A full-space quasi Lagrange-Newton-Krylov algorithm for trajectory optimization problems with space mission
碩士 === 國立中央大學 === 數學系 === 105 === The trajectory optimization is a commonly-used technique of applications in aerospace engineering, such as find the optimal trajectory to maximize the weight of the payload or minimize the time for satellite insertion the target orbit, etc. This type of problem can...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2017
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| Online Access: | http://ndltd.ncl.edu.tw/handle/gnm4x4 |