The design of modern aerospace systems relies on the efficient utilization of computational resources and the availability of computational tools to provide accurate system modeling. This research focuses on the development of a computer aided control system design application which provides a full range of stability analysis and control design capabilities for aerospace vehicles
Some means of combining both computer simulation and anlytical techniques are indicated in order to ...
This research focused on incorporating stability and control into a multidisciplinary de- sign optim...
This thesis is concerned with the application of computer-aided design to classical control theory. ...
The development of an advanced, computerized method for the analysis and evaluation of the aeroelast...
This paper describes the Rapid Aircraft DynamIcs AssessmeNt (RADIAN) project - an integration of the...
A Computer Aided Engineering (CAE) tool has been developed for the design of flight control and hydr...
The present study tackles the broad range of research activities seeking to provide theoretical foun...
Computer Aided Control Engineering involves three parallel streams: Simulation and modelling, Contro...
Control System Design methods are presented in terms of optimization techniques that incorporate Mu...
Includes bibliography.Successful multivariable control system design demands knowledge, skill and cr...
Flight control system design typically involves hardware and software development, requiring the def...
Computationally useful algorithms are considered that can aid the control engineer in designing syst...
The results of studies which were undertaken to contribute to the design of digital flight control s...
A computer assisted conceptual aircraft design program has been developed (CACAD). It has an optimi...
Research aircraft have become increasingly dependent on advanced control systems to accomplish progr...
Some means of combining both computer simulation and anlytical techniques are indicated in order to ...
This research focused on incorporating stability and control into a multidisciplinary de- sign optim...
This thesis is concerned with the application of computer-aided design to classical control theory. ...
The development of an advanced, computerized method for the analysis and evaluation of the aeroelast...
This paper describes the Rapid Aircraft DynamIcs AssessmeNt (RADIAN) project - an integration of the...
A Computer Aided Engineering (CAE) tool has been developed for the design of flight control and hydr...
The present study tackles the broad range of research activities seeking to provide theoretical foun...
Computer Aided Control Engineering involves three parallel streams: Simulation and modelling, Contro...
Control System Design methods are presented in terms of optimization techniques that incorporate Mu...
Includes bibliography.Successful multivariable control system design demands knowledge, skill and cr...
Flight control system design typically involves hardware and software development, requiring the def...
Computationally useful algorithms are considered that can aid the control engineer in designing syst...
The results of studies which were undertaken to contribute to the design of digital flight control s...
A computer assisted conceptual aircraft design program has been developed (CACAD). It has an optimi...
Research aircraft have become increasingly dependent on advanced control systems to accomplish progr...
Some means of combining both computer simulation and anlytical techniques are indicated in order to ...
This research focused on incorporating stability and control into a multidisciplinary de- sign optim...
This thesis is concerned with the application of computer-aided design to classical control theory. ...