Volume 35 Issue 5
Sep.  2015
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LIU Hailong, HAN Xu, SHI Xiaoping. Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase[J]. Journal of Space Science, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603
Citation: LIU Hailong, HAN Xu, SHI Xiaoping. Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase[J]. Journal of Space Science, 2015, 35(5): 603-610. doi: 10.11728/cjss2015.05.603

Attitude And Translation Control For Spacecraft To Approach To A Tumbling Non-Cooperative Object During The Final Phase

doi: 10.11728/cjss2015.05.603
  • Received Date: 2014-07-26
  • Rev Recd Date: 2015-03-02
  • Publish Date: 2015-09-15
  • This paper considers the process of motion synchronization of chaser satellite and target satellite in space. The problem of final approach to a non-cooperative tumbling target is studied in this paper. The accurate orbit and attitude dynamics model of two relative motion spacecrafts with arbitrary eccentrics is established. In order to insure the safety of final approach, the traditional linear synchronization rotating approach strategy is improved by designing an exponential decay reference trajectory to decay relative velocity with decreasing relative distance and reach zero when the chaser is hovering. The proportional-derivative-decouple relative attitude controller and relative orbit controller is proposed. The simulation shows the process of the relative velocity of the chaser decay to zero. The stability of the control law is demonstrated through Lyapunov analysis and effectiveness of controller is verified by the numerical simulation.

     

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  • [1]
    Zhu Renzhang, Wang Hongfang, Xu Yujie. From ETS-VII to HTV: Study of Japanese rendezvous and docking/Berthing technologies[J]. Spacec. Eng., 2011, 12(4): 113-117. In Chinese (朱仁璋, 王鸿芳, 徐宇杰. 从ETS-VII到HTV---日本交会对接 停靠技术研究[J]. 航天器工程, 2011, 12(4):113-117)
    [2]
    Pinson R M, Howard R T, Heaton A F. Orbital express advanced video guidance sensor: Ground testing, flight results and comparisons[C]//Proceedings of AIAA Guidance, Navigation and Control Conference. Reston: AIAA, 2008:1022-1027
    [3]
    Howard, R T, Pinson R M. Orbital Express AVGS Validation and Calibration for Automated Rendezvous[C]//Proceedings of AIAA/AAS Astrodynamics Specialist Conference. Reston: AIAA, 2008:345-349
    [4]
    Caswell D, Visentin G, Ortega G. ConeXpress Orbital Life Extension Vehicle (CX-OLEV) GNC[C]//Proceedings of AIAA 57th International Astronautical Congress. Paris: ESA, 2006:511-519
    [5]
    Tarabini L, Gil J, Gandia F. Ground guided CX-OLEV rendezvous with uncooperative geostationary satellite[J]. Acta Astron., 2007, 6(12):1014-1018
    [6]
    Zhang F, Duan G. Integrated relative position and attitude control of spacecraft in proximity operation missi-ons[J]. Intern. J. Autom. Comp., 2012, 9(4):342-351
    [7]
    Subbarao K, Welsh S J. Nonlinear control of motion synchronization for satellite proximity operations[J]. J. Guid., Contr. Dyn., 2008, 31(5):1284-1294
    [8]
    Welsh S J, Subbarao K. Adaptive synchronization and control of free flying robots for capture of dynamic free-floating spacecrafts[C]//Proceedings of AIAA/AAS Astrodynamics Specialist Conference. Reston: AIAA, 2004:1193-1214
    [9]
    Matsumoto S, Dubowsky S, Jacobsen S, et al. Fly-by approach and guidance for uncontrolled rotating satellite capture[C]//Proceedings of AIAA Guidance, Navigation and Control Conference and Exhibit. Reston: AIAA, 2003:1-10
    [10]
    Sanyal A, Holguin L, Viswanathan S P. Guidance and control for spacecraft autonomous chasing and close proximity maneuvers[C]//Proceedings of the 7th IFAC Symposium on Robust Control Design. Laxenburg: IFAC, 2012:753-758
    [11]
    Li Jiuren, Li Haiyang, Tang Guojin. Adaptive sliding mode control for approach to uncontrolled rotating satellite[J]. J. Astron., 2011, 32(4):815-822. In Chinese (李九人,李海阳, 唐国金. 对无控旋转目标逼近的自适应滑模 控制[J]. 宇航学报, 2011, 32(4):815-822)
    [12]
    Li Peng, Yue Xiaokui, Yuan Jiangping. Coupled backstepping control for spacecraft to approach with a tumbling non-cooperative object during the final phase[J]. J. Harbin Ins. Tech., 2013, 45(1):94-100. In Chinese (李鹏, 岳晓奎, 袁建平. 对翻滚非合作目标终端逼近的姿轨耦合反步控制[J]. 哈尔滨工业大学学报, 2013, 45(1):94-100)
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