Integrated Aircraft Robust Output Feedback Sliding Mode Autopilot and Guidance System Design
碩士 === 遠東科技大學 === 機械工程研究所 === 100 === The sliding mode control has developed for years. It can be applied in various situations, for example, ship controls or aircraft controls. This thesis develops a new chattering-free sliding mode control method. The output feedback is used to control the flight...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/44480151039738883549 |