title: Rigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 2
metadata.name: dc.contributor.author
metadata.value: Tikhonov, Аlexey А.
metadata.lang: -
metadata.name: dc.date.accessioned
metadata.value: 2024-07-04T12:05:20Z
metadata.lang: -
metadata.name: dc.date.available
metadata.value: 2024-07-04T12:05:20Z
metadata.lang: -
metadata.name: dc.date.issued
metadata.value: 2024-06
metadata.lang: -
metadata.name: dc.identifier.citation
metadata.value: Tikhonov А.А. 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, 2024, vol. 11 (69), issue 2, pp. 259–302. https://doi.org/10.21638/spbu01.2024.203 (In Russian)
metadata.lang: en_GB
metadata.name: dc.identifier.other
metadata.value: https://doi.org/10.21638/spbu01.2024.203
metadata.lang: -
metadata.name: dc.identifier.uri
metadata.value: http://hdl.handle.net/11701/45693
metadata.lang: -
metadata.name: dc.description.abstract
metadata.value: 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.
metadata.lang: en_GB
metadata.name: dc.language.iso
metadata.value: ru
metadata.lang: en_GB
metadata.name: dc.publisher
metadata.value: St Petersburg State University
metadata.lang: en_GB
metadata.name: dc.relation.ispartofseries
metadata.value: Vestnik of St Petersburg University. Mathematics. Mechanics. Astronomy;Volume 11 (69); Issue 2
metadata.lang: -
metadata.name: dc.subject
metadata.value: rigid body
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: spacecraft
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: artificial Earth satellite
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: dynamics
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: attitude motion
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: attitude control
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: stabilization
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: oscillations
metadata.lang: en_GB
metadata.name: dc.title
metadata.value: Rigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 2
metadata.lang: en_GB
metadata.name: dc.type
metadata.value: Article
metadata.lang: en_GB
resources.filename: 259-302.pdf
resources.url: https://dspace.spbu.ru/bitstream/11701/45693/1/259-302.pdf
resources.format: Adobe PDF
resources.size: 658,35 kB