Flight Attitude Simulation for the Model Helicopter

碩士 === 元智大學 === 機械工程學系 === 94 === The purpose of the thesis is to establish a numerical model method for a Raptor 50 V.2 model helicopter. According to the configuration parameters of the model helicopter, the nonlinear and linear mathematical models of the model helicopter, which are the fundamenta...

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Bibliographic Details
Main Authors: Wan-Wen Cheng, 鄭婉彣
Other Authors: 陳傳生
Format: Others
Language:zh-TW
Published: 2006
Online Access:http://ndltd.ncl.edu.tw/handle/61579797613348602445