IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences最新文献_第5页

Collision avoidance effectiveness: the past two decades 避碰效能:过去二十年

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66211

B. V. Tiblin

引用次数: 2

Interferometric fiber-optic gyroscopes: a summary of progress 干涉式光纤陀螺仪:进展综述

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66153

R. Liu, G. Adams

引用次数: 7

Real-time optimum calibration of large sensor systems by Kalman filtering 基于卡尔曼滤波的大型传感器系统实时优化标定

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66170

A. Lange

引用次数: 4

Terrain aided navigation using maximum a posteriori estimation 使用最大后验估计的地形辅助导航

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66215

N. Johnson, W. Tang, G. Howell

引用次数: 12

The missing (data) link in pilot navigation 飞行员导航中缺失的(数据)链接

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66238

M. Ritchie

引用次数: 1

Experiments for an integrated precise airborne navigation and gravity recovery system 精确机载导航与重力回收一体化系统试验

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66189

G. Hein, K. Hehl, H. Landau, M. Ertel

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引用次数: 7

An advanced driver information system concept and its communications considerations 一种先进的驾驶员信息系统概念及其通信考虑

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66201

W. G. Toperzer

引用次数: 0

The effect of the microwave landing system on airport capacity 微波着陆系统对机场容量的影响

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66241

D. Berninger

引用次数: 1

Common integrated processing in modular avionics 模块化航空电子设备中的通用集成处理

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66167

T. H. Robinson, E. Trujillo

引用次数: 0

Evaluation of GPS receiver ranging accuracy GPS接收机测距精度评估

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66194

M. May, E. Kreisher, T. Nasuti, C. Sives

{"title":"Evaluation of GPS receiver ranging accuracy","authors":"M. May, E. Kreisher, T. Nasuti, C. Sives","doi":"10.1109/PLANS.1990.66194","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66194","url":null,"abstract":"The GPS (Global Positioning System) Central Engineering Activity (CEA) of the Naval Air Development Center has developed facilities to support multiservice testing of Rockwell Collins GPS user equipment (UE). A capability has been developed within the CEA to evaluate the accuracy with which the GPS UE makes pseudorange measurement. CEA users are able to isolate and to examine receiver code tracking loop performance independently of GPS navigation performance. Pseudorange measurements consist of the true line-of-sight range and a number of error sources which include: tracking errors, satellite clock error, atmospheric delays, receiver clock error, and receiver channel delays. A range accuracy assessment process has been developed to isolate the tracking error from the other sources of error and the true line-of-sight range. Since the CEA provides a controllable test environment, some of the error sources can be zeroed (satellite clock error and ionospheric and tropospheric delay effects) while others can be quantified (receiver clock error and channel delays). The true line-of-sight range can be determined from the CEA trajectory generation function. The result is that the CEA provides for the direct determination of tracking error in UE receiver pseudorange values.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"2016 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125726940","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 4