Goutham Selvaraj, K. Rajashekara, Krishna Raj Ramachandran Potti
{"title":"基于无刷同步发电机的飞机直流电源系统中减小直流电容的改进前馈控制器","authors":"Goutham Selvaraj, K. Rajashekara, Krishna Raj Ramachandran Potti","doi":"10.1109/ITEC51675.2021.9490190","DOIUrl":null,"url":null,"abstract":"This paper proposes feedforward control improvements for minimizing the DC-link capacitance in a brushless Synchronous Generator (SG) based aircraft DC power system. The proposed techniques involve an output power based feedforward compensation for the DC-link voltage regulation control and a feedforward steady-state duty cycle compensation for the exciter SG field current control. This control scheme helps to meet the tight MIL-STD-704F transient voltage requirements for 270V aircraft DC power system with minimum DC-link capacitance. The proposed controller is validated through simulation and Controller Hardware-in-Loop (C-HIL) experiments for a 50KVA three-stage brushless SG system model with 600 ¼F DC-link capacitance and results are provided at different speeds of the machine.","PeriodicalId":339989,"journal":{"name":"2021 IEEE Transportation Electrification Conference & Expo (ITEC)","volume":"12 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-06-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"An Improved Feedforward Controller for Minimizing the DC-link Capacitance in a Brushless Synchronous Generator based Aircraft DC Power System\",\"authors\":\"Goutham Selvaraj, K. Rajashekara, Krishna Raj Ramachandran Potti\",\"doi\":\"10.1109/ITEC51675.2021.9490190\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper proposes feedforward control improvements for minimizing the DC-link capacitance in a brushless Synchronous Generator (SG) based aircraft DC power system. The proposed techniques involve an output power based feedforward compensation for the DC-link voltage regulation control and a feedforward steady-state duty cycle compensation for the exciter SG field current control. This control scheme helps to meet the tight MIL-STD-704F transient voltage requirements for 270V aircraft DC power system with minimum DC-link capacitance. The proposed controller is validated through simulation and Controller Hardware-in-Loop (C-HIL) experiments for a 50KVA three-stage brushless SG system model with 600 ¼F DC-link capacitance and results are provided at different speeds of the machine.\",\"PeriodicalId\":339989,\"journal\":{\"name\":\"2021 IEEE Transportation Electrification Conference & Expo (ITEC)\",\"volume\":\"12 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-06-21\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2021 IEEE Transportation Electrification Conference & Expo (ITEC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ITEC51675.2021.9490190\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 IEEE Transportation Electrification Conference & Expo (ITEC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ITEC51675.2021.9490190","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
An Improved Feedforward Controller for Minimizing the DC-link Capacitance in a Brushless Synchronous Generator based Aircraft DC Power System
This paper proposes feedforward control improvements for minimizing the DC-link capacitance in a brushless Synchronous Generator (SG) based aircraft DC power system. The proposed techniques involve an output power based feedforward compensation for the DC-link voltage regulation control and a feedforward steady-state duty cycle compensation for the exciter SG field current control. This control scheme helps to meet the tight MIL-STD-704F transient voltage requirements for 270V aircraft DC power system with minimum DC-link capacitance. The proposed controller is validated through simulation and Controller Hardware-in-Loop (C-HIL) experiments for a 50KVA three-stage brushless SG system model with 600 ¼F DC-link capacitance and results are provided at different speeds of the machine.