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...
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| Main Author: | Pankratov I.A. |
|---|---|
| Format: | Article |
| Language: | deu |
| Published: |
Academician I.G. Petrovskii Bryansk State University
2017-09-01
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| Series: | Научно-технический вестник Брянского государственного университета |
| Subjects: | |
| Online Access: | http://ntv-brgu.ru/wp-content/arhiv/2017-N3/2017-03-11.pdf |
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