Boundary control for attitude tracking and vibration suppression of large space truss structure

Author(s):  
Shilei Cao ◽  
Mingying Huo ◽  
Naiming Qi ◽  
Ce Zhao
2004 ◽  
Vol 11 (3-4) ◽  
pp. 173-186 ◽  
Author(s):  
L. Gaul ◽  
H. Albrecht ◽  
J. Wirnitzer

The present approach for vibration suppression of flexible structures is based on friction damping in semi-active joints. At optimal locations conventional rigid connections of a large truss structure are replaced by semi-active friction joints. Two different concepts for the control of the normal forces in the friction interfaces are implemented. In the first approach each semi-active joint has its own local feedback controller, whereas the second concept uses a global, clipped-optimal controller. Simulation results of a 10-bay truss structure show the potential of the proposed semi-active concept.


2016 ◽  
Vol 13 (04) ◽  
pp. 1641021 ◽  
Author(s):  
Zhiqin Cai ◽  
Yibei Zhang ◽  
Xuefu Li ◽  
Bingbing Jin

In this paper, vibration control algorithms for a large space truss structure are investigated. First, a precise integration method is used to solve the differential equation such that the validity and efficiency of the algorithm are guaranteed. Second, on the basis of the discrete algebraic equation combined with the decentralized control theory, the solving method of the control force based on the linear quadratic (LQ) optimal control theory is improved. Third, a new control method, the eigenvalue control method, is proposed in this paper, and its relationship with the LQ optimal control method is discussed. Finally, these two control methods are applied to the structure to analyze the effectiveness of vibration suppression. The simulation results show that the proposed algorithms can quickly suppress the vibration of a large space truss structure.


2014 ◽  
Vol 971-973 ◽  
pp. 860-863 ◽  
Author(s):  
Bao Xian Jia ◽  
Feng Gao ◽  
Wen Feng Bian

This paper works on the vibration control of the space truss structure. The damper made of viscoelastic composite was designed according to the configuration parameters of the truss structure. The parameters of damper were obtained by using the method of modal strain energy. The optimal position configuration of the damper was determined. The truss in the time domain and frequency domain was analyzed. The dynamic characteristics of three structures which are without damper, with damper in the random position configuration and with damper in the optimal position configuration were compared in the sweep excitation and pulse excitation. The result shows that the structure with damper in the optimal position configuration has a great improvement in the amplitude of vibration in the first resonance region and the amplitude attenuation of the truss. The space truss structure with viscoelastic composite damper has excellent vibration control effect.


1996 ◽  
Vol 62 (602) ◽  
pp. 3818-3825
Author(s):  
Toshio FUKUDA ◽  
Hideo MATSUURA ◽  
Fumihito ARAI ◽  
Kenji NISHIBORI ◽  
Takashi OGURI ◽  
...  

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