Dynamic Performance Evaluation of Various GNSS Receivers and Positioning Modes with Only One Flight Test
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Comparing Four Methods of Correcting GPS Data: DGPS, WAAS, L-Band, and Postprocessing Dick Karsky, Project Leader
United States Department of Agriculture Engineering Forest Service Technology & Development Program July 2004 0471-2307–MTDC 2200/2300/2400/3400/5100/5300/5400/ 6700/7100 Comparing Four Methods of Correcting GPS Data: DGPS, WAAS, L-Band, and Postprocessing Dick Karsky, Project Leader he global positioning system (GPS) of satellites DGPS Beacon Corrections allows persons with standard GPS receivers to know where they are with an accuracy of 5 meters The U.S. Coast Guard has installed two control centers Tor so. When more precise locations are needed, and more than 60 beacon stations along the coastal errors (table 1) in GPS data must be corrected. A waterways and in the interior United States to transmit number of ways of correcting GPS data have been DGPS correction data that can improve GPS accuracy. developed. Some can correct the data in realtime The beacon stations use marine radio beacon fre- (differential GPS and the wide area augmentation quencies to transmit correction data to the remote GPS system). Others apply the corrections after the GPS receiver. The correction data typically provides 1- to data has been collected (postprocessing). 5-meter accuracy in real time. In theory, all methods of correction should yield similar In principle, this process is quite simple. A GPS receiver results. However, because of the location of different normally calculates its position by measuring the time it reference stations, and the equipment used at those takes for a signal from a satellite to reach its position. stations, the different methods do produce different Because the GPS receiver knows exactly where results. -
Location Corrections Through Differential Networks (LOCD-IN)
Location Corrections through Differential Networks (LOCD-IN) A thesis presented to the faculty of the Russ College of Engineering and Technology of Ohio University In partial fulfillment of the requirements for the degree Master of Science Russell V. Gilabert December 2018 © 2018 Russell V. Gilabert. All Rights Reserved. 2 This thesis titled Location Corrections through Differential Networks (LOCD-IN) by RUSSELL V. GILABERT has been approved for the School of Electrical Engineering and Computer Science and the Russ College of Engineering and Technology by Maarten Uijt de Haag Edmund K. Cheng Professor of Electrical Engineering and Computer Science Dennis Irwin Dean, Russ College of Engineering and Technology 3 ABSTRACT GILABERT, RUSSELL V., M.S., December 2018, Electrical Engineering Location Corrections through Differential Networks (LOCD-IN) Director of Thesis: Maarten Uijt de Haag Many mobile devices (phones, tablets, smartwatches, etc.) have incorporated embedded GNSS receivers into their designs allowing for wide-spread on-demand positioning. These receivers are typically less capable than dedicated receivers and can have an error of 8-20m. However, future application, such as UAS package delivery, will require higher accuracy positioning. Recently, the raw GPS measurements from these receivers have been made accessible to developers on select mobile devices. This allows GPS augmentation techniques usually reserved for expensive precision-grade receivers to be applied to these low cost embedded receivers. This thesis will explore the effects of various GPS augmentation techniques on these receivers. 4 ACKNOWLEDGMENTS I would like to thank my academic advisor, Maarten Uijt de Haag, for providing guidance and opportunities in both my academic and professional careers. -
(GNSS) Based Augmentation System Low Latitude Threat Model
Effects Of Southern Hemisphere Ionospheric Activity On Global Navigation Satellite Systems (GNSS) Based Augmentation System Low Latitude Threat Model December 2014 Submitted to: Servicos de Defesa e Technologia de Processos (SDTP) And The U.S. Trade and Development Agency 1000 Wilson Boulevard, Suite 1600, Arlington, VA 22209-3901 Submitted by Mirus Technology LLC Prepared by the Mirus Technology, LLC (with Contributions from FAA, Stanford University, INPE, ICEA, Boston College, NAVTEC, and KAIST) Principal Investigator: Dr. Navin Mathur Executive Summary Ground-based Augmentation System (GBAS) augments the Global Positioning System (GPS) by increasing the accuracy to an appropriately equipped user. In addition to enhancing the accuracy of GPS derived accuracy, a GBAS provides the necessary integrity of accuracy (to a level defined by International Civil Aviation Organization, ICAO) required for a system that supports