title: Modeling of controlled coupled attitude-orbit motion in the neighborhood of collinear libration point L1
metadata.name: dc.contributor.author
metadata.value: Shymanchuk, Dmitry V.
metadata.lang: -
metadata.name: dc.date.accessioned
metadata.value: 2017-07-19T11:18:33Z
metadata.lang: -
metadata.name: dc.date.available
metadata.value: 2017-07-19T11:18:33Z
metadata.lang: -
metadata.name: dc.date.issued
metadata.value: 2017-06
metadata.lang: -
metadata.name: dc.identifier.citation
metadata.value: Shymanchuk D. V. Modeling of controlled coupled attitude-orbit motion in the neighborhood of collinear libration point L1. Vestnik of Saint Petersburg University. Applied Mathematics. Computer Science. Control Processes, 2017, vol. 13, iss. 2, pp. 147–167.
metadata.lang: en_GB
metadata.name: dc.identifier.other
metadata.value: 10.21638/11701/spbu10.2017.203
metadata.lang: -
metadata.name: dc.identifier.uri
metadata.value: http://hdl.handle.net/11701/6969
metadata.lang: -
metadata.name: dc.description.abstract
metadata.value: This paper considers the motion of a celestial body (as a rigid body) within the restricted threebody
  problem of the Sun—Earth system. The equations of controlled coupled attitude-orbit
  motion in the neighborhood of collinear libration point L1 are investigated. The translational
  orbital motion of a celestial body is described using Hill’s equations of a circular restricted threebody
  problem of the Sun—Earth system. Rotational orbital motion is described using Euler’s
  dynamic equations and quaternion kinematic equation. As an important result, we investigate
  the problems of celestial body motion stability in relative equilibrium positions and stabilization
  of a celestial body motion with proposed control laws in collinear libration point L1. To study
  stabilization problems, Lyapunov function is constructed in the form of the sum of the kinetic
  energy of a celestial body and special “kinematics” function of the Rodriguez—Hamiltonian
  parameters. The numerical modeling of the controlled rotational motion of a celestial body at
  libration point L1 is carried out. The numerical characteristics of the control parameters and
  rotational motion of the celestial body are given. Results of numerical integration are presented
  graphically. Refs 14. Figs 10.
metadata.lang: en_GB
metadata.name: dc.description.sponsorship
metadata.value: Работа выполнена при финансовой поддержке Санкт-Петербургского государственного университета (грант № 9.37.345.2015).
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 13; Issue 2
metadata.lang: -
metadata.name: dc.subject
metadata.value: restricted three body problem
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: Hill’s problem
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: libration point
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: rigid body
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: coupled attitude-orbit motion
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: control
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: stabilization
metadata.lang: en_GB
metadata.name: dc.title
metadata.value: Modeling of controlled coupled attitude-orbit motion in the neighborhood of collinear libration point L1
metadata.lang: en_GB
metadata.name: dc.type
metadata.value: Article
metadata.lang: en_GB
resources.filename: 03-Shimanchuk.pdf
resources.url: https://dspace.spbu.ru/bitstream/11701/6969/1/03-Shimanchuk.pdf
resources.format: Adobe PDF
resources.size: 780,77 kB