Volume 22, Issue 3 (JIAEEE Vol.22 No.3 2025)                   Journal of Iranian Association of Electrical and Electronics Engineers 2025, 22(3): 0-0 | Back to browse issues page

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Radmanesh H. Design and Analysis of a Novel High Step-Up DC-DC Converter for Aircraft Power Systems. Journal of Iranian Association of Electrical and Electronics Engineers 2025; 22 (3)
URL: http://jiaeee.com/article-1-1623-en.html
Design and Analysis of a Novel High Step-Up DC-DC Converter for Aircraft Power Systems
Hamid Radmanesh *
Shahid Sattari Aeronautical University of Science and Technology
Abstract:   (20 Views)
Abstract: This paper presents a new topology for a high step-up DC-DC converter utilizing a combination of voltage multiplier and coupled inductor. This topology is well suited for use in the aviation industry for more electric aircrafts. With the proposed topology, high voltage gain can be achieved with low duty cycle, resulting in low voltage stress among the active components. This reduces conduction loss and increases the converter's efficiency. Additionally, the proposed topology features an active switch, enabling simple control operation, and allows for continuous input current. Experimental test results on a 200W DC-DC prototype are used to confirm the steady-state performance and theoretical achievements of the proposed topology.
 
Keywords: Coupled Inductor, Voltage Multiplier Cell, High Step-Up, Continuous Input Current.
     
Type of Article: Research | Subject: Power
Received: 2023/08/12 | Accepted: 2024/10/13
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