Journal
IET CONTROL THEORY AND APPLICATIONS
Volume 1, Issue 6, Pages 1638-1649Publisher
INST ENGINEERING TECHNOLOGY-IET
DOI: 10.1049/iet-cta:20060455
Keywords
-
Ask authors/readers for more resources
The nonlinear flutter suppression of a typical wing section is investigated. A structural nonlinearity is considered in the pitch direction. Integral-input-to-state stability (iISS) concept is utilised for the construction of a feedback controller. One of the advantages of this design is its simplicity and straightforwardness. A backstepping method is used to compare the results for the typical section, which is a multi-input system. The iISS controller has an outstanding performance in comparison to the backstepping method, especially with regards to the disturbance attenuation problem. A Lyapunov-based controller was also introduced for the system.
Authors
I am an author on this paper
Click your name to claim this paper and add it to your profile.
Reviews
Recommended
No Data Available