Satellite relative equations in low earth orbits under third-body perturbation

被引:0
|
作者
Xu, Guang-Yan [1 ]
Chen, Ying [2 ]
Luo, Jian-Fu [1 ]
Chen, Xia [1 ]
机构
[1] Shenyang Aerospace University, Shenyang,110136, China
[2] Beijing Institute of Control Engineering, Beijing,100190, China
来源
Yuhang Xuebao/Journal of Astronautics | 2015年 / 36卷 / 01期
关键词
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I
10.3873/j.issn.1000-1328.2015.01.004
中图分类号
学科分类号
摘要
Equations of motion - Orbits
引用
收藏
页码:25 / 32
相关论文
共 50 条
  • [21] On the Generalized Kepler Problem under the Effect of Outer Third-Body Perturbation (vol 68, pg 429, 2024)
    Suzuki, M. R. S.
    ASTRONOMY REPORTS, 2024, 68 (10) : 1029 - 1030
  • [22] Relative orbit estimation and formation keeping control of satellite formations in low Earth orbits
    Zeng, Guoqiang
    Hu, Min
    Yao, Hong
    ACTA ASTRONAUTICA, 2012, 76 : 164 - 175
  • [23] Third-body perturbation using a single averaged model: Application in nonsingular variables
    Huaura Solorzano, Carlos Renato
    Bertachini de Almeida Prado, Antonio Fernando
    MATHEMATICAL PROBLEMS IN ENGINEERING, 2007, 2007
  • [24] Analytical spacecraft relative dynamics with gravitational, drag and third-body perturbations
    Chihabi, Yazan
    Ulrich, Steve
    ACTA ASTRONAUTICA, 2021, 185 : 42 - 57
  • [25] ANALYTICAL SPACECRAFT FORMATION DYNAMICS IN ECCENTRIC ORBITS WITH GRAVITATIONAL, DRAG AND THIRD-BODY PERTURBATIONS
    Chihabi, Yazan
    Ulrich, Steve
    SPACEFLIGHT MECHANICS 2019, VOL 168, PTS I-IV, 2019, 168 : 3471 - 3490
  • [26] AN ELECTRIC-PROPULSION-BASED MERCURY ORBIT TRANSFER STRATEGY SUBJECT TO THIRD-BODY PERTURBATION
    Wu, Shunan
    Wen, Shenghui
    Ma, Xue
    Wu, Zhigang
    FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III, 2018, 165 : 1705 - 1713
  • [27] Analysis of the Relative Motion Characteristics of Millimeter-level Satellite Formations under the Influence of Earth Oblateness Relative Perturbation
    Liu, Chunyang
    Wang, Jingji
    Yin, Junxiong
    Jiang, Zehua
    Zhou, Wei
    2021 PROCEEDINGS OF THE 40TH CHINESE CONTROL CONFERENCE (CCC), 2021, : 3435 - 3441
  • [28] Analysis and control of satellite orbits around oblate earth using perturbation method
    Yan, QG
    Kapila, V
    PROCEEDINGS OF THE 40TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-5, 2001, : 1517 - 1522
  • [29] CONTINUATION OF PERIODIC ORBITS OF A THIRD ORDER OSCILLATOR UNDER AUTONOMOUS PERTURBATION
    Afsharnejad, Z.
    Golmakani, A.
    JOURNAL OF DYNAMICAL SYSTEMS AND GEOMETRIC THEORIES, 2006, 4 (02) : 191 - 197
  • [30] THE THIRD ORDER SOLUTION OF ORBITAL PERTURBATION OF ARTIFICIAL EARTH'S SATELLITE
    刘林
    赵德滋
    Science China Mathematics, 1981, (06) : 813 - 828