Linearized formation flight dynamics model under J2 perturbation

被引:0
|
作者
机构
[1] Xing, Jian-Jun
[2] Shi, Wei
[3] Jiang, Bing-Yan
来源
Xing, J.-J. (xjj@csu.edu.cn) | 2013年 / China Spaceflight Society卷 / 34期
关键词
Orbits;
D O I
10.3873/j.issn.1000-1328.2013.05.002
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [21] In-Plane Satellite Formations in Eccentric Orbits under J2 Perturbation
    Xu, Guangyan
    Wang, Danwei
    Poh, Eng Kee
    Wu, Baolin
    2009 IEEE AEROSPACE CONFERENCE, VOLS 1-7, 2009, : 396 - 404
  • [22] Linearized J2 and atmospheric drag model for satellite relative motion with small eccentricity
    Cao, Lu
    Misra, Arun K.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (14) : 2718 - 2736
  • [23] Linearized dynamic equations for spacecraft subject to J2 perturbations
    Ross, IM
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (04) : 657 - 659
  • [24] Relative motion control for formation flying satellite constellations in the presence of J2 perturbation
    Zhang, Hong-Hua
    Zhang, Guo-Feng
    Lin, Lai-Xing
    Yuhang Xuebao/Journal of Astronautics, 2003, 24 (05):
  • [25] Precision analytical equation to relative motion of formation flying satellites for J2 perturbation
    Zhang, Jinxiu
    Cao, Xibin
    Wang, Jihe
    Yingyong Jichu yu Gongcheng Kexue Xuebao/Journal of Basic Science and Engineering, 2007, 15 (03): : 342 - 350
  • [26] Higher Order Sliding Mode Control of Formation Flying Satellites with J2 Perturbation
    Li Yafei
    Liu Xiangdong
    Xiao Yuzhi
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 643 - 648
  • [27] Correcting semi-major to reduce effect of J2 perturbation on formation flying
    Li, Hua-Yi
    Qiang, Wen-Yi
    Zhang, Ying-Chun
    Li, Bao-Hua
    PROCEEDINGS OF 2006 INTERNATIONAL CONFERENCE ON MACHINE LEARNING AND CYBERNETICS, VOLS 1-7, 2006, : 797 - +
  • [28] Design and Maintenance of InSAR Configuration for Digital Elevation Measurement under J2 Perturbation
    He, Yanchao
    Xu, Ming
    PROCEEDINGS OF THE 2016 12TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA), 2016, : 804 - 808
  • [29] Rendezvous Maneuvers of Multiple Spacecraft Using Differential Drag Under J2 Perturbation
    Bevilacqua, R.
    Romano, M.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (06) : 1595 - 1607
  • [30] Deployment and retrieval of tethered satellite system under J2 perturbation and heating effect
    Yu, B. S.
    Jin, D. P.
    ACTA ASTRONAUTICA, 2010, 67 (7-8) : 845 - 853