Rigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 4

Authors

  • Аlexey А. Tikhonov St. Petersburg State University, 7-9, Universitetskaya nab., St. Petersburg, 199034, Russian Federation

DOI:

https://doi.org/10.21638/spbu01.2024.402

Abstract

This article is a continuation of the survey dedicated to the 300th anniversary of Saint Petersburg State University and is an attempt to analyze the scientific achievements of the St.Petersburg School of Mechanics in the field of rigid body dynamics. This, the fourth part of the review, is devoted to studies of the dynamics of the uncontrolled motion of a charged rigid body in the gravitational and magnetic fields of the Earth.

Keywords:

rigid body, spacecraft, artificial Earth satellite, dynamics, attitude motion, attitude control, stabilization, oscillations, Lorentz torque

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Published

2024-12-28

How to Cite

Tikhonov А. А. (2024). Rigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 4. Vestnik of Saint Petersburg University. Mathematics. Mechanics. Astronomy, 11(4), 627–662. https://doi.org/10.21638/spbu01.2024.402

Issue

Vol. 11 No. 4 (2024)

Section

To the 300th anniversary of SPSU

License

Articles of "Vestnik of Saint Petersburg University. Mathematics. Mechanics. Astronomy" are open access distributed under the terms of the License Agreement with Saint Petersburg State University, which permits to the authors unrestricted distribution and self-archiving free of charge.