Aeroelastic response of flapped wing systems using robust estimation methodology

Sung Soo Na, Liviu Librescu, Pier Marzocca, Myung Hyun Kim, In Joo Jeong

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

4 Citations (Scopus)

Abstract

This paper concerns the active aeroelastic control of 3-D flap-wing systems exposed to gust and/or sonic boom in an incompressible flow field. This is achieved via implementation of a robust estimation capability (sliding mode observer: SMO), and of the use of the deflected flap as to suppress the flutter instability or enhance the subcritical aeroelastic response to gust or blast loads. To this end, a control methodology using LQG(Linear Quadratic Gaussian) in conjunction with SMO is implemented, and its performance toward suppressing flutter and reducing the vibrational level in the subcritical flight speed range is demonstrated. Moreover, its performances are compared with the ones provided via implementation of conventional LQG with Kalman filter.

Original languageEnglish
Title of host publicationCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Pages1764-1775
Number of pages12
Volume3
Publication statusPublished - 2004
EventCollect. of Pap. - 45th AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. and Mater. Conf.; 12th AIAA/ASME/AHS Adapt. Struct. Conf.; 6th AIAA Non-Deterministic Approaches Forum; 5th AIAA Gossamer Spacecraft Forum - Palm Springs, CA, United States
Duration: 2004 Apr 192004 Apr 22

Other

OtherCollect. of Pap. - 45th AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. and Mater. Conf.; 12th AIAA/ASME/AHS Adapt. Struct. Conf.; 6th AIAA Non-Deterministic Approaches Forum; 5th AIAA Gossamer Spacecraft Forum
CountryUnited States
CityPalm Springs, CA
Period04/4/1904/4/22

Fingerprint

Flaps
Incompressible flow
Kalman filters
Flow fields

ASJC Scopus subject areas

  • Architecture

Cite this

Na, S. S., Librescu, L., Marzocca, P., Kim, M. H., & Jeong, I. J. (2004). Aeroelastic response of flapped wing systems using robust estimation methodology. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (Vol. 3, pp. 1764-1775)

Aeroelastic response of flapped wing systems using robust estimation methodology. / Na, Sung Soo; Librescu, Liviu; Marzocca, Pier; Kim, Myung Hyun; Jeong, In Joo.

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Vol. 3 2004. p. 1764-1775.

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

Na, SS, Librescu, L, Marzocca, P, Kim, MH & Jeong, IJ 2004, Aeroelastic response of flapped wing systems using robust estimation methodology. in Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. vol. 3, pp. 1764-1775, Collect. of Pap. - 45th AIAA/ASME/ASCE/AHS/ASC Struct., Struct. Dyn. and Mater. Conf.; 12th AIAA/ASME/AHS Adapt. Struct. Conf.; 6th AIAA Non-Deterministic Approaches Forum; 5th AIAA Gossamer Spacecraft Forum, Palm Springs, CA, United States, 04/4/19.
Na SS, Librescu L, Marzocca P, Kim MH, Jeong IJ. Aeroelastic response of flapped wing systems using robust estimation methodology. In Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Vol. 3. 2004. p. 1764-1775
Na, Sung Soo ; Librescu, Liviu ; Marzocca, Pier ; Kim, Myung Hyun ; Jeong, In Joo. / Aeroelastic response of flapped wing systems using robust estimation methodology. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Vol. 3 2004. pp. 1764-1775
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