Development of co-axial Y6-Rotor UAV - design, mathematical modeling, rapid prototyping and experimental validation

@article{Czyba2015DevelopmentOC,
  title={Development of co-axial Y6-Rotor UAV - design, mathematical modeling, rapid prototyping and experimental validation},
  author={Roman Czyba and Grzegorz Szafranski and Marcin Janik and Krzysztof Pampuch and Michal Hecel},
  journal={2015 International Conference on Unmanned Aircraft Systems (ICUAS)},
  year={2015},
  pages={1102-1111}
}
This paper outlines development process of Y6-Rotor Micro UAV, which consists of concept of motion, modeling of the vehicle dynamics, rapid prototyping of the mechanics and finally practical realization of the VTOL. This paper presents a micro air vehicle designed to participate in the 2014 International Micro Air Vehicle Conference and Flight Competition (IMAV). Designed mechanical structure may also be referred to as a co-axial tri-rotor UAV, because has two rotors installed on each rotor… CONTINUE READING

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