Use of DGPS corrections with low power GPS receivers in a post SA environment

H. Gehue, Warren Hewerdine
{"title":"Use of DGPS corrections with low power GPS receivers in a post SA environment","authors":"H. Gehue, Warren Hewerdine","doi":"10.1109/AERO.2001.931360","DOIUrl":null,"url":null,"abstract":"With the removal of the dithering effects of Selective Availability (SA), use of Differential GPS (DGPS) corrections can now be applied for extended periods of time allowing enhanced performance for low power configurations of a Si RF based GPS receiver. The software selectable low power settings, implemented by Si RF, employ three states; track, navigate and trickle. During track and trickle states there is no UART communication making reception of DGPS correction unavailable. During the NAV state (when the navigation calculation is performed), corrections may be received. Previously, SA induced error shortened the viable extrapolation time to less than 30 seconds; else significant navigation error would build up between measurements. Additionally, the need to return to a full power state every 30 seconds significantly increased the overall average power dissipation over standard TricklePower/sup TM/ operation. Now that SA (the dominate error source of the DGPS correction) has been removed, the time limit that a DGPS correction can be applied has been extended from 30 seconds to several minutes without significant degradation in navigation performance. This opens up opportunity for low power GPS receiver operation to make use of the DGPS correction to improve navigation without severely impacting the average power requirements. Si RF's implementations of low power operation, leverages off its unique architecture that allows 100 ms signal reacquisition allowing a pseudorange measurement to as little 200 ms. The chipset is then shut down for 800 ms, significantly reducing the power consumption, while still maintaining 1 Hz navigation updates.","PeriodicalId":329225,"journal":{"name":"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)","volume":"36 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2001-03-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO.2001.931360","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

With the removal of the dithering effects of Selective Availability (SA), use of Differential GPS (DGPS) corrections can now be applied for extended periods of time allowing enhanced performance for low power configurations of a Si RF based GPS receiver. The software selectable low power settings, implemented by Si RF, employ three states; track, navigate and trickle. During track and trickle states there is no UART communication making reception of DGPS correction unavailable. During the NAV state (when the navigation calculation is performed), corrections may be received. Previously, SA induced error shortened the viable extrapolation time to less than 30 seconds; else significant navigation error would build up between measurements. Additionally, the need to return to a full power state every 30 seconds significantly increased the overall average power dissipation over standard TricklePower/sup TM/ operation. Now that SA (the dominate error source of the DGPS correction) has been removed, the time limit that a DGPS correction can be applied has been extended from 30 seconds to several minutes without significant degradation in navigation performance. This opens up opportunity for low power GPS receiver operation to make use of the DGPS correction to improve navigation without severely impacting the average power requirements. Si RF's implementations of low power operation, leverages off its unique architecture that allows 100 ms signal reacquisition allowing a pseudorange measurement to as little 200 ms. The chipset is then shut down for 800 ms, significantly reducing the power consumption, while still maintaining 1 Hz navigation updates.
在后SA环境中使用低功率GPS接收机进行DGPS校正
随着选择性可用性(SA)的抖动效应的消除,差分GPS (DGPS)校正的使用现在可以延长一段时间,从而增强基于Si射频的GPS接收机的低功耗配置的性能。软件可选低功耗设置,由Si RF实现,采用三种状态;跟踪,导航和涓涓细流。在跟踪和涓流状态下,没有UART通信使得接收DGPS校正不可用。在NAV状态(执行导航计算时),可能会收到更正。先前,SA诱导的误差将可行的外推时间缩短到30秒以内;否则,在两次测量之间就会产生重大的导航误差。此外,与标准的TricklePower/sup TM/操作相比,每30秒恢复到全功率状态的需要显着增加了总体平均功耗。现在,SA (DGPS校正的主要误差源)已经被删除,DGPS校正的时间限制已经从30秒延长到几分钟,而导航性能没有明显下降。这为低功耗GPS接收机操作提供了机会,利用DGPS校正来改善导航,而不会严重影响平均功率要求。Si RF实现低功耗操作,利用其独特的架构,允许100毫秒信号重采集,允许伪距测量到200毫秒。然后芯片组关闭800毫秒,显著降低功耗,同时仍然保持1 Hz的导航更新。
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 求助全文
来源期刊
自引率
0.00%
发文量
0
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信