The invention relates to the technical field of spacecrafts, in particular to an electric propulsion
fault analysis method and
system based on
system simulation, and the method comprises the steps: classifying, organizing and storing
test data of an electric propulsion vacuum bin, managing the
test data through a
database, carrying out null cleaning on the data, filtering the data, dividing working conditions, carrying out
statistical analysis, constructing features, and carrying out
dimensionality reduction. The method comprises the steps of building a
system simulation model, building an
anomaly detection model, mining threshold rules, building a
trend prediction model and building a comprehensive judgment model. According to the method, a deterministic model in a
design process, a ground ignition test and a large amount of on-
orbit telemetry data are utilized, real-time accurate interpretation and state evaluation of on-
orbit data are realized through
logic simulation operation, and a potential fault mode is effectively identified. Compared with a traditional electric propulsion on-
orbit state evaluation and fault diagnosis method, the electric propulsion on-orbit state evaluation and fault diagnosis method has higher accuracy and efficiency.