Design of Separate Lift and Thrust Hybrid UAV

Puspita Triana Dewi, Ghozali Suhariyanto Hadi, Muhammad Ramadhan Kusnaedi, Aris Budiyarto, Agus Budiyono

Abstract


Hybrid UAV is a new platform of UAV which is integrating fixed wing and multirotor to get vertical takeoff and landing capability with high range and long endurance. Thus it has the benefit of both fixed wing and multirotor platform. The design methodology of hybrid UAV is resembled fixed wing aircraft with modification at some part due to augmentation of multirotor. This Hybrid UAV has been manufactured and on testing phase.

Keywords


Hybrid; UAV; VTOL; fixed-wing; multirotor

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References


Chung-Hwong Poh, Chung-Kiak Poh, “Radio Controlled SD Aerobatic Airplanes as Basis for Fixed-Wing UAVs with VTOL Capability”, Open Journal of Applied Science, 2014.

Fredericks, William J., “Conceptual Design of A Vertical Takeoff and Landing Unmanned Aerial Vehicle with 24-HR Endurance”, NASA Langley Research Center, Hampton, VA 23681.

Jenkinson, L.R. and Machman, J.F., “Aircraft Design Projects for Engineering Students”, American Institute of Aeronautics and Astronautics, Inc. United State, 2003.

Li, Leon, “Experimental Testing of Low Reynolds Number Airfoil for Unmanned Aerial Vehicle”, University of Toronto, 2013.

McCormick, Barnes W., “Aerodynamics, Aeronautics and Flight Mechanics”, John Wiley & Sons, Inc.United State. 1979.

Meriam, J.L. and Kraige, L.G., “Engineering Mechanics Dynamic”, John Wiley & Sons, Inc. United State. 2003.

Raymer, Daniel P., “Aircraft Design: A Conceptual Approach Fourth Edition”, Virginia Polytechnic Institute and State University. United State. 2006.

Soojung Hwang, Yushin Kim, and Myeong Kyu Lee, “Tilt Rotor-Wing Concept for Multi-Purpose VTOL UAV”, KSAS International Journal, 2008.

Andre, Deperrois, Results vs. Prediction, Presentation document, July 2008,

http://xflr5.sourceforge.net/docs/Results_vs_Prediction.pdf

Andre, Deperrois, Stability and Control Analysis in XFLR 5 v6, Presentation document, September 2010,

http://xflr5.sourceforge.net/docs/XFLR5_and_Stability_analysis.pdf

Mohammad H. Sadraey, (2013) "Optimal control and line‐of‐sight guidance formation flight", International Journal of Intelligent Unmanned Systems, Vol. 1 Iss: 3, pp.228 – 244

Takuma Hino, Takeshi Tsuchiya, (2013) "Heuristic path planning of unmanned aerial vehicle formations", International Journal of Intelligent Unmanned Systems, Vol. 1 Iss: 2, pp.121 – 144

Haoyang Cheng, John Page, John Olsen, (2013) "Cooperative control of UAV swarm via information measures", International Journal of Intelligent Unmanned Systems, Vol. 1 Iss: 3, pp.256 – 275

Yi‐Ren Ding, Yi‐Chung Liu, Fei‐Bin Hsiao, (2013) "The application of extended Kalman filtering to autonomous formation flight of small UAV system", International Journal of Intelligent Unmanned Systems, Vol. 1 Iss: 2, pp.154 – 186

Brenton K. Wilburn, Mario G. Perhinschi, Hever Moncayo, Ondrej Karas, Jennifer N. Wilburn, (2013) "Unmanned aerial vehicle trajectory tracking algorithm comparison", International Journal of Intelligent Unmanned Systems, Vol. 1 Iss: 3, pp.276 – 302

Ghassan Al-Sinbol , Mario G Perhinschi , Brenton K Wilburn , (2015) "Simplified GPS model for UAV fault tolerant control laws design", International Journal of Intelligent Unmanned Systems, Vol. 3 Iss: 1, pp.39 – 60

Brenton K. Wilburn , Mario G. Perhinschi , Jennifer N. Wilburn , (2014) "A modified genetic algorithm for UAV trajectory tracking control laws optimization", International Journal of Intelligent Unmanned Systems, Vol. 2 Iss: 2, pp.58 – 90

Sanketh Ailneni , Sudesh K. Kashyap , N. Shantha Kumar , (2014) "INS/GPS fusion architectures for unmanned aerial vehicles", International Journal of Intelligent Unmanned Systems, Vol. 2 Iss: 3, pp.154 - 167


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