Space robots with flexible appendages: Dynamic modeling, coupling measurement, and vibration suppression

2017 ◽  
Vol 396 ◽  
pp. 30-50 ◽  
Author(s):  
Deshan Meng ◽  
Xueqian Wang ◽  
Wenfu Xu ◽  
Bin Liang
2018 ◽  
Vol 151 ◽  
pp. 904-918 ◽  
Author(s):  
Deshan Meng ◽  
Weining Lu ◽  
Wenfu Xu ◽  
Yu She ◽  
Xueqian Wang ◽  
...  

2011 ◽  
Vol 345 ◽  
pp. 46-52 ◽  
Author(s):  
Jun Qiang Lou ◽  
Yan Ding Wei

This paper concerns the dynamic modeling and vibration control of a space two-link flexible manipulator. Two types of PZT actuators, PZT shear actuator and torsional actuator, are used to suppress the bending-torsional-coupled vibration of the space manipulator. Using extended Hamilton’s principle and the finite element method, equations of motion of the space flexible manipulator with PZT actuators and tip mass are obtained. Based on modal analyze theory, the state space model of the system is then used to design the control system. A linear quadratic regulator (LQR) controller is designed to achieve vibration suppression of the space manipulator system. From the numerical results, we can get that the proposed controller has a suitable and efficient performance suppressing the bending-torsional-coupled vibration of the space two-link flexible manipulator.


2008 ◽  
Vol 41 (2) ◽  
pp. 11148-11153 ◽  
Author(s):  
Khalid H.M. Tantawi ◽  
Daniel Alazard ◽  
Christelle Cumer

2011 ◽  
Vol 217-218 ◽  
pp. 1093-1097
Author(s):  
Long Li ◽  
Zong Quan Deng ◽  
Bing Li

Snare space grapple device is designed for grappling large in-orbit payloads. Based on describing the grappling process, dynamic modeling of capturing a free-floating vehicle with large solar sails is performed by using Newton-Euler and hybrid coordinate methods in this paper. The models considering target vehicle as a rigid central body with flexible appendages which are discrete by using finite element method.


Author(s):  
Shijie Xu ◽  
Yingzi Guan ◽  
Youhua Fan

Mechanical arms are widely used in various industrial applications, especially in the field of aerospace and data storage [1–2]. Demands of new missions have more stringent requirements than before, and not only dimensions are larger, but also the accuracy. This raises the problem of less accuracy due to vibration of large flexible structures. A great deal of research has been recently focused on vibration suppression [3–6]. All of them have their own advantages, but they are difficult to widely used because their additional requirements on the structure and so on. For this problem, works in this article built an accurate model, and then combines it with Component Synthesis Vibration Suppression (CSVS) method [7–9]. This method can enhance vibration suppression. Results show there are almost no vibration when the maneuvering stopped.


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