31th Congress of the International Council of the Aeronautical Sciences

01 - Aircraft Design and Integrated Systems

DEVELOPMENT OF A COMPREHENSIVE ANALYSIS AND OPTIMIZED DESIGN FRAMEWORK FOR THE MULTIROTOR UAV

H. Kim¹, D. Lim¹, K. Yee¹; ¹Seoul National University, South Korea

It is necessary to establish the systematic design procedure of the multirotor UAV with the aim of accomplishing its mission profile. Analysis of the framework comprises one estimation and four analyzers: they are 1)weight estimation [1], 2)attitude, 3)structure, 4)aerodynamics, and 5)electric system analysis.


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