Dynamical evolution of space debris on high-elliptical orbits near high-order resonance zones / Kuznetsov Eduard,Zakharova Polina // ADVANCES IN SPACE RESEARCH. - 2015. - V. 56, l. 3. - P. 406-413.

ISSN/EISSN:

0273-1177 / 1879-1948

Type:

Article

Abstract:

Both analytical and numerical results are used to study high-order resonance regions in the vicinity of Molniya-type orbits. Based on data of numerical simulations, long-term orbital evolution are studied for HEO objects depending on their AMR. The Poynting-Robertson effect causes a secular decrease in the semi-major axis of a spherically symmetrical satellite. Under the Poynting-Robertson effect, objects pass through the regions of high-order resonances. The Poynting-Robertson effect and secular perturbations of the semi-major axis lead to the formation of weak stochastic trajectories. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.

Author keywords:

High-elliptical orbit; High-order resonance; Satellite; Stochastic trajectory PERTURBATIONS; ECCENTRICITY; SATELLITES; PRESSURE; OBJECTS

DOI:

10.1016/j.asr.2015.03.022

Web of Science ID:

ISI:000357905200005

Соавторы в МНС:

Другие поля

Поле	Значение
Month	AUG 1
Publisher	ELSEVIER SCI LTD
Address	THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND
Language	English
EISSN	1879-1948
Keywords-Plus	PERTURBATIONS; ECCENTRICITY; SATELLITES; PRESSURE; OBJECTS
Research-Areas	Astronomy \& Astrophysics; Geology; Meteorology \& Atmospheric Sciences
Web-of-Science-Categories	Astronomy \& Astrophysics; Geosciences, Multidisciplinary; Meteorology \& Atmospheric Sciences
Author-Email	eduard.kuznetsov@urfu.ru polina.zakharova@urfu.ru
Funding-Acknowledgement	Ministry of Education and Science of Russian Federation {[}RFMEFI59114X0003]; Russian Foundation for Basic Researches {[}13-02-00026a]
Funding-Text	Main results were obtained by the use of equipment of the unique scientific unit ``Kourovka Astronomical Observatory{''}. This research was partially supported by the state as represented by the Ministry of Education and Science of the Russian Federation (unique project identifier RFMEFI59114X0003) in a part of the orbital evolution and the Russian Foundation for Basic Researches (Grant 13-02-00026a) in a part of the stochastic trajectories formation.
Number-of-Cited-References	14
Usage-Count-Since-2013	4
Journal-ISO	Adv. Space Res.
Doc-Delivery-Number	CM7VS