identification for adaptive and reconfigurable control, AIAA Journal of Guidance, Control, & Dynamics, 18, 516, 10.2514/3.21417 Cole, J., & Sands, W. (1991). Statistical study of aircraft icing accidents. Proceedings of the 29th AIAA aerospace sciences meeting and exhibit, number AIAA-91-0558. Reno, NV. Didinsky, 1995, Parameter identification of uncertain plants using H∞ methods, Automatica, 31, 1227, 10.1016/0005-1098(95)00073-6 Etkin, 1996 Hillbrand, T. (1999). Identification of time-varying flight dynamics parameters for aircraft icing detection and classification using H∞ methods. Technical Report UILU-ENG-99-2223 DC-190, Coordinated Science Laboratory, University of Illinois at Urbana-Champaign. Kalman, 1961, New results in linear filtering and prediction theory, ASME Journal of Basic Engineering Series, 83D, 95, 10.1115/1.3658902 Khalil, 1996 Lee, 1999, Experimental investigation of simulated large-droplet ice shapes on airfoil aerodynamics, Journal of Aircraft, 36, 844, 10.2514/2.2518 Ljung, 1979, Asymptotic behavior of the extended Kalman filter as a parameter estimator for linear systems, IEEE Transactions on Automatic Control, AC-24, 36, 10.1109/TAC.1979.1101943 Ljung, L. (1999). System identification: Theory for the user, Information and Systems Sciences Series, (2nd ed.). Englewood Cliffs, NJ: Prentice-Hall. Morelli, 1995, Global nonlinear aerodynamic modeling using multivariate orthogonal functions, Journal of Aircraft, 32, 270, 10.2514/3.46712 Murray, 1994 NASA (1997). Weather investment recommendations. Technical Report, NASA Aeronautics Safety Investment Strategy. Olsen, W., & Shaw, R. (1984). Ice shapes and the resulting drag increase for a NACA 0012 airfoil. Technical Report 83556, NASA. Poor, 1994 Ratvasky, T. P., & Ranaudo, R. J. (1993). Icing effects on aircraft stability and control determined from flight data. Proceedings of the 31st AIAA aerospace sciences meeting and exhibit, number AIAA-93-0398. Reno, NV. Ratvasky, T. P., Van Zante, J., & Riley, J. T. (1999). NASA/FAA tailplane icing program overview. Proceedings of the 37th AIAA aerospace sciences meeting and exhibit, number AIAA-99-0370. Reno, NV. Roskam, 1982 Sage, A. P., & White III, C. C. (1977). Optimum systems control, (2nd ed.). Englewood Cliffs, NJ: Prentice-Hall. Sastry, S. S., & Bodson, M. (1989). Adaptive control: Stability, convergence and robustness. Information and System Sciences. Englewood Cliffs, NJ: Prentice-Hall. Schuchard, E. A., Melody, J. W., Başar, T., Perkins, W. R., & Voulgaris, P. (2000). Detection and classification of aircraft icing using neural networks. Proceedings of the 38th AIAA aerospace sciences meeting and exhibit, number AIAA-2000-0361. Reno, NV. Stevens, 1992 Ward, D. G., & Barron, R. (1995). A self-designing receding horizon optimal flight controller. Proceedings of the American control conference, Seattle, WA (pp. 3490–3494).