Tension control strategy for TSS retrieval process based on backstepping control method

[1] Cartmell M P,McKenzie D J.A review of space tether research[J].Progress in Aerospace Sciences,2008,44:1-21 [2] Kumar K D.Review of dynamics and control of nonelectrodynamic tethered satellite systems[J].Journal of Spacecraft and Rockets,2006,43(4):705-720 [3] 于绍华,刘强,杨林娜.绳系卫星系统二维平面运动和常规动力学[J].宇航学报,2000,21(4):15-24 Yu Shaohua,Liu Qiang,Yang Linna.Regular dynamics of inplanar motion oftethered satellite system[J].Journal of Astronautics,2000,21(4):15-24( in Chinese) [4] 黄奕勇,杨乐平.改进的绳系卫星系统距离速率控制律[J].上海航天,2007(3):30-33 Huang Yiyong,Yang Leping.The research on the modified range rate control law for tethered satellite[J].Aerospace Shanghai,2007(3):30-33(in Chinese) [5] Williams P.Optimal deployment/retrieval of tethered satellites[J].Journal of Spacecraft and Rockets,2008,45(2):324-343 [6] Williams P.Optimal deployment/retrieval of tethered satellites formation spinning in the orbital plane[J].Journal of Spacecraft and Rockets,2006,43(3):638-650 [7] Jin D P, Hu H Y.Optimal control of a tethered subsatellite of threedegrees of freedom[J].Nonlinear Dynamics,2006(46):161-178 [8] 郑敏捷.退步控制设计方法在航天器姿态控制系统中的应用 .北京:北京航空航天大学宇航学院,2007 Zheng Minjie.Spacecraft attitude control system design via backstepping control method .Beijing: School of Astronautics,Beijing University of Aeronatics and Astronantics,2007( in Chinese)