Design of Measurement and Control System on Fuel Tank Test Platform

Platform for fuel system test is used to simulate the flight attitude of an unmanned aerial vehicle (UAV), verify fuel system's performance and reliability, and help to improve and solve the design. This platform could simulate attitude angle, pressure and the engine fuel consumption of a tank. Detailed realization of servo tracking control based on BP neutral network PID controller is presented. The methods described could be applied to other hydro mechanical devices.