The Study of Appling Support Vector Machines to the Missile Control System-Take Roll for Example
碩士 === 國防大學理工學院 === 兵器系統工程碩士班 === 101 === This thesis used missile flying control theory to define six-degree of freedom, three-coordinate system, and rolling motion equations for missile maneuvering and used traditional PID controller for analyzing the results by gaining and out response. At last,...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2013
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| Online Access: | http://ndltd.ncl.edu.tw/handle/58203466331108373757 |