A Study of Minimum-Fuel Trajectories by Using a Parametric Optimization Method
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 an aircraft in the atmospheric flight by using a parametric optimization method. In this thesis, the aircraft is assumed to be a particle and the thrust and the load factor the contr...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/92263186522317413639 |