卫星编队飞行轨道和姿态控制研究

张治国; 李俊峰

卫星编队飞行轨道和姿态控制研究

清华大学航天航空学院,北京 100084

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
计量
- 文章访问数: 2861
- HTML全文浏览量: 149
- PDF下载量: 864
- 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

Study on the Orbit and Attitude Control of Spacecraft Formation Flying

School of Aerospace, Tsinghua University, Beijing 100084, P. R. China

摘要

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．
- 卫星编队飞行 /
- 相对轨道 /
- 相对姿态 /
- 动力学和控制
Abstract: Formation flying is a novel concept of distributing the functionality of large spacecraft among several smaller, less expensive, cooperative satellites. Some applications require that a controllable satellite keep relative position and attitude to observe a specific surface of another satellite among the cluster. Specially, the target space vehicle is malfunctioning. The problem of how to control a chaser satellite to fly around an outofwork target satellite closely in earth orbit and to track a specific surface is focused on. Relative attitude and first approximate relative orbital dynamics equations are presented. Control strategy is derived based on feedback linearization and Lyapunov theory of stability. Further, the uncertainty of inertia being considered, an adaptive control method is developed to obtain the correct inertial ratio. The numerical simulation is given to verify the validity of proposed control scheme.
- satellite formation flying /
- orbit /
- attitude /
- dynamics and control

HTML全文

参考文献(28)

[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.

施引文献

资源附件(0)

访问统计

计量

文章访问数: 2861
HTML全文浏览量: 149
PDF下载量: 864
被引次数: 0

姓名
邮箱
手机号码
标题
留言内容
验证码

留言板

卫星编队飞行轨道和姿态控制研究

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).

计量

Study on the Orbit and Attitude Control of Spacecraft Formation Flying

计量

目录

留言板

卫星编队飞行轨道和姿态控制研究

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).

计量

出版历程

Study on the Orbit and Attitude Control of Spacecraft Formation Flying

计量

出版历程

目录

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).