Mechanics of Solids (about journal) Mechanics of Solids
A Journal of Russian Academy of Sciences
 Founded
in January 1966
Issued 6 times a year
Print ISSN 0025-6544
Online ISSN 1934-7936

Russian Russian English English About Journal | Issues | Guidelines | Editorial Board | Contact Us
 


IssuesArchive of Issues2020-7pp.999-1012

Archive of Issues

Total articles in the database: 11262
In Russian (Èçâ. ÐÀÍ. ÌÒÒ): 8011
In English (Mech. Solids): 3251

<< Previous article | Volume 55, Issue 7 / 2020 | Next article >>
Dobroslavskiy A.V. and Krasilnikov P.S., "On the Evolution of Balloon Satellite Motions in a Plane Restricted Planetary Four-Body Problem with Light Pressure," Mech. Solids. 55 (7), 999-1012 (2020)
Year 2020 Volume 55 Number 7 Pages 999-1012
DOI 10.3103/S0025654420070092
Title On the Evolution of Balloon Satellite Motions in a Plane Restricted Planetary Four-Body Problem with Light Pressure
Author(s) Dobroslavskiy A.V. (Moscow Aviation Institute (National Research University), Moscow, 125080 Russia, a.dobroslavskiy@gmail.com)
Krasilnikov P.S. (krasil06@rambler.ru)
Abstract In this paper, we consider the plane restricted four-body problem taking into account the light pressure forces when the Earth’s orbit is a Keplerian ellipse with a focus at the Sun, the Moon’s orbit is a Keplerian ellipse with a focus at the Earth, and the balloon satellite is a passively gravitating body. The averaged perturbing function of the problem in osculating elements is obtained in the nonresonant case, when the unperturbed orbit of the Earth satellite lies in the outer sphere of the Earth’s gravitational influence, located beyond the lunar Hill sphere. It is found that the integrals of averaged equations in the osculating elements are the semimajor axis of the satellite orbit as well as the average value of the force function. The stationary modes of oscillations and their bifurcation depending on the light pressure coefficient and the semimajor axis are investigated. Phase oscillation portraits are constructed for different values of the light pressure coefficient. The librational and rotational orbits of the satellite in the ecliptic plane are calculated.
Keywords restricted planetary four-body problem, light pressure, averaged equations in osculating elements
Received 14 June 2019Revised 20 October 2019Accepted 30 October 2019
Link to Fulltext
<< Previous article | Volume 55, Issue 7 / 2020 | Next article >>
Orphus SystemIf you find a misprint on a webpage, please help us correct it promptly - just highlight and press Ctrl+Enter

101 Vernadsky Avenue, Bldg 1, Room 246, 119526 Moscow, Russia (+7 495) 434-3538 mechsol@ipmnet.ru https://mtt.ipmnet.ru
Founders: Russian Academy of Sciences, Ishlinsky Institute for Problems in Mechanics RAS
© Mechanics of Solids
webmaster
Rambler's Top100