Iterative adaptive control of a three degrees-of-freedom aeroelastic wing model

J. Tar, I. Rudas, János F. Bitó, Krisztián Kósi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

The aeroelastic wing model is an underactuated 3 Degrees-of-Freedom (DoF) system in which only a single control signal can be applied. Its model-based control attracted much attention recently. In the present contribution the effects of -20% modeling error in two significant system parameters are investigated in PI and P-type controllers that can be made adaptive by the application of Robust Fixed Point Transformations (RFPT). It is shown that by the use of this simple adaptive technique operating with altogether 4 control parameters precise control of the trailing-edge surface deflection is possible. This statement is substantiated by simulation results.

Original languageEnglish
Title of host publicationApplied Mechanics and Materials
Pages1593-1599
Number of pages7
Volume300-301
DOIs
Publication statusPublished - 2013
Event2nd International Conference on Mechatronics and Applied Mechanics, ICMAM 2012 - , Taiwan, Province of China
Duration: Dec 8 2012Dec 9 2012

Publication series

NameApplied Mechanics and Materials
Volume300-301
ISSN (Print)16609336
ISSN (Electronic)16627482

Other

Other2nd International Conference on Mechatronics and Applied Mechanics, ICMAM 2012
CountryTaiwan, Province of China
Period12/8/1212/9/12

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Controllers

Keywords

  • Adaptive control
  • Aeroelastic wing model
  • Robust fixed point transformations
  • Underactuated systems

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Tar, J., Rudas, I., Bitó, J. F., & Kósi, K. (2013). Iterative adaptive control of a three degrees-of-freedom aeroelastic wing model. In Applied Mechanics and Materials (Vol. 300-301, pp. 1593-1599). (Applied Mechanics and Materials; Vol. 300-301). https://doi.org/10.4028/www.scientific.net/AMM.300-301.1593

Iterative adaptive control of a three degrees-of-freedom aeroelastic wing model. / Tar, J.; Rudas, I.; Bitó, János F.; Kósi, Krisztián.

Applied Mechanics and Materials. Vol. 300-301 2013. p. 1593-1599 (Applied Mechanics and Materials; Vol. 300-301).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Tar, J, Rudas, I, Bitó, JF & Kósi, K 2013, Iterative adaptive control of a three degrees-of-freedom aeroelastic wing model. in Applied Mechanics and Materials. vol. 300-301, Applied Mechanics and Materials, vol. 300-301, pp. 1593-1599, 2nd International Conference on Mechatronics and Applied Mechanics, ICMAM 2012, Taiwan, Province of China, 12/8/12. https://doi.org/10.4028/www.scientific.net/AMM.300-301.1593
Tar J, Rudas I, Bitó JF, Kósi K. Iterative adaptive control of a three degrees-of-freedom aeroelastic wing model. In Applied Mechanics and Materials. Vol. 300-301. 2013. p. 1593-1599. (Applied Mechanics and Materials). https://doi.org/10.4028/www.scientific.net/AMM.300-301.1593
Tar, J. ; Rudas, I. ; Bitó, János F. ; Kósi, Krisztián. / Iterative adaptive control of a three degrees-of-freedom aeroelastic wing model. Applied Mechanics and Materials. Vol. 300-301 2013. pp. 1593-1599 (Applied Mechanics and Materials).
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