A distributed system for aircraft hydraulic system simulation test based on LXI

Aircraft hydraulic systems are used to actuate flight control surfaces, thrust vectoring and reversing mechanisms, landing gear, cargo doors, and in some cases, weapon systems. In hydraulic system simulation test, a test and measurement system was developed and programmed on a prototype. It is a best option that research and development distributed test and measurement system for aircraft hydraulic system simulation test which was used to collect many channel and many type signals which separated in differently position. In order to improve the software reusability and development efficiency of test and measurement software, after analyzing the features and requirements of the test object, one framework development approach for aircraft hydraulic simulation test was presented. This approach makes full use of such technologies as the unified modeling language (UML) and design patterns. This method can greatly reduce the effort required for all kinds of hydraulic simulation test framework development and achieve higher productivity, better reusability, extend ability and maintainability.