Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
Contactless Capture and Removal of Space Debris Objects Using Electromagnetic Induction. / Патель, Ишан Киранкумар; Тихонов, Алексей Александрович.
в: Vestnik St. Petersburg University: Mathematics, Том 54, № 4, 10.2021, стр. 418-427.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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TY - JOUR
T1 - Contactless Capture and Removal of Space Debris Objects Using Electromagnetic Induction
AU - Патель, Ишан Киранкумар
AU - Тихонов, Алексей Александрович
N1 - Publisher Copyright: © 2021, Pleiades Publishing, Ltd.
PY - 2021/10
Y1 - 2021/10
N2 - Abstract: The possibility of a contactless capture of the conductive space-debris objects (SDOs) using electromagnetic induction based on Faraday’s law of induction and Lenz’s law is analyzed. It is assumed that the spacecraft (SC) for capturing SDOs is equipped with a toroidal coil, which generates a sufficiently strong magnetic field and induces it on the SDO approaching the SC. The dynamics of the orbital motion of the SDO relative to the SC is modeled using the Clohessy–Wiltshire equations and studied numerically. The proposed method for the contactless electromagnetic capture of the conductive SDO can be used to move the SDO to a target orbit—in particular, to a graveyard orbit. The feasibility of the method is discussed based on modeling results. Directions for improvement and development of the method are identified.
AB - Abstract: The possibility of a contactless capture of the conductive space-debris objects (SDOs) using electromagnetic induction based on Faraday’s law of induction and Lenz’s law is analyzed. It is assumed that the spacecraft (SC) for capturing SDOs is equipped with a toroidal coil, which generates a sufficiently strong magnetic field and induces it on the SDO approaching the SC. The dynamics of the orbital motion of the SDO relative to the SC is modeled using the Clohessy–Wiltshire equations and studied numerically. The proposed method for the contactless electromagnetic capture of the conductive SDO can be used to move the SDO to a target orbit—in particular, to a graveyard orbit. The feasibility of the method is discussed based on modeling results. Directions for improvement and development of the method are identified.
KW - active debris removal
KW - contactless method
KW - electromagnetic induction
KW - space debris
UR - http://www.scopus.com/inward/record.url?scp=85121451246&partnerID=8YFLogxK
U2 - 10.1134/S1063454121040142
DO - 10.1134/S1063454121040142
M3 - Article
VL - 54
SP - 418
EP - 427
JO - Vestnik St. Petersburg University: Mathematics
JF - Vestnik St. Petersburg University: Mathematics
SN - 1063-4541
IS - 4
ER -
ID: 89688475