Mario Castro Santiago, Luis Sánchez Velasco, A. Aranda
{"title":"用于姿态控制的低成本磁模拟器","authors":"Mario Castro Santiago, Luis Sánchez Velasco, A. Aranda","doi":"10.1109/TAEE.2018.8476113","DOIUrl":null,"url":null,"abstract":"The aim of this paper is to propose an aerospace project, in order to allow Master’s Space students to put in practice their knowledge in physics, which can be crucial in this engineering area. Here, we face the attitude control issue of a cubesat, using a physical 1U satellite model and a magnetic field simulator, combined with real data from a desired orbit. The satellite model will use magnetorquers controlled by an Arduino board, in the same way as the magnetic simulator.","PeriodicalId":304068,"journal":{"name":"2018 XIII Technologies Applied to Electronics Teaching Conference (TAEE)","volume":"30 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Low cost magnetic simulator for attitude control\",\"authors\":\"Mario Castro Santiago, Luis Sánchez Velasco, A. Aranda\",\"doi\":\"10.1109/TAEE.2018.8476113\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The aim of this paper is to propose an aerospace project, in order to allow Master’s Space students to put in practice their knowledge in physics, which can be crucial in this engineering area. Here, we face the attitude control issue of a cubesat, using a physical 1U satellite model and a magnetic field simulator, combined with real data from a desired orbit. The satellite model will use magnetorquers controlled by an Arduino board, in the same way as the magnetic simulator.\",\"PeriodicalId\":304068,\"journal\":{\"name\":\"2018 XIII Technologies Applied to Electronics Teaching Conference (TAEE)\",\"volume\":\"30 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 XIII Technologies Applied to Electronics Teaching Conference (TAEE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/TAEE.2018.8476113\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 XIII Technologies Applied to Electronics Teaching Conference (TAEE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/TAEE.2018.8476113","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The aim of this paper is to propose an aerospace project, in order to allow Master’s Space students to put in practice their knowledge in physics, which can be crucial in this engineering area. Here, we face the attitude control issue of a cubesat, using a physical 1U satellite model and a magnetic field simulator, combined with real data from a desired orbit. The satellite model will use magnetorquers controlled by an Arduino board, in the same way as the magnetic simulator.
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