Limam Lakhdar, Boutte Aissa, Bentoutou Houari, Belaidi El Yazid
{"title":"纳米卫星低成本多电子负载样机的研制与测试","authors":"Limam Lakhdar, Boutte Aissa, Bentoutou Houari, Belaidi El Yazid","doi":"10.1109/ICAECCS56710.2023.10104914","DOIUrl":null,"url":null,"abstract":"Nanosatellites are becoming the new age of satellites for their small size, lightweight, fast and low-cost development within a small team. However, even with those advantages, it is still needed to use batteries as a secondary power source during eclipses. Those batteries require a good selection before being tested under a specific environment and integrated within the Nanosatellite. During the selection procedure or even during testing, batterie’s cells need to be discharged and charged several times requiring an electronic load, this one very expensive. In this paper, a low-cost electronic load prototype has been proposed based on the same technology for commercial electronic loads. The proposed electronic load is part of a Lithium-Ion battery test bench developed for aerospace applications, it has three different modes: Constant Current, Constant Power, and Constant Resistor. The final prototype will be duplicated in order to have several electronic loads, which will allow for the simultaneous testing of multiple battery cells, reducing the time and effort required.","PeriodicalId":447668,"journal":{"name":"2023 International Conference on Advances in Electronics, Control and Communication Systems (ICAECCS)","volume":"27 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-03-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Development and Testing of Low-Cost Multi-Electronic Load Prototype for Nanosatellites\",\"authors\":\"Limam Lakhdar, Boutte Aissa, Bentoutou Houari, Belaidi El Yazid\",\"doi\":\"10.1109/ICAECCS56710.2023.10104914\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Nanosatellites are becoming the new age of satellites for their small size, lightweight, fast and low-cost development within a small team. However, even with those advantages, it is still needed to use batteries as a secondary power source during eclipses. Those batteries require a good selection before being tested under a specific environment and integrated within the Nanosatellite. During the selection procedure or even during testing, batterie’s cells need to be discharged and charged several times requiring an electronic load, this one very expensive. In this paper, a low-cost electronic load prototype has been proposed based on the same technology for commercial electronic loads. The proposed electronic load is part of a Lithium-Ion battery test bench developed for aerospace applications, it has three different modes: Constant Current, Constant Power, and Constant Resistor. The final prototype will be duplicated in order to have several electronic loads, which will allow for the simultaneous testing of multiple battery cells, reducing the time and effort required.\",\"PeriodicalId\":447668,\"journal\":{\"name\":\"2023 International Conference on Advances in Electronics, Control and Communication Systems (ICAECCS)\",\"volume\":\"27 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-03-06\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2023 International Conference on Advances in Electronics, Control and Communication Systems (ICAECCS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICAECCS56710.2023.10104914\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 International Conference on Advances in Electronics, Control and Communication Systems (ICAECCS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICAECCS56710.2023.10104914","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Development and Testing of Low-Cost Multi-Electronic Load Prototype for Nanosatellites
Nanosatellites are becoming the new age of satellites for their small size, lightweight, fast and low-cost development within a small team. However, even with those advantages, it is still needed to use batteries as a secondary power source during eclipses. Those batteries require a good selection before being tested under a specific environment and integrated within the Nanosatellite. During the selection procedure or even during testing, batterie’s cells need to be discharged and charged several times requiring an electronic load, this one very expensive. In this paper, a low-cost electronic load prototype has been proposed based on the same technology for commercial electronic loads. The proposed electronic load is part of a Lithium-Ion battery test bench developed for aerospace applications, it has three different modes: Constant Current, Constant Power, and Constant Resistor. The final prototype will be duplicated in order to have several electronic loads, which will allow for the simultaneous testing of multiple battery cells, reducing the time and effort required.