A Study on Aerodynamic Model Applied to Aiding Inertial Navigation System

碩士 === 中原大學 === 資訊工程研究所 === 83 === The main object of this paper describes a way to improve the precision of a hybrid inertial navigation system (INS) with aerodynamic model . A primitive hybird INS take advantage of global positio...

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Bibliographic Details
Main Authors: Chen ,Feng-Heng, 陳豐亨
Other Authors: T.M. Hsieh ; Jeng-Heng Chen
Format: Others
Language:zh-TW
Published: 1995
Online Access:http://ndltd.ncl.edu.tw/handle/86097435053893601461