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...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/80607878946802733385 |