Computational modeling of the aerodynamic characteristics and flight mechanics and control of an unmanned aerial vehicle
This thesis outlines the effort in developing an integrated simulation framework for assessing the stability and control characteristics of an Unmanned Aerial Vehicle (UAV). The objectives are to understand flight instabilities experienced by the UAV and to propose solutions for the flight stability...
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格式: | Theses and Dissertations |
語言: | English |
出版: |
2010
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在線閱讀: | https://hdl.handle.net/10356/41778 |
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機構: | Nanyang Technological University |
語言: | English |