Using Subspace Method to Identify Aircraft Flying Parameters

碩士 === 國立交通大學 === 電機與控制工程系 === 87 === In this thesis, we discuss the use of subspace identification method on the real time estimation of aircraft parameters under constant and varying flying conditions. We discuss both the lateral and longitudinal flying systems . In lateral flying system , we cons...

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Bibliographic Details
Main Authors: Tiung-Ting Chen, 陳俊廷
Other Authors: Yung-Chun Wu
Format: Others
Language:zh-TW
Published: 1999
Online Access:http://ndltd.ncl.edu.tw/handle/38950213561920660606