Design of Hybrid Guidance Law for Interception of Ballistic Targets
碩士 === 國立中興大學 === 電機工程學系 === 93 === Part 1 ： Optimal Guidance Design An optimal midcourse guidance law based on the optimal trajectory shaping is analytically developed to create a near head-on interception condition so that an aerodynamically controlled missile is capable of intercepting a ballisti...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/38675008332869087825 |