Utilize este identificador para referenciar este registo: http://hdl.handle.net/10400.6/3648
Título: Roll motion control of a dissymmetrical wingspan aircraft
Autor: Tavares, Filipe Miguel Tanqueiro .
Orientador: Bousson, Kouamana
Gamboa, Pedro
Palavras-chave: Aeronave
Controlador de aeronave - Asa dissimétrica
Controlador de aeronave - Envergadura variável
Controlador robusto
Controlo do rolamento
Controlador Batz-Kleinman
Data de Defesa: 2011
Resumo: The present study focuses on the design of a controller for an unmanned aircraft using a variable-span dissymmetric system. This is primarily intended to stabilize roll, although it was designed as a robust system for total control. The system in use is new in its application, being studied similar aircraft built to date. The aircraft for which the system has been designed is an experimental UAV built entirely at the University of Beira Interior. The stability derivatives and other data were obtained with the help of XFLR software. The development and simulation were done using MATLAB, where were tested two different control methods, LQR and Batz-Kleinman controller. A review of the flight dynamics equations for a standard aircraft was originally done, being then adapted this new concept. The interaction between the control surfaces and the response of a general aircraft was studied. An implementation of predetermined flying qualities in order to scale the state weight matrix in the LQR controller for optimal levels was also performed. At the end three separate simulations were performed to confirm the validity of the theoretical system in control and stabilization, for leveled flight when suffering disturbances, and for various equilibrium states described by a sinusoidal equation and a random variation.
URI: http://hdl.handle.net/10400.6/3648
Designação: Dissertação apresentada à Universidade da Beira Interior para a obtenção do grau de mestre em Engenharia Aeronáutica
Aparece nas colecções:FE - DCA | Dissertações de Mestrado e Teses de Doutoramento

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Roll Motion Control of a Dissymmetrical Wingspan Aircraft.pdf12,42 MBAdobe PDFVer/Abrir


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