@inproceedings{b184b0d429784aa1992a67baadc7a6d3,

title = "Distributed parameter optimal control by adjoint aeroelastic differential operators for mode suppression control",

abstract = "This paper presents a distributed parameter optimal control method. The state-space equation of wing bending-torsion aeroelasticity is formulated using aeroelastic differential operators. The optimal control problem is formulated as linear quadratic regulator in a Hilbert inner product space. The solution to the optimal control problem leads to a differential operator Ricatti equation. Using a finite-series modal approximation, the differential operator Ricatti equation is converted into a spatially dependent Ricatti equation. The solution of this spatially dependent Ricatti equation is used to compute the distributed parameter optimal control which is spatially continuous. A flutter suppression control application is demonstrated on a flexible wing transport aircraft outfitted with a variable camber continuous trailing edge flap system.",

author = "Nhan Nguyen and Eric Ting and Sean Swei and Abraham Ishihara",

year = "2013",

language = "British English",

isbn = "9781624102240",

series = "AIAA Guidance, Navigation, and Control (GNC) Conference",

booktitle = "AIAA Guidance, Navigation, and Control (GNC) Conference",

note = "AIAA Guidance, Navigation, and Control (GNC) Conference ; Conference date: 19-08-2013 Through 22-08-2013",

}