Genetic algorithm for minimizing the energy costs for the reorientation of the plane of the spacecraft orbit
In the quaternion formulation, the problem of optimal reorientation of the orbital plane of a spacecraft (SC) is considered. The control (acceleration from the vector of the jet thrust orthogonal to the plane of the orbit) is limited in magnitude. It is necessary to minimize energy costs for the reo...
保存先:
| 第一著者: | |
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| フォーマット: | Artigo |
| 言語: | Alemão |
| 出版事項: |
Academician I.G. Petrovskii Bryansk State University
2017-09-01
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| シリーズ: | Научно-технический вестник Брянского государственного университета |
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| オンライン･アクセス: | http://ntv-brgu.ru/wp-content/arhiv/2017-N3/2017-03-11.pdf |
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