| 標題: | 反飛彈導引設計及軌跡最佳化之研究（含終端限制及系統不確定因素） |
| 作者: | 廖德誠 LIAW DER-CHERNG 交通大學電機與控制工程系 |
| 關鍵字: | 反飛彈導引;軌跡最佳化;Anti-missile guidance;Trajectory optimization |
| 公開日期: | 2000 |
| 官方說明文件#: | NSC89-CS-D009-013 |
| URI: | http://hdl.handle.net/11536/89122 https://www.grb.gov.tw/search/planDetail?id=542796&docId=99772 |
| Appears in Collections: | Research Plans |
- 可變結構系統理論在飛彈導引律設計上之應用 / 陳永平;CHEN YON-PING
- Design of Missile Mid-Course Guidance for Constrained Impact Angle / Chen, B. H.;Chen, T. L.
- 飛彈攔截機動目標之導引律設計 / 盧健勝;Chien-Sheng Lu;陳永平;Dr. Yon-Ping Chen
- 智慧型導引技術(II) / 梁耀文;LIANG YEW-WEN
- Design of Midcourse Guidance Laws via a Combination of Fuzzy and SMC Approaches / Chen, Chun-Hone;Liang, Yew-Wen;Liaw, Der-Cherng;Chang, Shih-Tse;Xu, Sheng-Dong
- Self-organizing fuzzy learning CLOS guidance law design / Lin, CM;Hsu, CF;Mon, YJ
- Intelligent Missile Guidance by Using Adaptive Recurrent Neural Networks / Wang, Chi-Hsu;Chen, Chun-Yao
- Intelligent Adaptive Law for Missile Guidance Using Fuzzy Neural Networks / Wang, Chi-Hsu;Hung, Kun-Neng
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