An Approach to Guidance and Control System Design using Genetic Algorithm and Fuzzy Logic Model
碩士 === 逢甲大學 === 自動控制工程學系 === 89 === The proportional navigation guidance law usually guides traditional aerodynamically controlled missiles in the terminal phase. Such design approaches possess little design flexibility on the improvement of engagement performance robustness. A novel appr...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2001
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| Online Access: | http://ndltd.ncl.edu.tw/handle/99542108043943352253 |