{"title":"低成本姿态估计系统。空气轴承试验台的性能评价","authors":"F. von Bergen, J. Giribet, P. Martos","doi":"10.1109/SASE-CASE.2015.7295843","DOIUrl":null,"url":null,"abstract":"In this work, a low-cost attitude navigation system for spacecrafts is presented. The system fuses measurements from a three axis MEMS gyroscope and a CCD camera that identifies a known pattern of points (which emulate the stars). The system has been implemented on an ARM Cortex-A8 processor, running a GNU/Linux operating system. The developed attitude system was tested on an air-bearing testbed as experimental validation.","PeriodicalId":346043,"journal":{"name":"2015 Sixth Argentine Conference on Embedded Systems (CASE)","volume":"16 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2015-10-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Low cost attitude estimation system. Performance evaluation on an airbearing based testbed\",\"authors\":\"F. von Bergen, J. Giribet, P. Martos\",\"doi\":\"10.1109/SASE-CASE.2015.7295843\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this work, a low-cost attitude navigation system for spacecrafts is presented. The system fuses measurements from a three axis MEMS gyroscope and a CCD camera that identifies a known pattern of points (which emulate the stars). The system has been implemented on an ARM Cortex-A8 processor, running a GNU/Linux operating system. The developed attitude system was tested on an air-bearing testbed as experimental validation.\",\"PeriodicalId\":346043,\"journal\":{\"name\":\"2015 Sixth Argentine Conference on Embedded Systems (CASE)\",\"volume\":\"16 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2015-10-12\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2015 Sixth Argentine Conference on Embedded Systems (CASE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/SASE-CASE.2015.7295843\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2015 Sixth Argentine Conference on Embedded Systems (CASE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SASE-CASE.2015.7295843","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Low cost attitude estimation system. Performance evaluation on an airbearing based testbed
In this work, a low-cost attitude navigation system for spacecrafts is presented. The system fuses measurements from a three axis MEMS gyroscope and a CCD camera that identifies a known pattern of points (which emulate the stars). The system has been implemented on an ARM Cortex-A8 processor, running a GNU/Linux operating system. The developed attitude system was tested on an air-bearing testbed as experimental validation.