留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

卫星编队飞行轨道和姿态控制研究

张治国 李俊峰

张治国, 李俊峰. 卫星编队飞行轨道和姿态控制研究[J]. 应用数学和力学, 2008, 29(1): 38-46.
引用本文: 张治国, 李俊峰. 卫星编队飞行轨道和姿态控制研究[J]. 应用数学和力学, 2008, 29(1): 38-46.
ZHANG Zhi-guo, LI Jun-feng. Study on the Orbit and Attitude Control of Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(1): 38-46.
Citation: ZHANG Zhi-guo, LI Jun-feng. Study on the Orbit and Attitude Control of Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(1): 38-46.

卫星编队飞行轨道和姿态控制研究

基金项目: 国家自然科学基金资助项目(10672084);高等学校博士学科点专项科研基金资助项目(20060003097)
详细信息
    作者简介:

    张治国(1979- ),男,湖南常德人,博士生(联系人.Tel:+86-10-62773402;Fax:+86-10-62781824;E-mail:zzg7979@126.com).

  • 中图分类号: V412.4

Study on the Orbit and Attitude Control of Spacecraft Formation Flying

  • 摘要: 卫星编队飞行是一种卫星应用的新概念,通过一系列造价更便宜的小卫星的分布式合作,代替大卫星实现复杂功能.在编队飞行一些应用中,要求受控卫星对目标卫星保持要求的相对位置和姿态以观察目标卫星的特定面,特别的,目标卫星可能是失效的.研究在近地轨道如何控制追踪星在失效的目标卫星附近飞行以追踪目标卫星特定面 的问题,给出了相对姿态和一阶近似的相对轨道动力学方程.基于线性反馈和Liapunov稳定性理论设计了控制策略.进一步的,考虑目标卫星转动惯量的不确定性,通过自适应控制的方法,获得正确的转动惯量比率.数值仿真算例验证了该控制方法的有效性.
  • [1] Vicram Kapila,Andrew G,Sparks,James M.Buffington,et al.Spacecraft formation flying: dynamics and control[A].In:Proceedings of American Control Conference[C].San Diego,California:June,1999,4137-4141.
    [2] Bo J Naasz. Classical element feedback control for spacecraft orbital maneuvers[D].America: the Virginia Polytechnic Institute and State University, 2002.
    [3] Steven P Hughes. Formation flying performance measures for Earth-pointing missions[D].America: the Virginia Polytechnic Institute and State University, 1999.
    [4] Folta D C, Newman L K, Gardner T. Foundations of formation flying for mission to planet earth and the new millenium[A].In:Proceedings of the AIAA/AAS Astrodynamics Conference[C].AIAA, Reston, VA:1996,656-666.
    [5] Roux A.Cluster regroups for relaunch[J].Aerospace America,1998,36(8):48-51.
    [6] Folkner W M,Hechlerz F,Sweetsery T H,et al.LISA orbit selection and stability[J].Classical and Quantum Gravity,1997,14(6):1405-1410. doi: 10.1088/0264-9381/14/6/003
    [7] Koss J, Pohlig S, Trichel M,et al. Precision radar surveillance and mapping with discovererⅡ[A].In:Proceedings of the AIAA Space Technology Conference and Exposition[C].Albuquerque,NM:1999, AIAA 99-4570.
    [8] LI Jun-feng, MENG Xin, GAO Yun-feng,et al.Study on relative orbital configuration in satellite formation flying[J].Acta Mechanica Sinica,2005,21(1):87-94. doi: 10.1007/s10409-004-0009-3
    [9] Atkins E, Pennecot Y. Autonomous satellite formation assembly and reconfiguration with gravity fields[J].IEEE,2002,296(2):783-796.
    [10] Beard R, Stirling W,Frost R.A hierarchical coordination scheme for satellite formation initialization[A].In:AIAA Guidance, Navigation and Control Conference[C].Boston, MA:August, 1998. AIAA 98-4225:677-685.
