Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
On the coupled orbit-attitude control motion of a celestial body in the neighborhood of the collinear libration point L1 of the Sun-Earth system. / Shymanchuk, Dzmitry.
2017 Constructive Nonsmooth Analysis and Related Topics (Dedicated to the Memory of V.F. Demyanov), CNSA 2017 - Proceedings. Institute of Electrical and Electronics Engineers Inc., 2017. 7974013.Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
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TY - GEN
T1 - On the coupled orbit-attitude control motion of a celestial body in the neighborhood of the collinear libration point L1 of the Sun-Earth system
AU - Shymanchuk, Dzmitry
PY - 2017/7/10
Y1 - 2017/7/10
N2 - This paper considers the motion of a celestial body (as a rigid body) within the restricted three-body 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 circular restricted three-body problem of the Sun-Earth system. Rotational orbital motion is described using Euler's dynamic equations and quaternion kinematic equation. The problems of celestial body motion stability in relative equilibrium positions and stabilization of a celestial body translational motion with proposed control law in collinear libration point L1 are investigated. Results of numerical integration are presented graphically.
AB - This paper considers the motion of a celestial body (as a rigid body) within the restricted three-body 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 circular restricted three-body problem of the Sun-Earth system. Rotational orbital motion is described using Euler's dynamic equations and quaternion kinematic equation. The problems of celestial body motion stability in relative equilibrium positions and stabilization of a celestial body translational motion with proposed control law in collinear libration point L1 are investigated. Results of numerical integration are presented graphically.
UR - http://www.scopus.com/inward/record.url?scp=85027440022&partnerID=8YFLogxK
U2 - 10.1109/CNSA.2017.7974013
DO - 10.1109/CNSA.2017.7974013
M3 - Conference contribution
AN - SCOPUS:85027440022
BT - 2017 Constructive Nonsmooth Analysis and Related Topics (Dedicated to the Memory of V.F. Demyanov), CNSA 2017 - Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 Constructive Nonsmooth Analysis and Related Topics
Y2 - 22 May 2017 through 27 May 2017
ER -
ID: 9426862