| Citation: | YUAN Qiufan, HUO Mingying, QI Naiming, et al. Vibration control for large flexible maneuvering spacecraft using modified positive position feedback[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(2): 375-382. doi: 10.13700/j.bh.1001-5965.2017.0101(in Chinese)
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Considering maneuvering spacecraft with high flexible appendages, the translational and rotational coupling vibration modes between flexible structures and center rigid body are excited by the simultaneous attitude and orbit maneuvering. Aimed at higher stability of attitude and orbit control of spacecraft, an integrated modified positive position feedback (MPPF) controller is proposed to suppress the vibration of flexible structure. First, dynamic model is established with translational and rotational coupling effects considered, and coupling mode parameters are calculated. Then, an integrated controller was designed to suppress the translational and rotational coupling vibration modes based on MPPF. Controller parameters were optimized through
| [1] |
杜华军, 黄文虎, 邹振祝.航天支架结构的被动振动控制[J].应用力学学报, 2002, 19(3):10-13. http://d.wanfangdata.com.cn/Periodical_yylxxb200203003.aspx
DU H J, HUANG W H, ZOU Z Z.Passive vibration control(PVC) of aerospace supporter[J].Chinese Journal of Applied Mechanics, 2002, 19(3):10-13(in Chinese). http://d.wanfangdata.com.cn/Periodical_yylxxb200203003.aspx
|
| [2] |
陕晋军, 刘暾.应用分力合成方法改善柔性系统性能的研究[J].系统仿真学报, 2002, 14(11):1536-1540. doi: 10.3969/j.issn.1004-731X.2002.11.036
SHAN J J, LIU T.Study on performance improvement of flexible systems using component synthesis method[J].Journal of System Simulation, 2002, 14(11):1536-1540(in Chinese). doi: 10.3969/j.issn.1004-731X.2002.11.036
|
| [3] |
陕晋军, 刘暾.挠性结构的输入成型与分力合成主动振动抑制方法研究[J].中国机械工程, 2002, 13(5):379-383. http://industry.wanfangdata.com.cn/dl/Export/Papers?ids=zgjxgc200205008&type=excel
SHAN J J, LIU T.Study on input shaping and component synthesis method of flexible structure[J].Chinese Journal of Mechanical Engineering, 2002, 13(5):379-383(in Chinese). http://industry.wanfangdata.com.cn/dl/Export/Papers?ids=zgjxgc200205008&type=excel
|
| [4] |
胡庆雷, 马广富.挠性航天器姿态机动控制的主动振动抑制[J].振动工程学报, 2005, 18(3):375-380. http://d.wanfangdata.com.cn/Periodical_scbgxb201201004.aspx
HU Q L, MA G F.Active vibration control of flexible spacecraft during attitude maneuver[J].Journal of Vibration Engineering, 2005, 18(3):375-380(in Chinese). http://d.wanfangdata.com.cn/Periodical_scbgxb201201004.aspx
|
| [5] |
陈勇, 陶宝祺, 刘果, 等.柔性结构振动控制的初步分析与试验研究[J].机械强度, 1998, 20(3):207-211. https://www.wenkuxiazai.com/doc/5856923a43323968011c92ae.html
CHEN Y, TAO B Q, LIU G, et al.Analysis and experimental study on the vibration control of flexible structures[J].Journal of Mechanical Strength, 1998, 20(3):207-211(in Chinese). https://www.wenkuxiazai.com/doc/5856923a43323968011c92ae.html
|
| [6] |
BALAS M J.Active control of flexible systems[J].Journal of Optimization Theory and Applications, 1978, 25(3):415-436. doi: 10.1007/BF00932903
|
| [7] |
FANSON J L, CAUGHEY T K.Positive position feedback control for large space structures[J].AIAA Journal, 1990, 28(4):717-724. doi: 10.2514/3.10451
|
| [8] |
MAMODI S N, AHMADIAN M.Active vibration control with modified positive position feedback[J].Journal of Dynamic Systems, Measurement and Control, 2009, 131(4):442-447. http://www.researchgate.net/publication/245372982_Active_Vibration_Control_With_Modified_Positive_Position_Feedback
|
| [9] |
MOHEIMANI S O R, ANDREW J F.Piezoelectric transducers for vibration control and damping[M].Berlin:Springer, 2006:9-66.
|
| [10] |
MAHMOODI S N, AHMADIAN M, INMAN D J.Adaptive modified positive position feedback for active vibration control of structures[J].Journal of Intelligent Systems and Structures, 2010, 21(6):571-578. doi: 10.1177/1045389X10361631
|
| [11] |
GENNARO D.Output stebilizama of flerible spacecraft with active vibration suppresson[J].IEEE Transactrons on Aerospace and Flearanic System, 2003, 39(3)747-759. doi: 10.1109/TAES.2003.1238733
|
| [12] |
胡庆雷, 马广富.改进型正位置反馈/变结构卫星姿态主动控制[J].振动工程学报, 2007, 20(4):324-329. http://kns.cnki.net/KCMS/detail/detail.aspx?filename=zdgc200704001&dbname=CJFD&dbcode=CJFQ
HU Q L, MA G F.Maneuvering and vibration damping of flexible spacecraft using adaptive variable structure control and suboptimal positive position feedback[J].Journal of Vibration Engineering, 2007, 20(4):324-329(in Chinese). http://kns.cnki.net/KCMS/detail/detail.aspx?filename=zdgc200704001&dbname=CJFD&dbcode=CJFQ
|
| [13] |
袁国平, 史小平, 李隆.飞行器姿态机动的自适应鲁棒控制及主动振动抑制[J].振动与冲击, 2013, 32(12):110-115. doi: 10.3969/j.issn.1000-3835.2013.12.021
YUAN G P, SHI X P, LI L. Adaptive robust attitude maneuver control of a flexible spacecraft with active vibration suppression[J].Journal of Vibration and Shock, 2013, 32(12):110-115(in Chinese). doi: 10.3969/j.issn.1000-3835.2013.12.021
|
| [14] |
GASBARRI P, SABATINI M, LEONANGELI N, et al.Flexibility issues in discrete on-off actuated spacecraft:Numerical and experimental tests[J].Acta Astronautica, 2014, 101:81-97. doi: 10.1016/j.actaastro.2014.04.012
|
| [15] |
SABATINI M, GASBARRI P, PALMERINI G B.Delay compensation for controlling flexible space multibodies:Dynamic modeling and experiments[J].Control Engineering Practice, 2015, 45:147-162. doi: 10.1016/j.conengprac.2015.09.013
|
| [16] |
OMIDI E, MCCARTY R, MAHMOODI S N. Implementation of modified positive velocity feedback controller for active vibration control in smart structures[C]//Conference on Active and Passive Smart Structures and Integrated Systems. Bellingham: SPIE, 2014, 9057: 90571N. http://spie.org/x648.xml?product_id=2044478
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