Investigation of the controllers for thrust-vectoring nozzles and analysis of the parameters on the bandwidth of the nozzles

碩士 === 中華大學 === 機械與航太工程研究所 === 93 === In this study, a thrust-vectoring micro jet engine was analyzed and the horizontal pendulum response was used to validate the engine model. The critical oscillation angle and time delay to the stable operation were used to determine the optimal combination of PI...

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Bibliographic Details
Main Authors: Hsu Tsai-Yuan, 徐才元
Other Authors: 楊一龍
Format: Others
Language:zh-TW
Published: 2005
Online Access:http://ndltd.ncl.edu.tw/handle/80607878946802733385