Based on the Target Trajectory Estimator to Design Anti-Ballistic Missile Guidance Law
碩士 === 國防大學理工學院 === 兵器系統工程碩士班 === 104 === Ballistic missile re-entry except with the characteristics of high-speed maneuver, that can also change the flight path according to mission requirements, in order to improve the intercept accuracy and increase the survival ability of warheads and penetratio...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2016
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| Online Access: | http://ndltd.ncl.edu.tw/handle/82849167016637902663 |