Abstract
With the development of electro-hydraulic integration technology, the control accuracy, complexity and dynamic response characteristics of aircraft hydraulic system actions have become a hot topic in the field of hydraulics. The traditional hydraulic system design method mainly uses the designer’s knowledge and experience to construct a dynamic system with real components, and then tests on the system, this method is more difficult to adjust parameters. Therefore, taking the hydraulic system of an aircraft as an example, the simulation model of each component of the system is established by using modeling and simulation technology and graphical modeling method, so as to provide support for aircraft fault diagnosis and prediction.
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