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SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT. / Grinevitskaya, L. K.; Polyakhova, E. N.

в: Cosmic Res, Том 14, № 3, 1976, стр. 311-314.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Grinevitskaya, LK & Polyakhova, EN 1976, 'SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT.', Cosmic Res, Том. 14, № 3, стр. 311-314.

APA

Grinevitskaya, L. K., & Polyakhova, E. N. (1976). SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT. Cosmic Res, 14(3), 311-314.

Vancouver

Grinevitskaya LK, Polyakhova EN. SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT. Cosmic Res. 1976;14(3):311-314.

Author

Grinevitskaya, L. K. ; Polyakhova, E. N. / SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT. в: Cosmic Res. 1976 ; Том 14, № 3. стр. 311-314.

BibTeX

@article{d7edfe6a495f477ab1d10f235e5bc325,
title = "SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT.",
abstract = "The motion of a spacecraft with planar solar sail, commencing from a circular geocentric orbit oriented arbitrarily with respect to the terrestrial equator, is considered. Using the small parameter method, general solutions of the equations of motion of the craft's center of mass are found, from which it follows that the perturbing force of solar ray pressure acts in a resonant mode and produces movement of the vehicle away from the earth. To within an accuracy of terms of the order of the small parameter it may be assumed that the motion occurs in the plane of the original orbit.",
author = "Grinevitskaya, {L. K.} and Polyakhova, {E. N.}",
year = "1976",
language = "English",
volume = "14",
pages = "311--314",
journal = "Cosmic Research",
issn = "0010-9525",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "3",

}

RIS

TY - JOUR

T1 - SOLUTION OF THE EQUATIONS OF MOTION OF A SPACECRAFT WITH SOLAR SAIL IN AN ARBITRARILY ORIENTED GEOCENTRIC ORBIT.

AU - Grinevitskaya, L. K.

AU - Polyakhova, E. N.

PY - 1976

Y1 - 1976

N2 - The motion of a spacecraft with planar solar sail, commencing from a circular geocentric orbit oriented arbitrarily with respect to the terrestrial equator, is considered. Using the small parameter method, general solutions of the equations of motion of the craft's center of mass are found, from which it follows that the perturbing force of solar ray pressure acts in a resonant mode and produces movement of the vehicle away from the earth. To within an accuracy of terms of the order of the small parameter it may be assumed that the motion occurs in the plane of the original orbit.

AB - The motion of a spacecraft with planar solar sail, commencing from a circular geocentric orbit oriented arbitrarily with respect to the terrestrial equator, is considered. Using the small parameter method, general solutions of the equations of motion of the craft's center of mass are found, from which it follows that the perturbing force of solar ray pressure acts in a resonant mode and produces movement of the vehicle away from the earth. To within an accuracy of terms of the order of the small parameter it may be assumed that the motion occurs in the plane of the original orbit.

UR - http://www.scopus.com/inward/record.url?scp=0016953688&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:0016953688

VL - 14

SP - 311

EP - 314

JO - Cosmic Research

JF - Cosmic Research

SN - 0010-9525

IS - 3

ER -

ID: 86488584