| 標題: | 飛彈攔截及小行星登陸問題之研究 A study of missile interception and spacecraft landing on an asteroid |
| 作者: | 林輝巨 Lin, Hui Ju 廖德誠 Liao, De Cheng 電控工程研究所 |
| 公開日期: | 1994 |
| URI: | http://140.113.39.130/cdrfb3/record/nctu/#NT832327023 http://hdl.handle.net/11536/59742 |
| Appears in Collections: | Thesis |
- 飛彈攔截與小行星登陸之非線性導引控制 / 張欽亮;Chang, Chin-Liang;廖德誠;Der-Cherng Liaw
- 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
- Variable structure control scheme for landing on a celestial object / Liaw, DC;Cheng, CC
- Intelligent Adaptive Law for Missile Guidance Using Fuzzy Neural Networks / Wang, Chi-Hsu;Hung, Kun-Neng
- 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
- 智慧型雷達預估器於追蹤高速運動目標之研究 / 陳一元;Yi-Yuan Chen;楊谷洋;kuu-Young Young
- 攔截飛彈複合控制系統設計 / 劉宇晉;LIU, YU-CHIN;林清安;LIN, CING-AN
- Design of Missile Mid-Course Guidance for Constrained Impact Angle / Chen, B. H.;Chen, T. L.
Loading...