Guidance and Control Systems Design for Anti-Ballistic-Missile Missiles with Lateral Jets
碩士 === 國立臺灣大學 === 電機工程學研究所 === 88 === This thesis discusses the guidance and control system design problem for missiles with high controllability and accuracy. Assume that there is a target ballistic missile (the target) moving very fast inside the atmosphere, and an anti-ballistic-missile missile...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/01223011414979502661 |