A Study of Parameters Selection for an Integrated Guidance and Flight Control Autopilot Used in UAV

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 92 ===   A F-16 as the UAV dynamic model and its integrated guidance and flight control autopilot is chosen in this research as the main focus of this study. The objective is to investigate the effect of autopilot parameters to the flight performance of an unmanne...

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Bibliographic Details
Main Authors: Hung-Wei Lin, 林煥巍
Other Authors: Yiing-Yuh Lin
Format: Others
Language:zh-TW
Published: 2004
Online Access:http://ndltd.ncl.edu.tw/handle/65122643883255035998