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...

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Podrobná bibliografie

Hlavní autoři:	Ilya Alekseevich Pankratov, Yuriy Nikolaevich Chelnokov, Yakov Grigoryevich Sapunkov
Médium:	Artigo
Jazyk:	Inglês
Vydáno:	Saratov State University 2020-03-01
Edice:	Известия Саратовского университета. Новая серия: Математика. Механика. Информатика
Témata:	spacecraft orbit optimal control quaternion.
On-line přístup:	https://mmi.sgu.ru/sites/mmi.sgu.ru/files/2020/02/93-104pankratov_et_al.pdf
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