PERTURBATION IN ORBITAL ELEMENTS OF A HIGH ELLIPTICAL ORBIT OF SATELLITE CONSTELLATIONS

被引：0

作者：

Mostafa, Osama ^{[1
]}

Fujita, Koki ^{[1
]}

Hanada, Toshiya ^{[1
]}

机构：

[1] Dept Aeronaut & Astronaut, Nishi Ku, Motooka 744, Fukuoka, Fukuoka 8190395, Japan

来源：

SPACEFLIGHT MECHANICS 2017, PTS I - IV | 2017年 / 160卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This work aim to study the effects of various perturbations on the motion of satellites constellation in high elliptical inclined orbit in order to make continuous coverage. A computational model developed at Space Systems Dynamics Laboratory, Kyushu University to study the effect of these perturbations on Molniya and Tundra satellite constellations for various periods one, five and 10 years. The equations of motion under effect of these perturbations forces are solved numerically using Gaussian equations. The results show that the satellites constellation in Molniya orbit have stability under effect of gravity of third body more than Tundra orbit in order to make a continuous coverage.

引用

页码：1733 / 1745

页数：13

共 50 条

[41] An optimization model for routing in Low Earth Orbit satellite constellations
Ferreira, A
Galtier, J
Mahey, P
Mateus, G
Oliveira, A
Pichereau, M
I-SPAN 2000: INTERNATIONAL SYMPOSIUM ON PARALLEL ARCHITECTURES ALGORITHMS AND NETWORKS, PROCEEDINGS, 2000, : 161 - 166
[42] Staged deployment of communications satellite constellations in low earth orbit
De Weck, Olivier
De Neufville, Richard
Chaize, Mathieu
Journal of Aerospace Computing, Information and Communication, 2004, (MAR.): : 119 - 136
[43] Interaction of the satellite constellations with the low earth orbit debris environment
Rossi, A
Anselmo, L
Pardini, C
Farinella, P
Cordelli, A
MISSION DESIGN & IMPLEMENTATION OF SATELLITE CONSTELLATIONS, 1998, 1 : 327 - 335
[44] Darkening Low-Earth Orbit Satellite Constellations: A Review
Lalbakhsh, Ali
Pitcairn, Andrew
Mandal, Kaushik
Alibakhshikenari, Mohammad
Esselle, Karu P.
Reisenfeld, Sam
IEEE ACCESS, 2022, 10 : 24383 - 24394
[45] Perturbation Effects in Orbital elements of CubeSats
Hanafi, Ahmed
Karim, Mohammed
Hachem, El-Kaber
Rachidi, Tajjeeddine
Sahmoudi, Mohamed
2017 3RD INTERNATIONAL CONFERENCE ON ADVANCED TECHNOLOGIES FOR SIGNAL AND IMAGE PROCESSING (ATSIP), 2017, : 397 - 402
[46] Beyond GEO - Using elliptical orbit constellations to multiply the space real estate
Draim, JE
Cefola, PJ
Inciardi, R
Carter, D
Proulx, R
Larsen, DE
ACTA ASTRONAUTICA, 2002, 51 (1-9) : 467 - 489
[47] Autonomous navigation method of high elliptical orbit satellite based on celestial navigation and GPS
Wang, Peng
Zhang, Ying-Chun
Kongzhi yu Juece/Control and Decision, 2015, 30 (03): : 519 - 525
[48] Optimal design and orbital control of satellite constellations for global coverage
Palmerini, GB
ASTRODYNAMICS 1995, 1996, 90 : 499 - 507
[49] PERIODIC ROTATION OF A SATELLITE IN THE PLANE OF AN ELLIPTICAL ORBIT.
Sarychev, V.A.
Sazonov, V.V.
Zlatoustov, V.A.
Cosmic research, 1979, 17 (02) : 159 - 173
[50] On the stability of resonant rotation of a symmetric satellite in an elliptical orbit
Bardin, Boris S.
Chekina, Evgeniya A.
REGULAR & CHAOTIC DYNAMICS, 2016, 21 (04): : 377 - 389

← 1 2 3 4 5 →