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An approach to reduce vibration and avoid shimmy on landing gears based on an adapted eigenstructure assignment theory
(2020-01-01)
Landing gear shimmy is a self excited vibration phenomenon which must be avoided during aircraft design due to its potentially catastrophic behaviour. In a preliminary specification of structural properties of a landing ...
Parallel Genetic Algorithm Fitness Function Team For Eigenstructure Assignment Via Lqr Designs
(IEEE Computer Society, 1999)
Rule-based Decision-making Unit For Eigenstructure Assignment Via Parallel Genetic Algorithm And Lqr Designs
(IEEE, Piscataway, NJ, United States, 2000)
Parallel Eigenstructure Assignment Via Lqr Design And Genetic Algorithms
(IEEE, Piscataway, NJ, United States, 1999)
Ultimate bound minimisation by state feedback in discrete-time switched linear systems under arbitrary switching
(Elsevier, 2016-08)
We present a novel state feedback design method for perturbed discrete-time switched linear systems. The method aims at achieving (a) closed-loop stability under arbitrary switching and (b) minimisation of ultimate bounds ...
Construção, instrumentação e controle de um bola viga modificado utilizando controle seguidor com realimentação de estados e atribuição de autoestrutura completa em tempo real
(Universidade Tecnológica Federal do ParanáCornelio ProcopioBrasilPrograma de Pós-Graduação em Engenharia MecânicaUTFPR, 2016-09-19)
This dissertation presents the construction, instrumentation and control of a modify ball and beam system, using tracking control with state feedback and complete eigenstructure assignment. In the present contribution, an ...
Desenvolvimento de um laboratório virtual e remoto para controle de um helicóptero com três graus de liberdade
(Universidade Tecnológica Federal do ParanáCornelio ProcopioBrasilPrograma de Pós-Graduação em Engenharia MecânicaUTFPR, 2020-04-03)
This thesis presents the development of a virtual and remote laboratory (VRL) for the control of a 3 degrees of freedom (DOF) Helicopter. This is a mechanical system to study the dynamics of an aircraft with parallel ...
Prototipagem virtual, simulação e controle de um quadrirotor utilizando controle seguidor com atribuição de autoestrutura completa
(Universidade Tecnológica Federal do ParanáCornelio ProcopioBrasilPrograma de Pós-Graduação em Engenharia MecânicaUTFPR, 2017-06-01)
This dissertation presents the development of a tracking control system, with state feedback, for a didactic plan of a quadrirotor constituted of four rotors arranged in a cross shape. The dynamics system is nonlinear and ...