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• W1991087163 abstract "No AccessEngineering NoteRobust Nonlinear Feedback Design for Wing Rock StabilizationSalim Ibrir and Chun-Yi SuSalim IbrirDepartment of Electrical and Computer Engineering, University of the West Indies, St. Augustine, Republic of Trinidad and Tobago*Senior Lecturer, Department of Electrical and Computer Engineering. Member AIAA.Search for more papers by this author and Chun-Yi SuDepartment of Mechanical and Industrial Engineering, Concordia University, Montreal, Quebec H3G 1M8, Canada†Professor, Department of Mechanical and Industrial Engineering, 1455 de Maisonneuve Blvd. W.Search for more papers by this authorPublished Online:10 Jan 2014https://doi.org/10.2514/1.61314SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Go T. H., “Lateral-Directional Aircraft Dynamics Under Static Moment Nonlinearity,” Journal of Guidance, Control, and Dynamics, Vol. 32, No. 1, 2009, pp. 305–309. doi:https://doi.org/10.2514/1.39025 JGCDDT 0162-3192 LinkGoogle Scholar[2] Go T. H. and Ramnath R. V., “An Analytical Theory of Three Degree-Of-Freedom Aircraft Wing Rock,” Journal of Guidance, Control, and Dynamics, Vol. 27, No. 4, 2004, pp. 657–664. doi:https://doi.org/10.2514/1.11132 JGCDDT 0162-3192 LinkGoogle Scholar[3] Pamadi B. N., Performance, Stability, Dynamics, and Control of Airplanes, edited by Schetz J. A., AIAA Education Series, 2nd ed., AIAA, Reston, VA, 2004, pp. 677–754. CrossrefGoogle Scholar[4] Ericsson L. E., “Various Sources of Wing Rock,” Journal of Aircraft, Vol. 27, No. 6, 1990, pp. 488–494. doi:https://doi.org/10.2514/3.25309 JAIRAM 0021-8669 LinkGoogle Scholar[5] Monahemi M. M. and Krstic M., “Control of Wing Rock Motion Using Adaptive Linearization,” Journal of Guidance, Control, and Dynamics, Vol. 19, No. 4, 1996, pp. 905–912. doi:https://doi.org/10.2514/3.21717 JGCDDT 0162-3192 LinkGoogle Scholar[6] Joshi S. V., Sreenatha A. G. and Chandrasekhar J., “Suppression of Wing Rock of Slender Delta Wings Using a Single Neuron Controller,” IEEE Transactions on Control Systems Technology, Vol. 6, No. 5, 1998, pp. 671–677. doi:https://doi.org/10.1109/87.709502 IETTE2 1063-6536 CrossrefGoogle Scholar[7] Go T. H., Aircraft Wing Rock Dynamics and Control, Ph.D. Thesis, Massachusetts Inst. of Technology, Cambridge, MA, Sept. 1999. Google Scholar[8] Sreenatha A. G., Wong P. P. and Choi J. Y., “Suppression of Wing Rock Using Artificial Neural Networks and Fuzzy Logic Controller,” Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1247–1252. doi:https://doi.org/10.2514/1.6848 JAIRAM 0021-8669 LinkGoogle Scholar[9] Lin C.-M. and Hsu C.-F., “Supervisory Recurrent Fuzzy Neural Network Control of Wing Rock for Slender Delta Wings,” IEEE Transactions on Fuzzy Systems, Vol. 12, No. 5, 2004, pp. 733–742. doi:https://doi.org/10.1109/TFUZZ.2004.834803 IEFSEV 1063-6706 CrossrefGoogle Scholar[10] Liu Z. L. and Svoboda J., “A New Control Scheme for Nonlinear Systems with Disturbances,” IEEE Transactions on Control Systems Technology, Vol. 14, No. 1, 2006, pp. 176–181. doi:https://doi.org/10.1109/TCST.2005.860510 IETTE2 1063-6536 CrossrefGoogle Scholar[11] Ordóñez R. and Passino K. V., “Control of Discrete Time Nonlinear Systems with a Time-Varying Structure,” Automatica, Vol. 39, No. 3, 2003, pp. 463–470. doi:https://doi.org/10.1016/S0005-1098(02)00249-2 ATCAA9 0005-1098 CrossrefGoogle Scholar[12] Nayfeh A. H., Elzebda J. M. and Mook D. T., “Analytical Study of the Subsonic Wing Rock Phenomenon for Slender Delta Wings,” Journal of Aircraft, Vol. 26, No. 9, 1989, pp. 805–809. doi:https://doi.org/10.2514/3.45844 JAIRAM 0021-8669 LinkGoogle Scholar Previous article Next article" @default.
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