Add to ORKGActive flutter suppression control laws were designed, implemented, and tested on an aeroelastically-scaled wind tunnel model in the NASA Langley Transonic Dynamics Tunnel. One of the control laws was successful in stabilizing the model while the dynamic pressure was increased to 24 percent greater than the measured open-loop flutter boundary. Other accomplishments included the design, implementation, and successful operation of a one-of-a-kind digital controller, the design and use of two simulation methods to support the project, and the development and successful use of a methodology for on-line controller performance evaluation
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program...
The status of the joint NASA/Rockwell Active Flexible Wing Wind-Tunnel Test Program is described. Th...
The synthesis and experimental validation of a control law for13; an actiqe flutter suppression syst...
The synthesis and experimental validation of an active flutter suppression controller for the Active...
Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes...
The process is described of analysis, design, digital implementation, and subsonic testing of an act...
The Active Flexible Wing Project is a collaborative effort between the NASA Langley Research Center ...
Three control law design techniques for flutter suppression are presented. Each technique uses multi...
An outline of the Active Flexible Wing (AFW) project that was meant to serve as an introduction to a...
The synthesis, implementation, and wind tunnel test of two flutter suppression control laws for an a...
A summary of the NASA/Rockwell Active Flexible Wing Program is presented. Major elements of the prog...
For a specific application of aeroservoelastic technology, Rockwell International Corporation develo...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program...
The status of the joint NASA/Rockwell Active Flexible Wing Wind-Tunnel Test Program is described. Th...
The synthesis and experimental validation of a control law for13; an actiqe flutter suppression syst...
The synthesis and experimental validation of an active flutter suppression controller for the Active...
Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes...
The process is described of analysis, design, digital implementation, and subsonic testing of an act...
The Active Flexible Wing Project is a collaborative effort between the NASA Langley Research Center ...
Three control law design techniques for flutter suppression are presented. Each technique uses multi...
An outline of the Active Flexible Wing (AFW) project that was meant to serve as an introduction to a...
The synthesis, implementation, and wind tunnel test of two flutter suppression control laws for an a...
A summary of the NASA/Rockwell Active Flexible Wing Program is presented. Major elements of the prog...
For a specific application of aeroservoelastic technology, Rockwell International Corporation develo...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...