preview

Prototyping Approach For Design Analysis And Testing Of Unmanned Vtol UAV

Decent Essays

Aktas, Y. O., Ozdemir, U., Dereli, Y., Tarhan, A. F., Cetin, A., Vuruskan, A. . . . Inalhan, G. (2014, May). A low cost prototyping approach for design analysis and flight testing of the TURAC VTOL UAV. Paper presented at the International Conference on Unmanned Aircraft Systems (ICUAS), Orlando, FL. http://dx.doi.org/10.1109/ICUAS.2014.6842354 Presented at the 2014 International Conference on Unmanned Aircraft Systems (ICAUS), this paper identifies the need for a low cost approach that is effective in building commercial based small unmanned VTOLs. The researchers’ discuss and analyze the TURAC, which is an easily reproduced tilt rotor VTOL. The paper details the design, manufacturing process, and platform architecture of the TURAC. …show more content…

The paper also presented a design which reduces the number of actuators compared to more traditional models. Since this design configuration suggests newer development strategies, further comparison research is necessary to develop an optimal baseline configuration. Research considerations also need to include under what conditions the platform will be operating and overall objectives. Muranoka, K., Okada, N., & Kubo, D. (2009, April). Quad tilt wing VTOL UAV: Aerodynamic characteristics and prototype flight test. Paper presented at AIAA Infotech Aerospace Conference, Seattle, WA.. Retrieved from https://arc-aiaa-org.ezproxy.libproxy.db.erau.edu/doi/pdf/10.2514/6.2009-1834 This paper was written to describe an unmanned quad tilt wing VTOL which is capable of both efficient hover and forward cruise performance. The researchers’ goal is to design and build a small prototype to demonstrate the operational capabilities and applications of such a design throughout all phases of flight. Extensive wind tunnel testing was conducted to determine the optimal aerodynamic characteristics needed for a quad tilt-wing VTOL UAS. The results of research and testing validated the authors’ concept but further development is required in the areas of flight control and wind configurations. This paper supports further research into the concept of VTOL UAS because the proof of concept was validated through actual flight testing. Stable flight was achieved throughout all

Get Access