[1] Smith O J M. Feedback control systems. New York: McGraw-Hill Book Company, 1958: 331-345.[2] Singer N C, Seering W P. Preshaping command inputs to reduce system vibration. Journal of Dynamic Systems, Measurement, and Control, 1990, 112: 76-82.[3] Tuttle T D, Seering W P. A zero-placement technique for designing shaped inputs to suppress multiple-mode vibration. Proceedings of the American Control Conference, 1994, 3: 2533-2537.[4] Pao L Y. Multi-input shaping design for vibration reduction. Automatica, 1999, 35(1): 81-89.[5] Hyde J M, Seering W P. Using input command pre-shaping to suppress multiple mode vibration. International Conference on Robotics and Automation, 1991: 2604-2609.[6] Tewari A. Active vibration suppression of spacecraft with rate-weighted optimal control and multi-mode command shaping. AIAA-2004-5296, 2004.[7] Lau M A, Pao L Y. Input shaping and time-optimal control of flexible structures. Automatica, 2003, 39(5): 893-900.[8] Wie B, Sinha R, Sunkel J, et al. Robust fuel and time optimal control of uncertain flexible space structure. Proceedings of the American Control Conference, 1993: 2475-2479.[9] Pao L Y, Singhose W E. On the equivalence of minimum time input shaping with traditional time-optimal control. Proceeding of the Conference on Control Application, 1995.[10] Singhose W E, Kim D, Kenison M. Input shaping control of double-pendulum bridge crane oscillations. Journal of Dynamic Systems, Measurement, and Control, 2008, 130(3): 034504.[11] Singhose W E, Derezinski S, Singer N C. Extra-insensitive input shapers for controlling flexible spacecraft. Journal of Guidance, Control, and Dynamics, 1996, 19(2): 385-391.[12] Singhose W E, Pao L Y, Seering W P. Time-optimal rest-to-rest slewing of multi-mode flexible spacecraft using ZVD robustness constraints. AIAA-1996-3845, 1996.[13] Yavuz H, Mstkogˇlu S, Kapucu S. Hybrid input shaping to suppress residual vibration of flexible systems. Journal of Vibration and Control, 2011, 18(1): 132-140.[14] Kong X R, Yang Z X, Ye D, et al. Feedback control in conjunction with input shaping for flexible spacecraft vibration suppression. Journal of Vibration and Shock, 2010, 29(3): 72-76. (in Chinese) 孔宪仁, 杨正贤, 叶东, 等. 基于输入成形的柔性航天器振动闭环抑制方法研究. 振动与冲击, 2010, 29(3): 72-76.[15] Hu Q L, Ma G F. Flexible spacecraft attitude maneuvering and vibration damping using variable structure control input shaping. Journal of Harbin Institude of Technology, 2006, 38(10): 1769-1776. (in Chinese) 胡庆雷, 马广富. 基于变结构/输入成形的航天器振动抑制方法. 哈尔滨工业大学学报, 2006, 38(10): 1769-1776.[16] Hu Q L, Ma G F. Active vibration suppression in flexible spacecraft with mismatched uncertainty via sliding mode/shaped input control. Journal of Vibration and Shock, 2007, 26(6): 133-138. (in Chinese) 胡庆雷, 马广富. 基于滑模输出反馈与输入成形控制相结合的挠性航天器主动振动抑制方法. 振动与冲击, 2007, 26(6): 133-138.[17] Cong B L, Liu X D, Chen Z. Adaptive integral sliding mode control for rigid spacecraft attitude tracking. Acta Aeronautica et Astronautica Sinica, 2013, 34(3): 620-628. (in Chinese) 丛炳龙, 刘向东, 陈振. 刚体航天器姿态跟踪系统的自适应积分滑模控制. 航空学报, 2013, 34(3): 620-628.[18] Wheeler G, Su C Y, Stepanenko Y. A sliding mode controller with improved adaption laws for the upper bounds on the norm of uncertainties. Automatica, 1998, 34(12): 1657-1661. |