Quaternion Models and Algorithms for Solving the General Problem of Optimal Reorientation of Spacecraft Orbit
The problem of optimal reorientation of the spacecraft orbit is considered in quaternion formulation. Control (vector of the acceleration of the jet thrust) is limited in magnitude. To solve the problem it is required to determine the optimal orientation of this vector in space. It is necessary to m...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Saratov State University
2020-03-01
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| Series: | Известия Саратовского университета. Новая серия. Серия Математика. Механика. Информатика |
| Subjects: | |
| Online Access: | https://mmi.sgu.ru/sites/mmi.sgu.ru/files/2020/02/93-104pankratov_et_al.pdf |