Stability Flight Control and Verification on Hybrid Powered Multi-Rotor System

碩士 === 國立成功大學 === 航空太空工程學系 === 104 === The development of multi-rotor system has been improved and applied to various applications. However, with constraints on battery and motor, the performance of multi-rotor system is limited in payload and flight endurance. The limitations are solved by introduc...

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Bibliographic Details
Main Authors: Kai-TiJhuang, 莊凱堤
Other Authors: Chin E. Lin
Format: Others
Language:en_US
Published: 2016
Online Access:http://ndltd.ncl.edu.tw/handle/862xep