Szczegóły

Tytuł artykułu

Non-Certainty-Equivalent Adaptive Control of a Nonlinear Aeroelastic System

Tytuł czasopisma

International Journal of Electronics and Telecommunications

Rocznik

2010

Wolumin

vol. 56

Numer

No 4

Autorzy publikacji

Wydział PAN

Nauki Techniczne

Wydawca

Polish Academy of Sciences Committee of Electronics and Telecommunications

Data

2010

Identyfikator

ISSN 2081-8491 (until 2012) ; eISSN 2300-1933 (since 2013)

Referencje

Fung Y. (1955), An Introduction to the Theory of Aeroelasticity, 207. ; (1995), A Modern Course in Aeroelasticity. ; Mukhopadhyay V. (2003), Historical perspective on analysis and control of aeroelastic responses, Journal of Guidance, Control, and Dynamics, 26, 5, 673. ; Lind R. (1999), Robust Aeroservoelastic Stability Analysis, doi.org/10.1007/978-1-4471-0849-8 ; Waszak M. (2001), Robust multivariable flutter suppression for the benchmark active control technology wind- tunnel model, Journal of Guidance, Control, and Dynamics, 24, 1, 147. ; Scott R. (2000), Benchmark active controls technology model aerodynamic data, Journal of Guidance, Control and Dynamics, 23, 5, 914. ; Mukhopadhyay V. (2000), Transonic flutter suppression control law design and wind-tunnel test results, Journal of Guidance, Control and Dynamics, 23, 5, 930. ; Kelkar A. (2000), Passivity-based robust control with application to benchmark active controls technologywing, Journal of Guidance, Control and Dynamics, 23, 5, 938. ; Barker J. (2000), Comparing linear parameter- varying gains-cheduled control techniques for active flutter suppression, Journal of Guidance, Control and Dynamics, 23, 5, 948. ; Guillot D. (2000), Fundamental aeroservoelastic study combining unsteady computational fluid mechanics with adaptive control, Journal of Guidance, Control and Dynamics, 23, 6, 1117. ; Scott R. (2000), Active control ofwind-tunnel model aeroelastic response using neural networks, Journal of Guidance, Control and Dynamics, 23, 6, 1100. ; Ko J. (1997), Nonlinear control of a prototypical wing section with torsional nonlinearity, Journal of Guidance, Control and Dynamics, 20, 6, 1181. ; Ko J. (1998), Stability and control of a structurally nonlinear aeroelastic system, Journal of Guidance, Control, and Dynamics, 21, 5, 718. ; Block J. (1998), Applied active control for a nonlinear aeroelastic structure, Journal of Guidance, Control, and Dynamics, 21, 6, 838. ; Lee K. (2007), Global robust control of an aeroelastic system using output feedback, Journal of Guidance, Control and Dynamics, 30, 1, 271. ; Xing W. (2000), Adaptive output feedback control of a nonlinear aeroelastic structure, Journal of Guidance, Control and Dynamics, 23, 6, 1109. ; Ko J. (1999), Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity, Nonlinear Dynamics, 18, 3, 289. ; Behal A. (2006), Adaptive control for a nonlinear wing section with multiple flaps, Journal of Guidance, Control, and Dynamics, 29, 3, 744. ; Singh S. (2003), Modular adaptive control of a nonlinear aeroelastic system, Journal of Guidance, Control, and Dynamics, 26, 3, 443. ; Narendra K. (1989), Stable Adaptive Systems. ; Krstic M. (1995), Nonlinear and adaptive control design. ; Astolfi A. (2003), Immersion and invariance : a new tool for stabilization and adaptive control of nonlinear systems, IEEE Transaction on Automatic Control, 48, 4, 590. ; Karagiannis D. (2004), Nonlinear adaptive control of systems in feedback form : An alternative to adaptive backstepping, null, 71. ; Astolfi A. (2008), Nonlinear and adaptive Control with applications. ; Seo D. (2008), High-performance spacecraft attitudetracking control through attracting-manifold design, Journal of Guidance, Control and Dynamics, 31, 4, 884. ; Seo D. (2009), Non-certainty equivalent adaptive control for robot manipulator systems, Systems & Control Letters, 58, 304. ; Lee K. (2009), Immersion and invariance based adaptive control of a nonlinear aeroelastic system, Journal of Guidance, Control, and Dynamics, 32, 4, 1100. ; Lee K. (2009), Noncertainty-equivalent adaptive satellite attitude control using solar radiation pressure, null.

DOI

10.2478/v10177-010-0063-7

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