Hybrid adaptive control of a dragonfly model

Dragonflies show unique and superior flight performances than most of other insect species and birds. They are equipped with two pairs of independently controlled wings granting an unmatchable flying performance and robustness. In this paper, it is presented an adaptive scheme controlling a nonlinear model inspired in a dragonfly-like robot. It is proposed a hybrid adaptive (HA) law for adjusting the parameters analyzing the tracking error. At the current stage of the project it is considered essential the development of computational simulation models based in the dynamics to test whether strategies or algorithms of control, parts of the system (such as different wing configurations, tail) as well as the complete system. The performance analysis proves the superiority of the HA law over the direct adaptive (DA) method in terms of faster and improved tracking and parameter convergence.

Application of fractional algorithms in the control of a robotic bird

In this paper, it is studied the dynamics of the robotic bird in terms of time response and robustness. It is analyzed the wing angle of attack and the velocity of the bird, the tail influence, the gliding flight and the flapping flight. The results are positive for the construction of flying robots. The development of computational simulation based on the dynamic of the robotic bird should allow testing strategies and different algorithms of control such as integer and fractional controllers.

Projeto, Desenvolvimento e implementação de um Robô Voador de Inspiração Biológica

Este trabalho consiste no projeto, desenvolvimento e implementação de uma máquina voadora de inspiração biológica. Para a sua construção, é elaborado um estudo do voo nos seres biológicos de forma a obter alguma informação para o seu dimensionamento e é elaborada uma análise de projetos que utilizem as mesmas características de voo. Com os dados recolhidos neste estudo, é elaborado o projeto da máquina. Numa última fase, com recurso a materiais leves, é implementada uma máquina capaz de exercer as forças envolvidas no voo, força de propulsão e força de sustentação, e são elaborados estudos a fim de perceber quais os pontos fortes e os pontos fracos da mesma.