Add to ORKGThe aim of this work is to develop an effective numerical tool oriented to optimization of stabilizer parameters according to different criteria that appear in engineering practice. We formulate a special optimization problem that allows us to determine optimal parameters of a stabilizer. The obtained results are applied to choose parameters of a spacecraft stabilization system. We discuss the choice of optimization criteria comparing the degree of stability objective function, the H _inf norm of the system transfer matrix, and the minimal “peak” criterion.Portuguese National Strategic Reference Framework (QREN)Fundação para a Ciência e a Tecnologia (FCT)European Regional Development Fund (FEDER)Portuguese Operational Programme for Competi...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
The objective of this contract was to develop mathematical algorithms for the integration of structu...
Two problems are presented in the area of optimal control and its application to the design of attit...
This work deals with numerical methods of parameter optimization for asymptotically stable systems....
This work deals with numerical methods of parameter optimization for asymptotically stable systems. ...
Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction...
The attitude control of a spacecraft using magnetorquers can be achieved by a feedback control law w...
In this paper the adaption of the software environment ’Multi-Objective Parameter Synthesis’ (MOPS) ...
The attitude stabilization of a spacecraft that uses magnetorquers as torque actuators is a very imp...
Abstract: Dynamics of a gravitational system satellite-stabilizer is studied. It is assume...
The numerical operations involved in a currently used optimization technique are discussed and analy...
Formal optimization methods and eigenvalue gradient information are used to develop a stabilizing co...
The spacecraft formation control problem sets high demands to the performance, especially with respe...
ABSTRACT: This paper describes an optimization procedure to design a minimum weight structure and op...
Computationally useful algorithms are considered that can aid the control engineer in designing syst...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
The objective of this contract was to develop mathematical algorithms for the integration of structu...
Two problems are presented in the area of optimal control and its application to the design of attit...
This work deals with numerical methods of parameter optimization for asymptotically stable systems....
This work deals with numerical methods of parameter optimization for asymptotically stable systems. ...
Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction...
The attitude control of a spacecraft using magnetorquers can be achieved by a feedback control law w...
In this paper the adaption of the software environment ’Multi-Objective Parameter Synthesis’ (MOPS) ...
The attitude stabilization of a spacecraft that uses magnetorquers as torque actuators is a very imp...
Abstract: Dynamics of a gravitational system satellite-stabilizer is studied. It is assume...
The numerical operations involved in a currently used optimization technique are discussed and analy...
Formal optimization methods and eigenvalue gradient information are used to develop a stabilizing co...
The spacecraft formation control problem sets high demands to the performance, especially with respe...
ABSTRACT: This paper describes an optimization procedure to design a minimum weight structure and op...
Computationally useful algorithms are considered that can aid the control engineer in designing syst...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
The objective of this contract was to develop mathematical algorithms for the integration of structu...
Two problems are presented in the area of optimal control and its application to the design of attit...