Return to search

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

Dissertação (mestrado) - Universidade Federal de Santa Catarina, Centro Tecnológico, Programa de Pós-Graduação em Engenharia de Automação e Sistemas, Florianópolis, 2015. / Made available in DSpace on 2016-02-09T03:01:12Z (GMT). No. of bitstreams: 1
337437.pdf: 7414111 bytes, checksum: 2bab6f7b0d4d376f975801166ea73051 (MD5)
Previous issue date: 2015 / 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>

Identiferoai:union.ndltd.org:IBICT/oai:repositorio.ufsc.br:123456789/158766
Date January 2015
CreatorsDonadel, Rodrigo
ContributorsUniversidade Federal de Santa Catarina, Becker, Leandro Buss, Raffo, Guilherme Vianna
Source SetsIBICT Brazilian ETDs
LanguageEnglish
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/publishedVersion, info:eu-repo/semantics/masterThesis
Format143 p.| il., grafs., tabs.
Sourcereponame:Repositório Institucional da UFSC, instname:Universidade Federal de Santa Catarina, instacron:UFSC
Rightsinfo:eu-repo/semantics/openAccess

Page generated in 0.0019 seconds