title: Controlling the orbital motion of the spacecraft near the libration point by changing the solar sail reflectivity
metadata.name: dc.contributor.author
metadata.value: Shmyrov, Alexander S.
metadata.lang: -
metadata.name: dc.contributor.author
metadata.value: Shmyrov, Vasiliy A.
metadata.lang: -
metadata.name: dc.contributor.author
metadata.value: Shymanchuk, Dmitry V.
metadata.lang: -
metadata.name: dc.date.accessioned
metadata.value: 2024-08-19T21:27:36Z
metadata.lang: -
metadata.name: dc.date.available
metadata.value: 2024-08-19T21:27:36Z
metadata.lang: -
metadata.name: dc.date.issued
metadata.value: 2024-06
metadata.lang: -
metadata.name: dc.identifier.citation
metadata.value: Shmyrov A. S., Shmyrov V. A., Shymanchuk D. V. Controlling the orbital motion of the spacecraft near the libration point by changing the solar sail reflectivity. Vestnik of Saint Petersburg University. Applied Mathematics. Computer Science. Control Processes, 2024, vol. 20, iss. 2, pp. 298–306. https://doi.org/10.21638/spbu10.2024.214 (In Russian)
metadata.lang: en_GB
metadata.name: dc.identifier.other
metadata.value: https://doi.org/10.21638/spbu10.2024.214
metadata.lang: -
metadata.name: dc.identifier.uri
metadata.value: http://hdl.handle.net/11701/47275
metadata.lang: -
metadata.name: dc.description.abstract
metadata.value: The article considers the strategy of keeping the spacecraft in the vicinity of the unstable
  Lagrange point (libration point) of the Sun Earth system. This strategy involves the use
  of special management. This control acts collinearly to the Sun Earth line and ensures
  Lyapunov stability of the orbital motion. The implementation of such control is proposed
  using a solar sail. The advantages and difficulties of such a strategy are discussed.
metadata.lang: en_GB
metadata.name: dc.description.sponsorship
metadata.value: This research was supported by Saint Petersburg State University, project N 95438429.
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. Applied Mathematics. Computer Science. Control Processes;Volume 20; Issue 2
metadata.lang: -
metadata.name: dc.subject
metadata.value: three bodies problem
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: libration point
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: solar sail
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: control
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: keeping
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: machine learning
metadata.lang: en_GB
metadata.name: dc.title
metadata.value: Controlling the orbital motion of the spacecraft near the libration point by changing the solar sail reflectivity
metadata.lang: en_GB
metadata.name: dc.type
metadata.value: Article
metadata.lang: en_GB
resources.filename: vestnik_spbu10_2024_298.pdf
resources.url: https://dspace.spbu.ru/bitstream/11701/47275/1/vestnik_spbu10_2024_298.pdf
resources.format: Adobe PDF
resources.size: 552,11 kB