Minimum-Time Interception with an Un-powered Flight Vehicle
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === In general, the boosting time of a solid-fuel rocket is very short. Therefore, it may be considered as an unpowered glider for the most part of its flight time. In this paper, the optimal control theory is applied to analyze the optimal flight trajectory of mini...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/33173513568891145700 |