    [11] Vadali S, Vaddi S. Orbit establishment for formation flying satellites[J].Advances in the Astronautical Sciences.2000,105(I):181-194.
    [12] Schaub H,Alfriend K T. Impulsive feedback control to establish specific mean orbit elements of spacecraft formations[J].Journal of Guidance, Control, and Dynamics,2001,24(4):739-745. doi: 10.2514/2.4774
    [13] De Queiroz M S, Kapila V, Yan Q. Adaptive nonlinear control of satellite formation flying[A].In:Proc AIAA Guidance, Navigation, and Control Conf[C].AIAA 99-4270,Portland,OR:1999,99-4270,1596-1604.
    [14] Roberto Armellin, Massari Mauro,Amalia Ercoli Finzi. Optimal formation flying reconfiguration and station keeping maneuvers using low-thrust propulsion[A].In:18th International Symposium on Space Flight Dynamics[C].Munich, Germany:Oct,2004.
    [15] Clohessy H, Wiltshire R S. Terminal guidance system for satellite rendezvous[J].Journal of the Aerospace Science,1960,27(9):653-674.
    [16] Inalhan G, Tillerson M, How Jonathan P. Relative dynamics and control of spacecraft formations in eccentric orbits[J].Journal of Guidance Control, and Dynamics,2002,25(1):48-59. doi: 10.2514/2.4874
    [17] Breger Louis, How Jonathan P.Gauss's variational equation-based dynamics and control for formation flying spaceraft[J].Journal of Guidance,Control,and Dynamics,2007,30(2):437-448. doi: 10.2514/1.22649
    [18] BAOYIN He-xi, LI Jun-feng, GAO Yun-feng. Dynamical behaviors and relative trajectories of spacecrafts formation flying[J].J Aerospace Science and Technology,2002,4(6):295-301.
    [19] 高云峰,宝音贺西,李俊峰.卫星编队飞行中C-W方程与轨道根数法的比较[J].应用数学和力学,2003,24(8):799-804.
    [20] Koon W S, Marsden J E, Masdemont J, et al. J2 dynamics and formation flight[A].In:Proceedings of AIAA Guidance, Navigation, and Control Conference[C].Montreal:August, AIAA 2001,4090.
    [21] KANG Wei,YEH Hsi-han,Sparks Andrew. Coordinated control of relative attitude for satellite formation[R]. Aug.2001, AIAA 2001,4093.
    [22] KANG Wei,Sparks Andrew.Coordinated attitude and formation control of multi-satellite systems[R]. Aug.2002, AIAA 2002,4655.
    [23] KANG Wei,YEH Hsi-han.Co-ordinated attitude control of multisatellite system[J].International Journal of Robust and Nonlinear Control,2002,12(2/3): 185-205. doi: 10.1002/rnc.682
    [24] 苏罗鹏, 李俊峰,高云峰. 卫星编队飞行相对姿态控制[J].清华大学学报(自然科学版), 2003,43(5):28-36.
    [25] 张治国,李俊峰,宝音贺西. 卫星编队飞行指向跟踪姿态控制[J].清华大学学报(自然科学版),2006,46(11):32-39.
    [26] 林来兴. 微小卫星绕飞空间站的动力学和控制[J]. 航天控制,1999,17(3):26-33.
    [27] Hirohisa Kojima. Fly-around motion control based on exact linearization with adaptive law[J].J Guidance, Control and Dynamics,2005,28(1):167-169. doi: 10.2514/1.5943
    [28] David R Merkin.Introduction to the Theory of Stability[M].New York: Springer, 1996.
  • 加载中
计量
  • 文章访问数:  2689
  • HTML全文浏览量:  100
  • PDF下载量:  863
  • 被引次数: 0
出版历程
  • 收稿日期:  2007-01-17
  • 修回日期:  2007-11-12
  • 刊出日期:  2008-01-15

目录

    /

    返回文章
    返回