對具有閃躲操縱性重返載具之攔截導引系統設計
碩士 === 國防大學中正理工學院 === 兵器系統工程研究所 === 90 === In the near future, it will be the tendency that most attacking missiles will be designed to have the evasive maneuvering capability. The intercepting missiles(Anti-missile Missiles)should be developed to counter this target characteristic. Therefore, how t...
Main Authors: | Yu-Cheng Chen, 陳昱丞 |
---|---|
Other Authors: | 宋真堯 |
Format: | Others |
Language: | zh-TW |
Published: |
2002
|
Online Access: | http://ndltd.ncl.edu.tw/handle/54657833638868186944 |
Similar Items
-
攔截超低空目標之飛彈導引控制系統設計
by: HUANG, YI-XUN, et al.
Published: (1993) -
輸入估測法在重返載具彈道估測上之應用與分析
by: HU, NIEN-HSIEN, et al.
Published: (2003) -
利用角動量補償機構於太空飛行載具姿態之近似最佳化導引設計
by: WANG,TING-HUI, et al.
Published: (1990) -
遙控飛行載具飛行控制系統設計方法探討
by: Yu, Guo-Min, et al.
Published: (1987) -
反彈道飛彈攔截軌跡最佳化導引律之研究
by: Chia-Chi Chao, et al.
Published: (2007)