2019 European Space Power Conference (ESPC)最新文献_第10页

Transformer optimization for 3D PLUS Universal RCN Front End converter 3D PLUS通用RCN前端转换器的变压器优化

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932006

Cédric Colonna, P. Dubus, D. Labrousse

引用次数: 0

High-Efficiency Low Voltage/High Current Power Supplies for High Performance Digital Equipment by using GaN FET Technology 基于GaN场效应管技术的高性能数字设备的高效低压/大电流电源

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8931977

Franz Stoegerer, T. Panhofer

{"title":"High-Efficiency Low Voltage/High Current Power Supplies for High Performance Digital Equipment by using GaN FET Technology","authors":"Franz Stoegerer, T. Panhofer","doi":"10.1109/ESPC.2019.8931977","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8931977","url":null,"abstract":"High performance processing boards using ASICs and reconfigurable FPGAs require particular power supplies with voltages below 1 V and current capabilities up to 50 A. High efficiency is mandatory for low power consumption and thermal reasons and is considered as most important goal for the DCDC converter. Off-the-shelf radiation hardened point-of-load (POL) converters are not optimized for such an application. Most devices are limited to approximately 10 A and show maximum efficiency at approximately half load current. Only a few parts offer the possibility for parallel operation to increase the current capability. Apart from the non-isolating POL converters also high-current supplies based on an isolated converter topology with good efficiency are available on the market. The efficiency of both concepts relies on high-performance/low-on-resistance FETs, and GaN technology seems to be a very attractive solution. This paper evaluates discrete designs of a non-isolating POL converter and an isolating converter based on GaN FETs regarding their suitability for low voltage/high current applications. Beside of theoretical investigations, experimental results gained from laboratory prototypes are presented.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"8 1","pages":"1-7"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"81591992","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 1

Identification of COTS Cells to Meet Space Market Segment Requirements 识别COTS单元以满足空间细分市场的要求

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932047

Alex Clarke, R. Buckle

引用次数: 1

Power Assessment Indices of Solar Arrays under MPPT and DET methods for Spacecraft 航天器太阳能电池阵在MPPT和DET方法下的功率评估指标

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932076

Zhang Xuan, Kang Qing, Y. Wentao, Xing Jie, Li Feng, You Xiangan

引用次数: 2

RHPWM01 Radiation hardened dual channel current mode PWM RHPWM01抗辐射双通道电流模式PWM

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932054

S. Pappalardo, Carmelo Ardizzone, Orazio Principato, Agatino Alessandro, I. Mirabella, F. Tonicello, Michail Tourloukis

引用次数: 0

SEGR and PIGS Failure Analysis of SiC Mosfet SiC Mosfet的SEGR和pig失效分析

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8931999

F. Pintacuda, S. Massett, E. Vitanza, M. Muschitiello, V. Cantarella

引用次数: 0

Efficient 200W Low Voltage DC/DC for Redundant On-Board Processing Systems 高效200W低压DC/DC冗余板载处理系统

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932052

M. Persson, S. Petersen, B. Søderberg

引用次数: 0

Design and Modeling of useful Tool for Satellite Solar Array Preliminary Sizing and Power System Analysis 卫星太阳能电池阵初步选型及电力系统分析实用工具的设计与建模

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932060

A. H. Dida

{"title":"Design and Modeling of useful Tool for Satellite Solar Array Preliminary Sizing and Power System Analysis","authors":"A. H. Dida","doi":"10.1109/ESPC.2019.8932060","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932060","url":null,"abstract":"Design for any satellite includes its electrical power needs and the system to supply them. The availability of solar energy has encouraged the development of solar cell arrays which are major structural element for providing power generation of many spacecraft. Solar cell array design must be instituted early in the development of satellite design mission. The high performance of satellite solar cell array design depends on the intensity of sunlight incident, the conversion efficiency of solar cells and the interaction of the array with satellite. The advances in technology are nowadays allowing the production of solar cells in different sizes and more importantly with increased efficiencies exceeding 30%. The most efficient technology for electricity generation from solar energy is multi-junction solar cells. Simplicity, relatively modest cost, and high reliability have caused these solar cells based on GaAs to be chosen for supplying the electrical power system of almost satellites. The aim of this research work was designed and modeled a useful tool for satellite solar array preliminary sizing and power system analysis of our spacecraft system. We had also simulated and compared a various solar cells to investigate their performance in terms of efficiency to select the adequate type of cells that should be chosen to insure performance at the required output to the end of the mission while minimizing costs. The useful tool of satellite solar array sizing was validated using data Alsat-1 project. The required area and weight of satellite solar array are calculated and selected to provide the required end-of-mission power without complicating installation of cells.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"82 1","pages":"1-4"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"75958336","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 2

Revised stability criteria for cascaded DC-DC converters in space applications 修订的空间应用级联DC-DC变换器稳定性标准

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932078

M. Triggianese, H. Carbonnier, F. Tonicello

引用次数: 1

EXOMARS 2020 mission Descent module & Rover batteries EXOMARS 2020任务下降模块和漫游者电池

2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8931994

Hélène Tricot, P. Brochard

引用次数: 2