A method based on the metamorphic principle is proposed for the analysis of the configuration design of a space truss deployable mechanism. The configuration change and correspondent topological graphs and adjacency matrixes at different work-stage of the mechanism,which is helpful to completely understand the composition and change rules of the metamorphic mechanism,are analyzed to indicate the metamorphic relationship in one working cycle. Furthermore,the static distance matrix,dynamic distance matrix and stiffness matrix of the mechanism are derived to assess the ability of the designed configuration to reveal some of the topological characteristics like compactness,dynamic sensitivity and stiffness. Using this proposed method in a space truss deployable mechanism helps the designer to evaluate its performance at the conceptual stage of design and make a rapid,reasonable selection for configuration design,which provides means for processing its type of analysis by computer.
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