Intelligent measurement and control device for aeroplane environment control system

The utility model relates to an intelligent measurement and control device for an environment control system of an aeroplane. The utility model comprises an airflow temperature sensor of an entrance of an aeroplane cockpit, a temperature selector and a flow adjusting valve in the aeroplane cockpit, an airflow temperature sensor of an entrance of an electronic compartment cockpit, a pressure sensor and a flow adjusting valve in the electronic compartment cockpit, a data acquisition SCM, a motor control SCM, a main control algorism SCM and an upper supervisory control computer. The utility model shares the information of every subsystems in a public control system by an airborne data bus line. Commands are transmitted by the comprehensive dispatch of the upper supervisory control computer. The main control algorism SCM executes the optimized control decision. The data acquisition SCM and the motor control SCM directly integrate and measure the raw information and control the terminal. The utility model combines modern high technologies such as artificial intelligence technology as fuzzy inference and expert system, communication and computer technology, motor speed regulation, sensor technology, etc. into a whole. Thereby, the utility model can become the main stream direction of the development in measurement and control technology of the environment control system of the aeroplane.