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COMPARISON OF TWO METHODS IN SATELLITE FORMATION FLYING

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【作者】 高云峰宝音贺西李俊峰

【Author】 GAO Yun-feng, BAOYIN He-xi, LI Jun-feng(Department of Engineering Mechanics, Tsinghua University, Beijing 100084, P.R.China)

【机构】 Department of Engineering MechanicsTsinghua UniversityBeijing 100084P.R.ChinaP.R.China

【摘要】 <正> 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. A new 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

【Abstract】 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. A new 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.

【基金】 Foundation items: the National Natural Science Foundation of China (10202008); the Post Doctoral Science Foundation of China ((2001)31)
  • 【文献出处】 Applied Mathematics and Mechanics(English Edition) ,应用数学和力学(英文版) , 编辑部邮箱 ,2003年08期
  • 【分类号】V520
  • 【被引频次】2
  • 【下载频次】45
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