Novel Controller Design for Missiles to Intercept Maneuvering Target
碩士 === 國立臺灣大學 === 電機工程學研究所 === 95 === The decision part in missiles: guidance law and autopilot system is presented in this thesis. The guidance law is designed with linear differential game theory in order to consider the motion of target and to minimize the distance between the missile and the tar...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2007
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| Online Access: | http://ndltd.ncl.edu.tw/handle/93827697318932952514 |