TY - JOUR

T1 - Rigid-Body Dynamics from the Euler Equations to the Attitude Control of Spacecraft in the Works of Scientists from St. Petersburg State University. Part 3

AU - Tikhonov, A.A.

N1 - Export Date: 21 October 2024 Адрес для корреспонденции: Tikhonov, A.A.; St. Petersburg State UniversityRussian Federation; эл. почта: a.tikhonov@spbu.ru Сведения о финансировании: Russian Science Foundation, RSF, 24-21-00104 Текст о финансировании 1: This work was supported by the Russian Scientific Foundation (project no. 24-21-00104).

PY - 2024/9/1

Y1 - 2024/9/1

N2 - Abstract: This work is a continuation of the review dedicated to the 300th anniversary of St. Petersburg State University (SPbSU) and is an attempt to analyze the scientific achievements of the St. Petersburg School of Mechanics in the field of rigid-body dynamics. This third part of the review is devoted to a fifty-year period ending in 2023. It focuses on applied research carried out by scientists from St. Petersburg State University in the 1970s and devoted to the uncontrolled attitude motion of a rigid body in the gravitational and magnetic fields of the Earth. A significant place among these studies is occupied by the solution of problems related to the passive gravitational stabilization of spacecraft using magnetic interaction to create restoring and damping torques. © Pleiades Publishing, Ltd. 2024. ISSN 1063-4541, Vestnik St. Petersburg University, Mathematics, 2024, Vol. 57, No. 3, pp. 307–321. Pleiades Publishing, Ltd., 2024. Russian Text The Author(s), 2024, published in Vestnik Sankt-Peterburgskogo Universiteta: Matematika, Mekhanika, Astronomiya, 2024, Vol. 11, No. 3, pp. 455–476.

AB - Abstract: This work is a continuation of the review dedicated to the 300th anniversary of St. Petersburg State University (SPbSU) and is an attempt to analyze the scientific achievements of the St. Petersburg School of Mechanics in the field of rigid-body dynamics. This third part of the review is devoted to a fifty-year period ending in 2023. It focuses on applied research carried out by scientists from St. Petersburg State University in the 1970s and devoted to the uncontrolled attitude motion of a rigid body in the gravitational and magnetic fields of the Earth. A significant place among these studies is occupied by the solution of problems related to the passive gravitational stabilization of spacecraft using magnetic interaction to create restoring and damping torques. © Pleiades Publishing, Ltd. 2024. ISSN 1063-4541, Vestnik St. Petersburg University, Mathematics, 2024, Vol. 57, No. 3, pp. 307–321. Pleiades Publishing, Ltd., 2024. Russian Text The Author(s), 2024, published in Vestnik Sankt-Peterburgskogo Universiteta: Matematika, Mekhanika, Astronomiya, 2024, Vol. 11, No. 3, pp. 455–476.

KW - artificial Earth satellite

KW - attitude motion

KW - dynamics

KW - gravitational stabilization

KW - oscillation damping

KW - rigid body

KW - spacecraft

U2 - 10.1134/s1063454124700158

DO - 10.1134/s1063454124700158

M3 - статья

VL - 57

SP - 307

EP - 321

JO - Vestnik St. Petersburg University: Mathematics

JF - Vestnik St. Petersburg University: Mathematics

SN - 1063-4541

IS - 3

ER -