Modeling and control of a tiltrotor unmanned aerial vehicle for path tracking

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Modeling and control of a tiltrotor unmanned aerial vehicle for path tracking

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dc.contributor Universidade Federal de Santa Catarina pt_BR
dc.contributor.advisor Becker, Leandro Buss pt_BR
dc.contributor.author Donadel, Rodrigo pt_BR
dc.date.accessioned 2016-02-09T03:01:12Z
dc.date.available 2016-02-09T03:01:12Z
dc.date.issued 2015 pt_BR
dc.identifier.other 337437 pt_BR
dc.identifier.uri https://repositorio.ufsc.br/xmlui/handle/123456789/158766
dc.description Dissertação (mestrado) - Universidade Federal de Santa Catarina, Centro Tecnológico, Programa de Pós-Graduação em Engenharia de Automação e Sistemas, Florianópolis, 2015. pt_BR
dc.description.abstract Abstract : This master thesis deals with the modeling and control of a small scale birotor tiltrotor unmanned aerial vehicle (UAV). A tiltrotor is characterized by a mechanism that tilts the aircraft's rotors in order to control the flight. An UAV with such characteristics is being developed by this author and other researchers in the scope of the project named ProVANT. The developed UAV prototype is used in this work to obtain experimental results. This kind of system can be characterized by its underactuated, highly nonlinear, and coupled dynamics. Instead of using a dynamic model available in literature, this work proposes a more accurate model considering the UAV as a multibody system. By doing so the tilting angles become generalized coordinates and the tilt mechanism dynamics are naturally added to the model, as well as the coupling between the bodies. The result is an eight degrees of freedom model obtained through Euler-Lagrange formulation. The path tracking problem is solved here with linear optimal controllers for the full model, instead of the classical approach of cascade control for the translation and rotation subsystems. The developed controllers are linear quadratic regulators, a H1 controller and a multiobjective H2=H1 controller, all with LMI formulation. A nonlinear backstepping controller taken from the literature is implemented in order to be compared with the designed controllers. In addition, controllers for the hovering problem are also designed to be used in experiments with ProVANT's tiltrotor. They reduce the complexity of the initial experimental flights, focusing not only in the validation of the control system, but the complete project, including its electronics, mechanical design, and additional software. Such experiments are presented and discussed in details along this work. The work also addresses how flight-related information are gathered and processed. This includes the design of a nonlinear complementary filter for the attitude estimation that works with data acquired from the UAV sensors.<br> pt_BR
dc.format.extent 143 p.| il., grafs., tabs. pt_BR
dc.language.iso eng pt_BR
dc.subject.classification Engenharia de sistemas pt_BR
dc.subject.classification Automação pt_BR
dc.subject.classification Controle automático pt_BR
dc.subject.classification Aeronave não tripulada pt_BR
dc.title Modeling and control of a tiltrotor unmanned aerial vehicle for path tracking pt_BR
dc.type Dissertação (Mestrado) pt_BR
dc.contributor.advisor-co Raffo, Guilherme Vianna pt_BR


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