The purpose of this presentation is to inform the Guidance and Control community of capabilities which were developed by the Aeroservoelasticity Branch to evaluate the performance of multivariable control laws, on-line, during wind-tunnel testing. The capabilities are generic enough to be useful for all kinds of on-line analyses involving multivariable control in experimental testing. Consequently, it was decided to present this material at this workshop even though it has been presented elsewhere. Topics covered include: essential on-line analysis requirements; on-line analysis capabilities; on-line analysis software; frequency domain procedures; controller performance evaluation frequency-domain flutter suppression; and plant determinatio...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
A variety of on-line analysis tools were developed to support two active flexible wing (AFW) wind-tu...
Described here is the development and implementation of on-line, near real time controller performan...
Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
A Controller Performance Evaluation (CPE) methodology for multi-input/multi-output digital control s...
Active flutter suppression control laws were designed, implemented, and tested on an aeroelastically...
The process is described of analysis, design, digital implementation, and subsonic testing of an act...
Three control law design techniques for flutter suppression are presented. Each technique uses multi...
The status of the joint NASA/Rockwell Active Flexible Wing Wind-Tunnel Test Program is described. Th...
This work addresses control law synthesis for active flutter suppression followed by the design and ...
Three flutter suppression control law design techniques are presented. Each uses multiple control su...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...
A variety of on-line analysis tools were developed to support two active flexible wing (AFW) wind-tu...
Described here is the development and implementation of on-line, near real time controller performan...
Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
A Controller Performance Evaluation (CPE) methodology for multi-input/multi-output digital control s...
Active flutter suppression control laws were designed, implemented, and tested on an aeroelastically...
The process is described of analysis, design, digital implementation, and subsonic testing of an act...
Three control law design techniques for flutter suppression are presented. Each technique uses multi...
The status of the joint NASA/Rockwell Active Flexible Wing Wind-Tunnel Test Program is described. Th...
This work addresses control law synthesis for active flutter suppression followed by the design and ...
Three flutter suppression control law design techniques are presented. Each uses multiple control su...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
Design of a control law for simultaneously suppressing the symmetric and antisymmetric flutter modes...
The computer-controlled data-acquisition system recently installed for use with a transonic dynamics...