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...

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Bibliographic Details
Main Authors: Sapunkov, Yakov Grigor'evich, Molodenkov, Alexei Vladimirovich
Format: Article
Language:English
Published: Saratov State University 2023-03-01
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