Flutter suppression for the active flexible wing: Control system design and experimental validation AIAA-92-2097

Waszak, Martin R and Srinathkumar, S (1992) Flutter suppression for the active flexible wing: Control system design and experimental validation AIAA-92-2097. In: Dynamics specialists conference.

[img] PDF
92-2097.pdf

Download (2MB)
[img] Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt

Download (9kB)

Abstract

The synthesis and experimental validation of a control law for13; an actiqe flutter suppression system for the Active Flexible13; Wing wind-tunnel model is presenied. The design was13; accomplished with traditional root locus and Nyquist methods13; using interactive computer graphics tools and with extensive use13; of simulation-based analysis. The design approach relied on a13; fundamental understanding of the flutter mechanism to13; formulate a simple control law structure. Experimentally, the13; flutter suppression controller succeeded in simultaneous13; suppression of two flutter modes, significantly increasing the13; flutter dynamic pressure despite errors in the design model. The13; flutter suppression controller was also successfully operated in13; combination with a rolling maneuver controller to perform13; flutter suppression during rapid rolling maneuvers.

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Flutter dynamic;Flutter suppression
Subjects: AERONAUTICS > Aircraft Stability and Control
Depositing User: Mrs Manoranjitha M D
Date Deposited: 24 Feb 2006
Last Modified: 13 Oct 2015 08:14
URI: http://nal-ir.nal.res.in/id/eprint/1067

Actions (login required)

View Item View Item