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22、ZE HKPMH、iu :Pistdm :vn H ULKmhMR*. n-.x 1.14. Il hX AL丄41斗用鼻 ii耳 |UlJ R E tank IMMIHMf MMHjMvm ? .i4卯屮wwr Ti皆i耳 * Sfl tiB r miXIM:LFWi L a心HK*:I-KJ j tia. EMJKUICKrini haf：土A-n* Hrnai 9JKJ BEJrK -rat IFTAi 1-H_, d： -saLfew .si.： j L rJ - i In ternatio nal Journal of Con trol a nd Automation Vol. 4,

23、 No. 4, December, 2011 15F. Terui, “ Positi on and Attitude Con trol of a Spacecraft by Slidi ng Mode Con trolProceedings of the American Control Conference, (1998, pp. 217-221. 16 D. T.Sta nsbery and J. R. Cloutier,“ Positi on and Attitude Con trol of a Spagdhraft UsiStateDependent Riccati Equation

24、 Technique” , Proceedings of the American ControlConference, (2000, pp. 1867-1871. 17 P. Singla, K. Subbarao and J. L. Junkins,“ Adaptive Output Feedback Con trol for Spacecraft Ren dezvous and Dock ing Un derMeasureme nt Un certa inty” , Jour nal of Guida nee, Con trol, and Dyn amics, vol. 29, (200

25、6,pp. 892-902. 18 K. Subbarao and S. Welsh,“ Non li near Con trol of MotionSynchroni zati on for Satellite Proximity Operati ons” , Jour nal of Guida nee, Con trol, andDynamics, vol. 31, (2008, pp. 1284-1294. 19 M. Xin and H. Pan,“Integrated NonlinearOptimal Control of Spacecraft in Proximity Operat

26、ions”，International Journal of Control,vol. 83, (2010, pp. 347-363. 20 M. D. J. Brow n,“ Co ntin uous and Smooth Slidi ngMode Control ” , Ph.D. dissertation, University of Alabama in Huntsville, Dept. ofElectrical a nd Computer Engin eeri ng , chap. 8, (2001, pp, 117-120. 21 B. Wie and J. Lu,”*yr! 4

27、wn Aril WHHH_#尢9B 9K. * 4U ill =r z | P .-I-怦可- J-l T-.耐rS.*4 -Itewai rif-MM M刍 EH pp( (vwwwpaHl MfFeedback Con trol Logic for Spacecraft Eige naxis Rotatio ns Un der Slew Rate andCon trol Con straints ” , Jour nal of Guida nee. Con trol, and Dyn amics, vol. 18, (1995, pp.1372-1379. 22 M. D. Lichter

28、 and S. Dubowsky,“State, Shape, and ParameterEstimation of Space Objects from Range Images” , Proceedings of the 2004 IEEEIn ternatio nal Co nference on Robotics & Automatio n, (2004, pp. 2974-2979. 23 U.Hille nbrand and R. Lampariello,“ Moti on and Parameter Estimatio-FlofeiinFreeSpace Object f

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31、9-846. 26 F. Adpili and K. Parsa,“ An Adaptive Visio n Systemfor Guidance of a Robotic Manipulator to Capture a Tumbling Satellite with UnknownDynamics ” , Proceedings of the 2008 IEEE/RSJ International Conference on IntelligentRobots and Systems, (2008 , pp. 839-846. 27 Y. B. Shtessel a nd J. M. Bu

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33、nd Con trol Conference and Exhibit,AIAA-2000- 3964. 29 G. Bartolini and P. Pydynowski,“ An Improved Chattering Free,V.S.C. Scheme for Uncertain Dynamical Systems”，lEEBTsansacttomaticControl, vol. 41, (1996, pp. 1220-1226. 30 G. Bartolini, A. Ferrara and E. Usai,“Chattering Avoidance by SecondOrder S

34、liding Mode Control” , IEEE Transactions onAutomatic Control, vol. 41, (1998, pp. 241-246. Authors LU Wei received B. E. & M. E.degrees in Spacecraft Desig n from the Harbin In stitute of Tech no logy, Chi na, i n 2006and 2008 respectively. Curre ntly, he is a Ph. D. Can didate in Spacecraft Des

35、ig n from theHarbin In stitute of Tech no logy, Harbin, China. He has published about 2 refereed jour nal and conferencepapers. His research in terest covers Slidi ng Mode Con trol, Robust Control, and Autonomous docking witha tumbling target. E-mail: (Corresp onding Author. 21In ternatio nal Journa

36、l of Con trol a nd Automation Vol. 4, No. 4, December, 2011GENG Yunhai received B. E. degree in Engineering Mechanics from the TongjiUniversity, M. E. degree and Ph. D degree in Spacecraft Design from the Harbin Institute of Technology,China, in 1992, 1995 and 2003 respectively. Currently, he is a Professor and doctoral advisor of SpacecraftDesig n, Harbin In st