Control Stabilization of Double-Link Inverted Pendulum System Using the Coefficient Diagram Method
碩士 === 國立成功大學 === 航空太空工程學系 === 87 === Because of the consideration of drag and environment, changing the direction of the engine nozzle controlled the flight direction of the rocket. The concept of the inverted pendulum system is generated from this. The inverted pendulum system is an uns...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1999
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| Online Access: | http://ndltd.ncl.edu.tw/handle/35565367203997411994 |