Minimum-fuel Orbit Transfer Between Coplanar Orbits with Continuous Low Thrust Force
碩士 === 國立成功大學 === 航空太空工程學系 === 89 === The purpose of this thesis is to analyze the minimum-fuel trajectory of orbit transfer for a satellite with continuous low thrust force of which the direction is adjustable. Strict nonlinear control theory is used to derive the necessary co...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2001
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| Online Access: | http://ndltd.ncl.edu.tw/handle/97737790479414983444 |