Design and Implementation of GPS/INS Integrated System Initial Alignment

碩士 === 淡江大學 === 航空太空工程學系碩士班 === 94 === The thesis is dealing with the problem of initial alignment of INS/GPS integrated system; and in flight calibration of position, speed, and attitude. The basic structure of the integrated system is treating the navigation data from inertial navigation system as...

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Bibliographic Details
Main Authors: Cheng-Kai Lee, 李正凱
Other Authors: Der-Ming Ma
Format: Others
Language:zh-TW
Published: 2006
Online Access:http://ndltd.ncl.edu.tw/handle/96621816128529247314