The new algorithm of quasi-optimal reorientation of a spacecraft
The classical problem of optimal control of the attitude maneuver of a spacecraft as a rigid body of arbitrary dynamic configuration under arbitrary boundary conditions for the angular position and angular velocity of a spacecraft without restriction on the control vector function and with a fixed t...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
Saratov State University
2023-03-01
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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/text-pdf/2023/02/95-112-sapunkov-molodenkov.pdf |