title: Averaging technique in the problem of satellite attitude stabilization in indirect position in the orbital reference frame with the use of Lorentz torque
metadata.name: dc.contributor.author
metadata.value: Aleksandrov, Aleksandr Yu.
metadata.lang: -
metadata.name: dc.contributor.author
metadata.value: Andriyanova, Natalya R.
metadata.lang: -
metadata.name: dc.contributor.author
metadata.value: Tikhonov, Aleksey A.
metadata.lang: -
metadata.name: dc.date.accessioned
metadata.value: 2021-05-04T19:30:53Z
metadata.lang: -
metadata.name: dc.date.available
metadata.value: 2021-05-04T19:30:53Z
metadata.lang: -
metadata.name: dc.date.issued
metadata.value: 2021-03
metadata.lang: -
metadata.name: dc.identifier.citation
metadata.value: Aleksandrov A.Yu., Andriyanova N.R., Tikhonov A.A. Averaging technique in the problem of satellite attitude stabilization in indirect position in the orbital reference frame with the use of Lorentz torque. Vestnik of Saint Petersburg University. Mathematics. Mechanics. Astronomy, 2021, vol. 8 (66), issue 1, pp. 123–137.
metadata.lang: en_GB
metadata.name: dc.identifier.other
metadata.value: https://doi.org/10.21638/spbu01.2021.111
metadata.lang: -
metadata.name: dc.identifier.uri
metadata.value: http://hdl.handle.net/11701/28439
metadata.lang: -
metadata.name: dc.description.abstract
metadata.value: A dynamically symmetric satellite in a circular orbit of small inclination is considered. The
  problem of the Lorentzian stabilization of the satellite in the orbital coordinate system in
  the indirect equilibrium position is solved under the conditions of the perturbing effect of the
  gravitational torque. To solve this problem, which is characterized by incomplete control,
  a method of averaging differential equations is developed. Using the original construction
  of the unsteady Lyapunov function, we obtain sufficient conditions for the asymptotic
  stability of the programmed satellite motion mode in the form of constructive inequalities
  with respect to the control parameters.
metadata.lang: en_GB
metadata.name: dc.description.sponsorship
metadata.value: This work is supported by Russian Foundation for Basic Research (grant No. 19-01-00146-a).
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 8 (66); Issue 1
metadata.lang: -
metadata.name: dc.subject
metadata.value: satellite
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: stabilization
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: attitude motion
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: asymptotic stability
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: Lyapunov function method
metadata.lang: en_GB
metadata.name: dc.title
metadata.value: Averaging technique in the problem of satellite attitude stabilization in indirect position in the orbital reference frame with the use of Lorentz torque
metadata.lang: en_GB
metadata.name: dc.type
metadata.value: Article
metadata.lang: en_GB
resources.filename: 123-137.pdf
resources.url: https://dspace.spbu.ru/bitstream/11701/28439/1/123-137.pdf
resources.format: Adobe PDF
resources.size: 372,17 kB