On renormalization of the approximate solution of the orbital coordinate system equations of orientation
In the quaternion formulation, the problem of mathematical modeling of the spacecraft motion in an elliptical orbit is considered. The control is a modulo-limited acceleration vector from the jet thrust, directed orthogonally to the plane of the spacecraft orbit. The motion of the spacecraft center...
| Published in: | Известия Саратовского университета. Новая серия: Математика. Механика. Информатика |
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| Format: | Article |
| Language: | English |
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Saratov State University
2024-08-01
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| Online Access: | https://mmi.sgu.ru/sites/mmi.sgu.ru/files/text-pdf/2024/08/415-422-pankratov.pdf |