Vibration Isolation Platform with Multiple Tuned Mass Dampers for Reaction Wheel on Satellites

被引:6
作者
Zhang, Yao [1 ]
Zhang, Jingrui [1 ]
Zhai, Guang [1 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
关键词
ATTITUDE-CONTROL;
D O I
10.1155/2013/574072
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Vibration isolation is a direct and effective approach to improve the ultraprecise pointing capability of an imaging satellite. To have a good trade-off between the resonance amplitude and the high frequency attenuation for the original vibration isolation platform, a novel vibration isolation system for reaction wheel (RW), including a multistrut vibration isolation platform and multiple tuned mass dampers, is proposed. The first step constructs the integrated satellite dynamic model including the RWs and the vibration isolation systems, while the static and dynamic imbalances of the rotor and base movements are considered in the modeling process. The transmissibility matrix of the vibration isolation system is then obtained, and its frequency domain characteristics are described. The third part presents the application of the vibration isolation system for RWs. The effective attenuation of RW disturbances by the new vibration isolation system is illustrated, and its safety performance is also verified. Finally, using the reasonable parameters of the vibration isolation system, its performance on the satellite is testified by numerical simulations. The study shows that the novel vibration isolation system presented cannot only be successfully applied to a satellite but also improve the attitude stability.
引用
收藏
页数:14
相关论文
共 23 条
[1]   Jitter Control for Imaging Spacecraft [J].
Agrawal, Brij .
RAST 2009: PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES, 2009, :615-620
[2]  
Basdogan I., 2000, P CONTR VIBR NOIS NE
[3]  
Blaurock C, 2005, OPTICAL MODELING PER, V5867-34, P1
[4]   Vibration isolator for large space telescopes [J].
Bronowicki, AJ .
JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (01) :45-53
[5]  
Cheng YH, 2011, INT J INNOV COMPUT I, V7, P4149
[6]   A Newton-Euler formulation for the inverse dynamics of the stewart platform manipulator [J].
Dasgupta, B ;
Mruthyunjaya, TS .
MECHANISM AND MACHINE THEORY, 1998, 33 (08) :1135-1152
[7]  
Davis L. P., 1986, N8722702 NASA
[8]  
Dewell L., 2005, P SOC PHOTO-OPT INS, P1
[9]   Dynamic analysis of space structures with multiple tuned mass dampers [J].
Guo, Y. Q. ;
Chen, W. Q. .
ENGINEERING STRUCTURES, 2007, 29 (12) :3390-3403
[10]  
Hoang N., 2007, Engineering structures, V29, P1548