空间绳系机器人抓捕后复合体姿态协调控制

doi:10.7527/S1000-6893.2013.0323

Abstract

Abstract:

The coordinated attitude control of the combination system after the target is captured by the Space Tethered Robot is studied in this paper. Firstly, a combination system dynamic model is established and its dynamic characteristics are analyzed. Secondly, taking into consideration such combination system characteristics as the limitation of fuel and thruster force, two attitude controllers are designed: one is the coordinated controller of the tether force and thruster force and the other the sliding mode controller of the thruster force only. The combination system attitude is controlled by these two controllers which are utilized according to the switch condition. Finally, the numerical simulation is conducted to validate the feasibility of the proposed coordinated control method. The simulation result shows the combination system attitude can be controlled by the coordinated control method and the fuel consumption is effectively reduced.

Key words: tethered space robot, post-capture, attitude control, coordinated control, sliding mode control

CLC Number:

V448.234

WANG Dongke, HUANG Panfeng, MENG Zhongjie, CAI Jia. Coordinated Attitude Control of the Combination System After Target Capture by a Tethered Space Robot[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(8): 1998-2006.

References

[1] Zhai G, Qiu Y, Liang B, et al. On-orbit capture with flexible tether-net system. Acta Astronautica, 2009, 65(5-6):613-623.

[2] Xu X D, Huang P F, Meng Z J, et al. Space tethered robot optimal trajectory planning for medium approaching range based on velocity impulse. Acta Aeronautica et Astronautica Sinica, 2012, 33(8):1531-1539. (in Chinese) 徐秀栋,黄攀峰,孟中杰,等.基于速度增量的空间绳系机器人中距离逼近过程最优轨迹规划.航空学报,2012,33(8):1531-1539.

[3] Cartmell M P, McKenzie D J. A review of space tether research. Progress in Aerospace Science, 2008, 44(1):1-21.

[4] Nohmi M, Yamamoto T, Takagi Y. Microgravity experiment for attitude control of a tethered body by arm link motion. Proceedings of IEEE International Conference on Mechatronics and Automation, 2007: 265-276.

[5] Nohmi M. Attitude control of a tethered space robot by link motion under microgravity. Proceedings of the 2004 IEEE International Conference on Control Applications, 2004:424-429.

[6] Wen H, Chen H, Jin D P, et al. Deployment and attitude control of a tethered sub-satellite with controllable arm. Acta Mechanica Sinica, 2012, 44(2):408-414. (in Chinese) 文浩, 陈辉, 金栋平, 等. 带可控臂绳系卫星释放及姿态控制. 力学学报, 2012, 44(2): 408-414.

[7] Kumar K D,Kumar K. Satellite pitch and roll attitude maneuvers through very short tethers. Acta Astronautica, 1999, 44(5):257-265.

[8] Beda P B. On requirements for attitude dynamics and stability control for tethered satellite systems. JSME International Journal,Series C: Mechanical Systems, Machine Elements and Manufacturing, 2000, 43(3):678-683.

[9] Mori O, Matunaga S. Formation and attitude control for rotational tethered satellite. Journal of Spacecraft and Rockets, 2007, 43(3):678-683.

[10] Chang I, Park S Y, Choi K H. Nonlinear attitude control of a tether-connected multi-satellite in three-dimensional space. IEEE Transactions on Aerospace and Electronic Systems, 2010, 46(4): 1950-1968.

[11] Menon C, Bombardelli C. Self-stabilising attitude control for spinning tethered formations. Acta Astronautica, 2007, 60(10):828-833.

[12] Liu H D, Liang B, Li C, et al. Research on coordinate control method for stabilizing a coupling system after the spacecraft is captured. Journal of Astronautics, 2012, 33(7): 920-929. (in Chinese) 刘厚德,梁斌,李成,等.航天器抓捕后复合体系统稳定的协调控制研究.宇航学报, 2012, 33(7):920-929.

[13] Aghili F.Optimal control of a space manipulator for detumbling of a target satellite. International Conference on Robotics and Automation, 2009:3019-3024.

[14] Xing G Q, Parvez S A. Nonlinear attitude state tracking control for spacecraft. Journal of Guidance Control, and Dynamics, 2001, 24(3):624-626.

[15] Crassidis J L, Markley F L. Sliding mode control using modified Rodrigues parameters. Journal of Guidance control and Dynamics, 1996; 19(6):1381-1383.

Coordinated Attitude Control of the Combination System After Target Capture by a Tethered Space Robot

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