Double-Loop Push-Pull Forward DC/DC Converter Control System

Abstract:

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.

• Periodical: Applied Mechanics and Materials (Volumes 130-134)
• Pages: 3365-3369
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.130-134.3365
• Online since: October 2011
• Authors: Gai Li Yue, Rong Li, Chao Chen, Xiao Long Wei
• Keywords: Air Static Inverter, Dc-Dc Converter, Double-Loop, Push-Pull Forward

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