The Analysis of Small Unmanned Aircraft Landing Based on Kansei Engineering

• Main Authors: Lin, Chang-Jui, 林昌瑞
• Other Authors: Wang, Jee-Ray
• Format: Others
• Language: zh-TW
• Published: 2014
• Online Access: http://ndltd.ncl.edu.tw/handle/62414898242612974491

碩士 === 建國科技大學 === 自動化工程系暨機電光系統研究所 === 102 === In this study, Kansei engineering methods to analyze the way for the landing of small unmanned aircraft being used, and interviews with experts expert opinion survey conducted to explore traditional wheeled landing with a parachute landing required design considerations, the way the unmanned aircraft landing design concept decision analysis. First, search for relevant information, the use of unmanned aircraft landed 5W1H design ideas for the type of decision to put the elements to identify important factors. Then after using interpretive structural modeling (Interpretive Structure Model-ISM) to resolve a variety of design structure roadmap to LGRA-AHP method consensus optimal structural design assessment strategies through professional who not only got the best design path Sort results identify small unmanned aircraft landing approach path design practical solutions to select the appropriate decisions, design ideas become targets of small unmanned aircraft landing approach.