Guidance-Control Design and Real-Time Simulation for Tilt-Rotor Aircraft
碩士 === 逢甲大學 === 自動控制工程所 === 98 === The purpose of this research is to accomplish the aerodynamic force and control technology development of VTOL(Vertical Take-off and Landing) and automatic transition for the tilt-rotor aircraft. We have built the mathematic model and control executive system of th...
| 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/20022078854986073126 |