Details

Title

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

Journal title

International Journal of Electronics and Telecommunications

Yearbook

2010

Volume

vol. 56

Numer

No 4

Publication authors

Divisions of PAS

Nauki Techniczne

Description

International Journal of Electronics and Telecommunications (IJET, eISSN 2300-1933, untill 2013 also print ISSN 2081-8491) is a periodical of Electronics and Telecommunications Committee of Polish Academy of Sciences and it is published by Warsaw Science Publishers of PAS. It continues tradition of the Electronics and Telecommunications Quarterly (ISSN 0867-6747) established in 1955 as the Rozprawy Elektrotechniczne. The IJET is a scientific periodical where papers present the results of original, theoretical, experimental and reviewed works. They consider widely recognized aspects of modern electronics, telecommunications, microelectronics, optoelectronics, radioelectronics and medical electronics.

The authors are outstanding scientists, well‐known experienced specialists as well as young researchers – mainly candidates for a doctor's degree. The papers present original approaches to problems, interesting research results, critical estimation of theories and methods, discuss current state or progress in a given branch of technology and describe development prospects. All the papers published in IJET are reviewed by international specialists who ensure that the publications are recognized as author's scientific output.

The printed periodical is distributed among all those who deal with electronics and telecommunications in national scientific centers as well as in numeral foreign institutions, and it is subscribed by many specialists and libraries. Its electronic version is available at http://ijet.pl.

The papers received are published within half a year if the cooperation between author and the editorial staff is efficient. The papers may be submitted to the editorial office by the journal web page http://ijet.pl.

Publisher

Polish Academy of Sciences Committee of Electronics and Telecommunications

Date

2010

Identifier

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

References

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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