GAO Yun-feng, BAOYIN He-xi, LI Jun-feng. Comparison of Two Methods in Satellite Formation Flying[J]. Applied Mathematics and Mechanics, 2003, 24(8): 799-804.
Citation: GAO Yun-feng, BAOYIN He-xi, LI Jun-feng. Comparison of Two Methods in Satellite Formation Flying[J]. Applied Mathematics and Mechanics, 2003, 24(8): 799-804.

Comparison of Two Methods in Satellite Formation Flying

  • Received Date: 2001-11-27
  • Rev Recd Date: 2003-05-06
  • Publish Date: 2003-08-15
  • Recently,the research of dynamics and control of the satellite formation flying has been attracting a great deal of attentions of the researchers.The theory of the research was mainly based on Clohessy-Wiltshire's(C-W's) equations,which describe the relative motion between two satellites.But according to some special examples and qualitative analysis,neither the initial parameters nor the period of the solution of C-W's equations accord with the actual situation,and the conservation of energy is no longer held.Anew method developed from orbital element description of single satellite,named relative orbital element method(ROEM),was introduced.This new method,with clear physics conception and wide application range,overcomes the limitation of C-W's equation,and the periodic solution is a natural conclusion.The simplified equation of the relative motion is obtained when the eccentricity of the main satellite is small.Finally,the results of the two methods(C-W's equation and ROEM) are compared and the limitations of C-W's equations are pointed out and explained.
  • loading
  • [1]
    林来兴.微小卫星编队飞行组成虚拟卫星研究[A].见:林来兴编.微小卫星编队飞行组成分布式卫星技术研讨会[C].北京:国家高技术专家委员会微星技术组,2002,1-35.
    [2]
    肖业伦,张晓敏.微小卫星编队飞行动力学特征与构形设计[A].见:林来兴编.微小卫星编队飞行组成分布式卫星技术研讨会[C].北京:国家高技术专家委员会微星技术组,2002,133-144.
    [3]
    David Folta,Francesco Bordi,Christopher Scolese.Considerations on formation flying separation for earth observing satellite missions[J].AAS 92-144.Advances in the Astronautical Sciences,1992,79(2):803-822.
    [4]
    David Weidow,John Bristow.NASA/DoD university nano-satellites for distributed spacecraft control[A].In:SSC99-V-5.13th.AIAA/USU Small Satellite Conference[C].Logan,Utah,1999,23-26.
    [5]
    Clohessy W H,Wiltshire R S.Terminal guidance system for satellite rendezvous[J].Journal of the Aerospace Science,1960,27:653-674.
    [6]
    Yan Q,Kapila V,Sparks A G.Pulse-based periodic control for spacecraft formation flying[A].In:Proceeding of the American Control Conference[C].Chicago,Illinois,2000,374-378.
    [7]
    Kapila V,Sparks A G,Buffington J M,et al.Spacecraft formation flying:dynamics and control[A].In:Proceeding of the American Control Conference[C].San Diego,California,1999,4137-4141.
    [8]
    杨维廉.卫星相对运动的新解法[J].中国空间科学技术,1999,20(6):20-26.
    [9]
    张晓敏.航天器相对轨道运动动力学与控制研究[D].[博士论文].北京:北京航空航天大学,2000.
    [10]
    章仁为.航天器轨道姿态动力学与控制[M].北京:北京航空航天大学出版社,1998,1-7.
    [11]
    高云峰.卫星编队飞行相对轨道运动动力学研究[D].[博士论文].北京:清华大学,2001.
    [12]
    杨家墀.航天器轨道动力学与控制[M].北京:宇航出版社,1995,52-54.
    [13]
    陈予恕,唐云,郑兆昌,等.非线性动力学中的现代分析方法[M].北京:科学出版社,1992,10-30.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (4071) PDF downloads(970) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return