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TO THE 300TH ANNIVERSARY OF SPSU
Rigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 2
A. A. Tikhonov
St. Petersburg State University, 7-9, Universitetskaya nab., St. Petersburg, 199034, Russian Federation
Abstract:
This article represents the second part of a survey dedicated to the 300th anniversary of Saint Petersburg State University (SPbSU). The article is intended on analysis the scientific achievements of the Saint Petersburg School of Mathematics and Mechanics in the field of rigid body dynamics in the last 50 years. The main attention in the article is paid to theoretical research in the field of uncontrolled and controlled motions of a rigid body
Keywords:
rigid body, spacecraft, artificial Earth satellite, dynamics, attitude motion, attitude control, stabilization, oscillations.
Received: 02.10.2023
Revised: 04.11.2023
Accepted: 09.11.2023
Citation:
A. A. Tikhonov, “Rigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 2”, Vestnik of Saint Petersburg University. Mathematics. Mechanics. Astronomy, 11:2 (2024), 259–302
Linking options:
https://www.mathnet.ru/eng/vspua296 https://www.mathnet.ru/eng/vspua/v11/i2/p259
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Citation in format AMSBIB
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