A method by which modern and classical theory techniques may be integrated in a synergistic fashion and used in the design of practical flight control systems is presented. A general procedure is developed, and several illustrative examples are included. Emphasis is placed not only on the synthesis of the design, but on the assessment of the results as well
This report contains the development of a digital outer-loop three dimensional radio navigation (3-D...
New control synthesis procedures for digital flight control systems were developed. The theoretical ...
The development of a comprehensive and electric methodology for conceptual and preliminary design of...
A method by which modern and classical control theory techniques may be integrated in a synergistic ...
Over the last two and a half years we have been demonstrating a new methodology for the design of ro...
Research dealt with the general area of optimal flight control synthesis for manned flight vehicles....
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
Using automatic control theory with simple pilot model for synthesizing helicopter landing approach ...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
This article proposes simultaneous helicopter and control system design and illustrates its advantag...
A control-system design method, Quadratic Optimal Cooperative Control Synthesis (CCS), is applied to...
Theoretical development is reported for the parameter optimization design technique needed for digit...
Cette thèse s'inscrit dans le domaine de l’étude des lois de commandes de vol pour hélicoptères. Les...
A multivariable control design method based on constrained parameter optimization was applied to the...
This report contains the development of a digital outer-loop three dimensional radio navigation (3-D...
New control synthesis procedures for digital flight control systems were developed. The theoretical ...
The development of a comprehensive and electric methodology for conceptual and preliminary design of...
A method by which modern and classical control theory techniques may be integrated in a synergistic ...
Over the last two and a half years we have been demonstrating a new methodology for the design of ro...
Research dealt with the general area of optimal flight control synthesis for manned flight vehicles....
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
Using automatic control theory with simple pilot model for synthesizing helicopter landing approach ...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
This article proposes simultaneous helicopter and control system design and illustrates its advantag...
A control-system design method, Quadratic Optimal Cooperative Control Synthesis (CCS), is applied to...
Theoretical development is reported for the parameter optimization design technique needed for digit...
Cette thèse s'inscrit dans le domaine de l’étude des lois de commandes de vol pour hélicoptères. Les...
A multivariable control design method based on constrained parameter optimization was applied to the...
This report contains the development of a digital outer-loop three dimensional radio navigation (3-D...
New control synthesis procedures for digital flight control systems were developed. The theoretical ...
The development of a comprehensive and electric methodology for conceptual and preliminary design of...