2002•1st UAV ConferenceRequires access

Design and Flight Test of a Fixed Wing MAV

Hee Hwang, D. Chung, Kwang Joon Yoon, Hoon Cheol Park, Young Lee, Tae Sam Kang

Abstract

In the present paper, development of fixed wing MAV(Micro Air Vehicle) with electric motor system is presented in detail. Electric motor system has been adopted due to its lower noise level than that of engine system. The MAV named “SPOT” has a 15cm wing span, 75g weight. It has successfully flown for 2 minutes at the flight test.

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Key concepts: Fixed wing, Flight test, Wing, Computer science, Test (biology), Aerospace engineering, Engineering, Geology