A Controller Performance Evaluation (CPE) methodology for multi-input/multi-output digital control systems was developed and tested on an aeroelastic wind-tunnel model. Modern signal processing methods were used to implement control laws and to acquire time domain data of the whole system (controller and plant) from which appropriate transfer matrices of the control system could be generated. Matrix computational procedures were used to calculate singular values of return-difference matrices at the plant input and output points to evaluate the performance of the control system. The CPE procedures effectively identified potentially destabilizing controllers and confirmed the satisfactory performance of stabilizing ones
A variety of on-line analysis tools were developed to support two active flexible wing (AFW) wind-tu...
A sensitivity analysis technique for multiloop flight control systems is studied. This technique use...
The design, evaluation, and testing of a practical, multivariable, linear quadratic regulator contro...
Described here is the development and implementation of on-line, near real time controller performan...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
The purpose of this presentation is to inform the Guidance and Control community of capabilities whi...
Research on flight control systems is reviewed. Investigations were conducted to evaluate and test a...
Singular value analysis can give conservative stability margin results. Applying structure to the un...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program...
The analysis and design of complex multivariable reliable control systems are considered. High perfo...
Digital techniques to increase reliability and accuracy of spacecraft control and stabilization syst...
A frequency-based performance identification approach was evaluated using flight data from the NASA ...
New performance measures, detailed examples, modeling of error detection process, performance evalua...
Formal methods research begins to produce methods which will enable mathematic modeling of the physi...
A variety of on-line analysis tools were developed to support two active flexible wing (AFW) wind-tu...
A sensitivity analysis technique for multiloop flight control systems is studied. This technique use...
The design, evaluation, and testing of a practical, multivariable, linear quadratic regulator contro...
Described here is the development and implementation of on-line, near real time controller performan...
A real time multiple-function digital controller system was developed for the Active Flexible Wing (...
The purpose of this presentation is to inform the Guidance and Control community of capabilities whi...
Research on flight control systems is reviewed. Investigations were conducted to evaluate and test a...
Singular value analysis can give conservative stability margin results. Applying structure to the un...
Multivariable control theory is applied to the design of multiple input and output engine controls. ...
Flutter suppression (FS) is one of the active control concepts being investigated by the AFW program...
The analysis and design of complex multivariable reliable control systems are considered. High perfo...
Digital techniques to increase reliability and accuracy of spacecraft control and stabilization syst...
A frequency-based performance identification approach was evaluated using flight data from the NASA ...
New performance measures, detailed examples, modeling of error detection process, performance evalua...
Formal methods research begins to produce methods which will enable mathematic modeling of the physi...
A variety of on-line analysis tools were developed to support two active flexible wing (AFW) wind-tu...
A sensitivity analysis technique for multiloop flight control systems is studied. This technique use...
The design, evaluation, and testing of a practical, multivariable, linear quadratic regulator contro...