Planar Problem Motion Stabilization Using the Rotational Motion and the Light Pressure Forces at the Collinear Libration Point

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Planar Problem Motion Stabilization Using the Rotational Motion and the Light Pressure Forces at the Collinear Libration Point. / Шиманчук, Дмитрий Викторович.

Proceedings of the 2023 3rd International Conference on Robotics and Control Engineering. 2023. p. 25-31 (ACM International Conference Proceeding Series).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Harvard

Шиманчук, ДВ 2023, Planar Problem Motion Stabilization Using the Rotational Motion and the Light Pressure Forces at the Collinear Libration Point. in Proceedings of the 2023 3rd International Conference on Robotics and Control Engineering. ACM International Conference Proceeding Series, pp. 25-31, 2023 3rd International Conference on Robotics and Control Engineering, Нанкин, China, 12/05/23. https://doi.org/10.1145/3598151.3598156

BibTeX

@inproceedings{8efb691342d0440cb65b0b1332e2330c,

title = "Planar Problem Motion Stabilization Using the Rotational Motion and the Light Pressure Forces at the Collinear Libration Point",

abstract = "This article represented the controlled planar orbital motion of a spacecraft with a solar sail. The motion of a spacecraft is described by using the Hill's problem of the circular restricted three-body problem of the Sun-Earth system. The attitude motion is determined by using the Euler dynamic equations and the quaternion kinematic equation. The spacecraft keeping planar problem in a neighborhood of a collinear libration point using the example of a solar sail is investigated. The orientation problem of a solar sail solving by constructing a feedback control as a special function of phase coordinates. This function is represent the linear approximation of a stable invariant manifold in a neighborhood of a libration point. Problem of spacecraft attitude control motion with a flywheel is considered. Numerical simulation of the controlled motion of a spacecraft at a libration point is carried out. The numerical estimations of the control law parameters and controlled motion are given.",

keywords = "attitude motion, control, invariant manifold, libration point, rigid body, solar sail, space robotics",

author = "Шиманчук, {Дмитрий Викторович}",

year = "2023",

month = may,

day = "12",

doi = "10.1145/3598151.3598156",

language = "English",

isbn = "9781450398107",

series = "ACM International Conference Proceeding Series",

pages = "25--31",

booktitle = "Proceedings of the 2023 3rd International Conference on Robotics and Control Engineering",

note = "null ; Conference date: 12-05-2023 Through 14-05-2023",

url = "https://robce.org/",

}

RIS

TY - GEN

T1 - Planar Problem Motion Stabilization Using the Rotational Motion and the Light Pressure Forces at the Collinear Libration Point

AU - Шиманчук, Дмитрий Викторович

PY - 2023/5/12

Y1 - 2023/5/12

N2 - This article represented the controlled planar orbital motion of a spacecraft with a solar sail. The motion of a spacecraft is described by using the Hill's problem of the circular restricted three-body problem of the Sun-Earth system. The attitude motion is determined by using the Euler dynamic equations and the quaternion kinematic equation. The spacecraft keeping planar problem in a neighborhood of a collinear libration point using the example of a solar sail is investigated. The orientation problem of a solar sail solving by constructing a feedback control as a special function of phase coordinates. This function is represent the linear approximation of a stable invariant manifold in a neighborhood of a libration point. Problem of spacecraft attitude control motion with a flywheel is considered. Numerical simulation of the controlled motion of a spacecraft at a libration point is carried out. The numerical estimations of the control law parameters and controlled motion are given.

AB - This article represented the controlled planar orbital motion of a spacecraft with a solar sail. The motion of a spacecraft is described by using the Hill's problem of the circular restricted three-body problem of the Sun-Earth system. The attitude motion is determined by using the Euler dynamic equations and the quaternion kinematic equation. The spacecraft keeping planar problem in a neighborhood of a collinear libration point using the example of a solar sail is investigated. The orientation problem of a solar sail solving by constructing a feedback control as a special function of phase coordinates. This function is represent the linear approximation of a stable invariant manifold in a neighborhood of a libration point. Problem of spacecraft attitude control motion with a flywheel is considered. Numerical simulation of the controlled motion of a spacecraft at a libration point is carried out. The numerical estimations of the control law parameters and controlled motion are given.

KW - attitude motion

KW - control

KW - invariant manifold

KW - libration point

KW - rigid body

KW - solar sail

KW - space robotics

UR - https://www.mendeley.com/catalogue/ee70fbc9-6d87-3bd9-96ab-6a6ecf9b1027/

U2 - 10.1145/3598151.3598156

DO - 10.1145/3598151.3598156

M3 - Conference contribution

SN - 9781450398107

T3 - ACM International Conference Proceeding Series

SP - 25

EP - 31

BT - Proceedings of the 2023 3rd International Conference on Robotics and Control Engineering

Y2 - 12 May 2023 through 14 May 2023

ER -

ID: 114716160