Control Law Design and Experiment For a Small Coaxial UAV Helicopter
碩士 === 元智大學 === 機械工程學系 === 98 === In this paper, the author has designed and experimented the control law for a small coaxial UAV helicopter. The process starts with identifying the dynamic models for the heading, pitch and roll attitudes of the UAV helicopter. These models are identified by using t...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2010
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| Online Access: | http://ndltd.ncl.edu.tw/handle/70794131036306636560 |