Double-loop Push-pull Forward DC/DC Converter Control System
With the continuous development of aviation technology, reliability requirements for air power is growing. As an important component, air static inverter air power has been studied extensively. In this paper, we study the following about the design of the front push-pull forward converter of Aeronautical Static Inverter: First, we design the Push-Pull Forward DC/DC converter control system on the basis of small-signal modeling; Secondly set control system parameters ; Finally, Through the simulation in MATLAB Simulink, we verify the design of the converter control parameter is reasonable, and then verify that Double-loop push-pull Forward DC/DC converter control system in the aviation static inverter is effectiveness.
Air Static Inverter Double-loop Push-pull Forward DC/DC Converter
Gai-Li Yue Rong Li Chao Chen Xiao-Long Wei
School of Electrization and Control Engineering, Xian University of Science and Technology,Xian Sh School of Automation, Northwestern Polytechnical University, Xian , Shaanxi China, 710072
国际会议
合肥
英文
3365-3369
2011-09-23(万方平台首次上网日期,不代表论文的发表时间)