High Update Rate Star Tracker for Gyroless Spacecraft Operation

Mikael Marin, H. Bang
{"title":"High Update Rate Star Tracker for Gyroless Spacecraft Operation","authors":"Mikael Marin, H. Bang","doi":"10.1109/METROAEROSPACE.2018.8453507","DOIUrl":null,"url":null,"abstract":"Traditional star trackers are designed for high accuracy but low update rate and rely on rate gyros to interpolate between measurements. However, the available rate gyros are either noisy, or expensive and heavy. The proposed work demonstrates the advantage of sacrificing some of the star tracker's accuracy for a higher update rate. As a result, aside from removing the need for a rate gyro, Attitude Determination and Control Systems overall performances are increased. The proposed star tracker achieved a 0.001 ° accurate Attitude Determination, with a 98.8% sky coverage at a 50Hz update rate. In addition, the image processing and star matching algorithm are designed to be efficiently implemented as a fully pipelined single-pass FPGA circuit.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"87 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/METROAEROSPACE.2018.8453507","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

Abstract

Traditional star trackers are designed for high accuracy but low update rate and rely on rate gyros to interpolate between measurements. However, the available rate gyros are either noisy, or expensive and heavy. The proposed work demonstrates the advantage of sacrificing some of the star tracker's accuracy for a higher update rate. As a result, aside from removing the need for a rate gyro, Attitude Determination and Control Systems overall performances are increased. The proposed star tracker achieved a 0.001 ° accurate Attitude Determination, with a 98.8% sky coverage at a 50Hz update rate. In addition, the image processing and star matching algorithm are designed to be efficiently implemented as a fully pipelined single-pass FPGA circuit.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
用于无陀螺航天器运行的高更新率星跟踪器
传统的星跟踪器精度高,但更新率低,并且依靠速率陀螺仪在测量之间进行插值。然而,现有的速率陀螺仪要么噪声大,要么价格昂贵且笨重。所提出的工作证明了牺牲一些星跟踪器的精度以获得更高的更新率的优势。因此,除了消除对速率陀螺仪的需求外,姿态确定和控制系统的整体性能也得到了提高。提出的星跟踪器实现了0.001°的精确姿态确定,在50Hz更新速率下具有98.8%的天空覆盖率。此外,图像处理和星型匹配算法被设计成一个全流水线的单通FPGA电路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Smart Air-Data Probe for Fault-Tolerant Flow Measurements Stereoscopic Vision-Based Relative Navigation for Spacecraft Proximity Operations Temperature Sensitivity of a Quartz Crystal Microbalance for TGA in Space Application of Piezoelectric Sensors for Structural Health Monitoring in Aerospace Characterization and Testing of a High-Resolution Time-of-Flight Camera for Autonomous Navigation
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1