Add to ORKGTwo flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a DC-10 derivative wing. Both control laws demontrated increases in flutter speed in excess of 25 percent above the passive wing flutter speed. In addition, one of the control laws was effective in reducing loads due to turbulence generated in the wind tunnel. The effect of variations in gain and phase on the closed-loop performance was measured and is compared with predictions. In general, both flutter and gust response predictions agree reasonably well with experimental data
Active flutter suppression control laws were designed, implemented, and tested on an aeroelastically...
A general discussion of the airplane applications of active flutter suppression systems is presented...
This work addresses control law synthesis for active flutter suppression followed by the design and ...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
Comparisons are presented analytically predicted and experimental turbulence responses of a wind tun...
The synthesis, implementation, and wind tunnel test of two flutter suppression control laws for an a...
Results of work done on active controls on the modified YF-17 flutter model are summarized. The basi...
The synthesis and experimental validation of a control law for13; an actiqe flutter suppression syst...
The application of active control technology to the suppression of flutter has been successfully dem...
The effects of active controls on flutter suppression and gust alleviation of the Arava twin turbopr...
Three control law design techniques for flutter suppression are presented. Each technique uses multi...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
Active flutter suppression control laws were designed, implemented, and tested on an aeroelastically...
A general discussion of the airplane applications of active flutter suppression systems is presented...
This work addresses control law synthesis for active flutter suppression followed by the design and ...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
Comparisons are presented analytically predicted and experimental turbulence responses of a wind tun...
The synthesis, implementation, and wind tunnel test of two flutter suppression control laws for an a...
Results of work done on active controls on the modified YF-17 flutter model are summarized. The basi...
The synthesis and experimental validation of a control law for13; an actiqe flutter suppression syst...
The application of active control technology to the suppression of flutter has been successfully dem...
The effects of active controls on flutter suppression and gust alleviation of the Arava twin turbopr...
Three control law design techniques for flutter suppression are presented. Each technique uses multi...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
Active flutter suppression control laws were designed, implemented, and tested on an aeroelastically...
A general discussion of the airplane applications of active flutter suppression systems is presented...
This work addresses control law synthesis for active flutter suppression followed by the design and ...