Dynamic testing method for space docking mechanism

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.

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