Minimum-Fuel Trajectory from the Earth Surface to the Orbit
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 92 === The objective of this thesis is to analyze the minimum-fuel trajectory of a three-stage rocket from the earth surface to a designated orbit in order to determine the maximum payload which the rocket can carry.The nonlinear optimal control problem is solved...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/94083833055157159430 |