| Citation: | ZHANG X Y，ZHANG F Q，GUO R X，et al. A fault propagation path analysis method for flight control system based on improved FPPN[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1829-1841 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0520
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In view of the multi-redundancy and multi-closed-loop structural characteristics of the flight control system, the directed graph model and the fuzzy Petri net (FPN) model were used, and a fuzzy probability Petri net (FPPN) model for fault propagation of the flight control system was constructed, so as to solve the fault propagation path of the flight control system with a specific structure. The improved FPPN model consisted of three parts:directed graph model of flight control system, quantitative calculation model for fault propagation characteristics, and FPPN model for fault propagation. A directed graph model of system fault propagation was built by analyzing the functional behavior and physical structure of the flight control system through object-oriented technology and utilizing complex network theory. The Floyd algorithm was introduced to carry out the system coupling correlation analysis, and the system fault propagation characteristics were defined based on the two indicators of node degree and edge betweenness. On the basis of the directed graph model, the corresponding structure mapping rules were proposed. The FPPN model for fault propagation of the flight control system was constructed. With the improved parameter quantization method, two reasoning algorithms were set to effectively analyze the fault propagation paths of the system with multi-redundancy and closed-loop structure characteristics. Through numerical analysis and example verification, the typical fault propagation path of the flight control system and the status value of the relevant nodes on the path were obtained, so as to verify the effectiveness of the proposed method.
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