DEVELOPMENT OF 30KVA INVERTER USING SIC MOSFET FOR 180◦C AMBIENT TEMPERATURE OPERATION Feng Qi1, Miao Wang, Longya Xu, Bo Zhao, Zhe Zhou 1The Ohio State University, USA -Smart Grid Research Institute of SGCC, China

DEVELOPMENT OF 30KVA INVERTER USING SIC MOSFET

FOR 180◦C AMBIENT TEMPERATURE OPERATION

Feng Qi1, Miao Wang1, Longya Xu1, Bo Zhao2, Zhe Zhou2

1The Ohio State University, USA

2Smart Grid Research Institute of SGCC, China

COBEP 2015 : 2015 IEEE 13th Brazilian Power Electronics Conference and 1st Southern Power Electronics Conference (COBEP/SPEC)

Abstract

 A 30kVA SiC MOSFET inverter is developed for 180°C ambient temperature operation.The entire inverter system is designed for high temperature (HT) except the DSP control circuit in room temperature environment. Power structure is designed using SiC MOSFETs, HT capacitors and a liquid cooling plate. The gate drivers with protections and power structure are placed in HT environment of 180○C. The prototype inverter has been built and successfully tested in 180○C environment at 30kVA for accumulative 5 hours without any problems.

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LLC DC to DC 공진 컨버터의 고주파 변압기 최적화 설계에 관한 연구 A study on an optimal design of the high frequency transformer in LLC DC to DC resonant converter -Jong-Hae Kim

 LLC DC to DC 공진 컨버터의 고주파 변압기 최적화 설계에 관한 연구 A study on an optimal design of the high frequency transformer in LLC DC to DC resonant converter 김 종 해* 

★ Jong-Hae Kim* 

 Abstract 

This paper presents an optimal design of the slim type high frequency transformer used in the LLC DC to DC resonant converter for 65-inch UHD-TV with the rated power of 315W. This paper also performs an optimal design of the slim type high frequency through core loss analysis, AC winding loss analysis, and optimization design of the winding arrangement of the LLC resonant transformer. Particularly, the high-efficiency and slim type high frequency transformer based on the obtained results from theoretical analysis in this paper is constructed in the interleaved and vertical winding structures of its transformer to realize the winding method of automatic type and minimize AC winding loss. The primary and secondary windings of the slim type high frequency transformer the vertical winding structure proposed in this paper used the Litz-wire windings, PCB and copper plate windings, respectively. Finally, an optimal design of the slim type high frequency transformer proposed in this paper was carried out through the experimental results to confirm the validity of theoretical analysis based on the simulation results using Maxwel

j.inst.Korean.electr.electron.eng.Vol.27,No.4,587~600,December 2023 논문번호 23-04-31 https：//doi.org/10.7471/ikeee.2023.27.4.587l 2D and 3D tool.

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ORIGINAL SOURCE:https://ikeee.jams.or.kr/co/locale.kci?lang=en_US

단상 태양광 발전용 고효율 벅부스트 하프브리지 인버터 A High-efficiency Buck-boost Half-bridge Inverter for Single-phase Photovoltaic Generation-Hyung-Min Ryu

단상 태양광 발전용 고효율 벅부스트 하프브리지 인버터 A High-efficiency Buck-boost Half-bridge Inverter for Single-phase Photovoltaic Generation 류 형 민* ★ Hyung-Min Ryu*

 j.inst.Korean.electr.electron.eng.Vol.27,No.4,450~455,December 2023

 Abstract 

Among single-phase photovoltaic inverters that can avoid excessive leakage current caused by the large parasitic capacitance of photovoltaic panels, a boost converter followed by a half-bridge inverter is the simplest and has the smallest leakage current. However, due to the high DC-link voltage, the rated voltage of the switching devices is high and the switching loss is large. This paper proposes a new circuit topology which can operate as a buck-boost inverter by adding two bidirectional switches to the output side of the half-bridge inverter instead of removing the boost converter. By reducing two stages of power conversion through the high-voltage DC-link to one stage, power loss can be reduced without increasing costs and leakage current. The feasibility of the proposed circuit topology is verified by computer simulation and power loss calculation.

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Analysis and design of –PID controller for a quadrotor in the frequency domain- Alhassan Dodo Adamou Soudeize* , Ji-Sun Park* , Ho-Lim Choi*-j.inst.Korean.electr.electron.eng.Vol.28,No.3,253~260,September 2024

 Analysis and design of –PID controller for a quadrotor in the frequency domain Alhassan Dodo Adamou Soudeize*, Ji-Sun Park*, Ho-Lim Choi*

 Abstract 

In this paper, we propose an -PID controller for the altitude control of the quadrotor from the ground by considering the mass of the AR Drone and external disturbance. The first part consists of modeling the quadrotor and carrying out the system analysis with the proposed controller and the second part consists of carrying out the experiment in the lab to show that our control method along with the analysis coincides with the experiment.

 

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Quadcopter stabilization by using PID controllers- Luis E. Romero, David F. Pozo, Jorge A. Rosales Universidad de Las Américas, Escuela Politécnica Nacional

 Quadcopter stabilization by using PID controllers Luis E. Romero1, David F. Pozo2, Jorge A. Rosales3 1 Escuela Politécnica Nacional, Ladrón de Guevara E11 - 253, Quito, Ecuador, EC170127. 2 IEEE Member, Universidad de Las Américas, Av. De los Granados E12-41 y Colimes esq., Quito, Ecuador, EC170125. 3 IEEE Member, Escuela Politécnica Nacional, Ladrón de Guevara E11 - 253, Quito, Ecuador, EC170127. Autores para correspondencia: luiseduromp@hotmail.com, david.pozo@udla.edu.ec, andres.rosales@epn.edu.ec Fecha de recepción: 21 de septiembre de 2014 - Fecha de aceptación: 17 de octubre de 2014 

 RESUMEN 

En este trabajo se presenta la estabilización de un cuadricóptero mediante el uso de controladores PID para la regulación de sus 4 movimientos básicos: ángulos de alabeo, cabeceo, guiñada y altitud. La estabilización del sistema se realiza a partir de un modelo simplificado que facilita la implementación de controladores en un sistema SISO, demostrando efectividad dentro de un rango de ±10° para los ángulos de alabeo y cabeceo y rango completo en guiñada y altitud. El módulo del controlador PID es diseñado para ser usado en cuadricópteros comerciales y ha sido implementado en base a sensores inerciales y ultrasónicos. Además, el sistema cuenta con una interface para observar el desempeño de la aeronave durante el vuelo.

 ABSTRACT

 This work presents the stabilization of a quadcopter by using PID controllers to regulate its four basic movements: roll, pitch, yaw angles, and altitude. The stabilization of the system is made from a simplified model which makes easier the implementation of controllers on a SISO system, showing effectiveness within a range of ±10° for a roll and pitch angles and a full range on yaw angle and altitude. The PID controller module is designed to be used with commercial quadcopters and it has been implemented using inertial and ultrasonic sensors. Furthermore, the system also features a wireless interface to observe the aircraft performance during the flight.

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https://publicaciones.ucuenca.edu.ec/ojs/index.php/maskana/article/view/585/509