[논문]Flight test of flying-wing type unmanned aerial vehicle with partial wing-loss

Kim, Kijoon; Kim, Seungkeun; Suk, Jinyoung; Ahn, Jongmin; Kim, Nakwan; Kim, Byoung-Soo

doi:10.1177/0954410018758497

Flight test of flying-wing type unmanned aerial vehicle with partial wing-loss

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, v.233 no.5, 2019년, pp.1611 - 1628

Kim, Kijoon (Dependable CPS Research Department, Infra Core Software Technology Research Division, SW Content Research Laboratory, Electronics and Telecommunications Research Institute (ETRI), Daejeon, Korea) , Kim, Seungkeun (Department of Aerospace Engineering, Chungnam National University, Daejeon, Korea) , Suk, Jinyoung (Department of Aerospace Engineering, Chungnam National University, Daejeon, Korea) , Ahn, Jongmin (Department of Flight Control and Avionics, Agency for Defense Development, Daejeon, Korea) , Kim, Nakwan (Department of Naval Architecture and Ocean Engineering, Seoul National University, Seoul, Korea) , Kim, Byoung-Soo (Department of Aerospace and System Engineering, Gyeongsang National University, Jinju, Korea)

Abstract ▼ AI-Helper

This paper investigates experimental evaluation via flight tests for applying adaptive neural network controller to a flying-wing type unmanned aerial vehicle experiencing partial wing-loss. For this, six-degree-of-freedom numerical model is constructed taking into account damage-induced changes to the unmanned aerial vehicle in aerodynamic coefficients, mass, center of gravity, and moments of inertia. Numerical simulations are performed to investigate the flight dynamics change and to verify the performance of the neural network based controller. During the flight test, main wing-loss is artificially generated by 22% or 33% area moment. The flight test verifies that the damaged unmanned aerial vehicle shows drastic roll behavior with the unstable longitudinal response, and the neural network based adaptive controller combined with feedback linearization successfully compensates for the wing damage.

참고문헌 (8)

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상세보기
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상세보기
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Flight test of flying-wing type unmanned aerial vehicle with partial wing-loss

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Flight test of flying-wing type unmanned aerial vehicle with partial wing-loss

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