HARDWARE-IN-THE-LOOP GROUND SIMULATION OF SPACECRAFT ATTITUDE CONTROL SUBSYSTEM

碩士 === 國立成功大學 === 航空太空工程學系 === 82 === This research prsents some analysis and comparison of the attitude stabilization control methods for a low-earth orbit satellite by using personal computer controlled simple equipment and hardware setup. In this paper...

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Bibliographic Details
Main Authors: YONG-LIN KUO, 郭永麟
Other Authors: YIING-YUH LIN
Format: Others
Language:zh-TW
Published: 1994
Online Access:http://ndltd.ncl.edu.tw/handle/49571269478703166505