Controle de posição com restrição à orientação de um Veículo Aéreo Não-Tripulado tipo Quadrirrotor
Quadrotors aircraft are composed by four propellers mounted on four engines on a cross or x disposition, and, in this structure, the engines on the same arm spin in the same direction and the other arm in the opposite direction. By rotating each helix generates vertical upward thrust. The control is...
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| פורמט: | Dissertação |
| שפה: | por |
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Universidade Federal do Rio Grande do Norte
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| גישה מקוונת: | https://repositorio.ufrn.br/jspui/handle/123456789/15493 |
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