Dynamic testing method for space docking mechanism
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 December 2003
Abstract
In this paper, dynamic behavior of docking mechanism during its acquisition period is analyzed. The results show that the docking mechanism can be modeled as a six‐freedom rigid body with a flexible support during this period, i.e. a typical structure. Because there exists nonlinear characteristics due to spacing, retardation, and friction in transmission elements and elements themselves, the theoretical analysis shows that docking mechanism can be simplified as a linear system and its dynamic characteristics determined through testing‐spectral function recognition method based on the linear vibration theory and corresponding software, after weakening effects of nonlinear factors. In order to determine whether docking mechanism has basic characteristics of a linear structure, some experiments have been carried out. The results show that testing‐spectral function recognition method can be used in dynamic systems.
Keywords
Citation
Yang, Z., Xi‐Bin, C. and Zhao‐Wei, S. (2003), "Dynamic testing method for space docking mechanism", Aircraft Engineering and Aerospace Technology, Vol. 75 No. 6, pp. 600-604. https://doi.org/10.1108/00022660310503084
Publisher
:MCB UP Ltd
Copyright © 2003, MCB UP Limited