Standard

The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order. / Zegzhda, S. A.; Soltakhanov, Sh Kh; Yushkov, M. P.

In: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, Vol. 38, No. 2, 2005, p. 95-98.

Research output: Contribution to journal › Article › peer-review

Harvard

Zegzhda, SA, Soltakhanov, SK & Yushkov, MP 2005, 'The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order', Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, vol. 38, no. 2, pp. 95-98.

APA

Zegzhda, S. A., Soltakhanov, S. K., & Yushkov, M. P. (2005). The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya, 38(2), 95-98.

Vancouver

Zegzhda SA, Soltakhanov SK, Yushkov MP. The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order. Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 2005;38(2):95-98.

Author

Zegzhda, S. A. ; Soltakhanov, Sh Kh ; Yushkov, M. P. / The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order. In: Vestnik Sankt-Peterburgskogo Universiteta. Ser 1. Matematika Mekhanika Astronomiya. 2005 ; Vol. 38, No. 2. pp. 95-98.

BibTeX

@article{2c78ec31dc174319bc6f136c60e38747,
title = "The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order",
abstract = "The transition of a satellite from an elliptic orbit close to circular to another circular one is considered. The law of varying in time the radial and transversal control forces is searched, the smooth transition being realized. It is shown that in solving of the problem given the theory of motion of non-holonomic systems with high order constraints can be used.",
author = "Zegzhda, {S. A.} and Soltakhanov, {Sh Kh} and Yushkov, {M. P.}",
note = "Copyright: Copyright 2012 Elsevier B.V., All rights reserved.",
year = "2005",
language = "English",
volume = "38",
pages = "95--98",
journal = "ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ",
issn = "1025-3106",
publisher = "Издательство Санкт-Петербургского университета",
number = "2",

}

RIS

TY - JOUR

T1 - The smooth transition of a satellite from a circular orbit to a circular one as an example of the motion with a non-holonomic constraint of the third order

AU - Zegzhda, S. A.

AU - Soltakhanov, Sh Kh

AU - Yushkov, M. P.

N1 - Copyright: Copyright 2012 Elsevier B.V., All rights reserved.

PY - 2005

Y1 - 2005

N2 - The transition of a satellite from an elliptic orbit close to circular to another circular one is considered. The law of varying in time the radial and transversal control forces is searched, the smooth transition being realized. It is shown that in solving of the problem given the theory of motion of non-holonomic systems with high order constraints can be used.

AB - The transition of a satellite from an elliptic orbit close to circular to another circular one is considered. The law of varying in time the radial and transversal control forces is searched, the smooth transition being realized. It is shown that in solving of the problem given the theory of motion of non-holonomic systems with high order constraints can be used.

UR - http://www.scopus.com/inward/record.url?scp=33744537351&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:33744537351

VL - 38

SP - 95

EP - 98

JO - ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ

JF - ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ

SN - 1025-3106

IS - 2

ER -

ID: 71885375