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IJSTR >> Volume 6 - Issue 4, April 2017 Edition



International Journal of Scientific & Technology Research  
International Journal of Scientific & Technology Research

Website: http://www.ijstr.org

ISSN 2277-8616



Design Of Vertical Take-Off And Landing (VTOL) Aircraft System

[Full Text]

 

AUTHOR(S)

Win Ko Ko Oo, Hla Myo Tun, Zaw Min Naing, Win Khine Moe

 

KEYWORDS

VTOL, Dual Copter, Tri Copter, Helicopter, aerodynamic, Vertical take -off and landing and mathematical model.

 

ABSTRACT

Vertical Take Off and Landing Vehicles (VTOL) are the ones which can take off and land from the same place without need of long runway. This paper presents the design and implementation of tricopter mode and aircraft mode for VTOL aircraft system. Firstly, the aircraft design is considered for VTOL mode. And then, the mathematical model of the VTOL aircraft is applied to test stability. In this research, the KK 2.1 flight controller is used for VTOL mode and aircraft mode. The first part is to develop the VTOL mode and the next part is the transition of VTOL mode to aircraft mode. This paper gives brief idea about numerous types of VTOLs and their advantages over traditional aircraftsand insight to various types of tricopter and evaluates their configurations.

 

REFERENCES

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[6] C. ShlokAgarwal,Apoorva Mohan and Kamlesh Kumar,Design, Construction And Structure Analysis OfTwinrotorUAV,Department of Mechatronics, Manipal University, India. Department of Mechatronics, Manipal University, India. Department of Aeronautical and Automobile, Manipal University, India.

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