{"title":"一种适用于实验火箭模型的飞行数据采集系统的设计与构建","authors":"Alejandro Urrego","doi":"10.18180/tecciencia.2019.27.8","DOIUrl":null,"url":null,"abstract":". This document describes the different stages of development need to design, build and characterize a flight data acquisition system for the experimental rocket USB - Rocket I. To do so, some simulated flight con-ditions collected from a computer program, and the manufacturing and as-sembly process of an integrated electronic circuit are presented. As a result, the flight data collected in a horizontal ground displacement and commer-cial flight test are presented with this device.","PeriodicalId":22331,"journal":{"name":"TECCIENCIA","volume":null,"pages":null},"PeriodicalIF":0.7000,"publicationDate":"2020-02-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Design and Construction of a Flight Data Acquisition System Adapted to an Experimental Rocket Model\",\"authors\":\"Alejandro Urrego\",\"doi\":\"10.18180/tecciencia.2019.27.8\",\"DOIUrl\":null,\"url\":null,\"abstract\":\". This document describes the different stages of development need to design, build and characterize a flight data acquisition system for the experimental rocket USB - Rocket I. To do so, some simulated flight con-ditions collected from a computer program, and the manufacturing and as-sembly process of an integrated electronic circuit are presented. As a result, the flight data collected in a horizontal ground displacement and commer-cial flight test are presented with this device.\",\"PeriodicalId\":22331,\"journal\":{\"name\":\"TECCIENCIA\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.7000,\"publicationDate\":\"2020-02-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"TECCIENCIA\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.18180/tecciencia.2019.27.8\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"ENGINEERING, MULTIDISCIPLINARY\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"TECCIENCIA","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.18180/tecciencia.2019.27.8","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ENGINEERING, MULTIDISCIPLINARY","Score":null,"Total":0}
Design and Construction of a Flight Data Acquisition System Adapted to an Experimental Rocket Model
. This document describes the different stages of development need to design, build and characterize a flight data acquisition system for the experimental rocket USB - Rocket I. To do so, some simulated flight con-ditions collected from a computer program, and the manufacturing and as-sembly process of an integrated electronic circuit are presented. As a result, the flight data collected in a horizontal ground displacement and commer-cial flight test are presented with this device.
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