landing of an aircraft at an airport where GBAS is available. In addition, a GBAS system is designed to ensure the process of integrity and required continuity of GBAS operations and associated operational availability. The integrity of GBAS is threatened by several internal or external factors that can be broadly classified into three categories namely; Space Vehicle (SV) induced errors, environmental induced errors, and internally generated errors. Over the last decade, the US Federal Aviation Administration (FAA) has systematically defined, classified, characterized, and addressed each of the error sources in those categories that apply within CONUS. These efforts culminated in approval of several GBAS Category-I approaches within CONUS at various locations (such as Newark, Houston, etc.). Through the process of GBAS development for CONUS, the aviation and scientific communities realized that the Ionosphere is one of the key contributors to GBAS integrity threat. -
(Gnss) in View of Progress Made in Gagan
INDIA LIABILITY IN CONTEXT TO THE AIR NAVIGATION SERVICE PROVIDER + By Ranjana Kaul* The Global Navigation Satellite System1 is poised to be one of the most critical technologies in the twenty-first century. Like most other technologies, GNSS was first developed for military application, and arguably, like other dual use technologies, it is a double edged sword. The 1990 Gulf War demonstrated how GNSS can be successfully deployed as a military force multiplier. Equally civilian applications of GNSS have brought lucrative returns2 and incremental developmental benefits to countries around the world3. In specific context to @ copyright Ranjana Kaul + This paper is the expanded version of Ranjana Kaul ‟s presentation on ”INDIA: LIABILITY IN CONTEXT TO THE AIR NAVIGATION SERVICE PROVIDER‟ made at the International Conference on Contemporary Issues in Air Transport, Air Law & Regulation, New Delhi, India, 23-25 April 2008. * B.A.( Bombay University); MA; PhD. (University of Poona) LLB ( University of Delhi); LL.M (Institute of Air & Space Law, Faculty of Law, Mc Gill University, Montreal, Canada); Partner, Dua Associates, (Advocates & Solicitors) , New Delhi, India. 1 Global Navigation Satellite System (GNSS) is the standard generic term for satellite navigation systems that provide autonomous geo-spatial positioning with global coverage. A GNSS allows small electronic receivers to determine their location (longitude, latitude, and altitude) to within a few metres using time signals transmitted along a line of sight by radio from satellites. Receivers on the ground with a fixed position can also be used to calculate the precise time as a reference for scientific experiments. As of 2007, the United States NAVSTAR Global Positioning System (GPS) is the only fully operational GNSS. -
And Dual-Frequency GPS and GLONASS Observations on Point Accuracy Under Forest Canopies
Effects of Differential Single- and Dual-Frequency GPS and GLONASS Observations on Point Accuracy under Forest Canopies Erlk Naesset Deckert and Bolstad (1996) and Sigrist et al. (1999) reported A 20-channel, dual-frequency receiver observing dual-fie- accuracies of approximately 3.1 to 4.4 m and 1.8 to 2.5 m for the quency pseudorange and carrier phase of both GPS and average position of 500 and 480 repeated measurements of indi- GLONASS was used to determine the positional accuracy of 29 vidual points under tree canopies, respectively, based on differ- points under tree canopies. The mean positional accuracy ential pseudorange. Nsesset (1999)found that, even under tree based on differential postprocessing of GPS+GLONASS single- canopies, carrier phase observations represent valuable addi- frequency observations ranged from 0.16 m to 1.I 6 m for 2.5 tional information as compared to traditional pseudorange min to 20 min of observation at points with basal area ranging acquisition. By using both single-frequency pseudorange and from <20 m2/ha to 230 m2/ha. The mean positional accuracy carrier phase observations in an adjustment with coordinates of differential postprocessing of dual-frequency GPS+GLONASS and carrier phase ambiguities as unknown parameters (float observations ranged from 0.08 m to 1.35 m. Using the dual- solution), an accuracy of 0.8 m was reported for two 12-chan- frequency carrier phase as main observable and fixing the nel receivers based on 30 min of observation. The correspond- initial integer phase ambiguities, i.e., a fixed solution, gave ing accuracy using pseudorange only was 1.2 to 1.9 m. -
ABAS), Satellite-Based Augmentation System (SBAS), Or Ground-Based Augmentation System (GBAS
Current Status and Future Navigation Requirements for Mexico City New Airport New Mexico City Airport in figures: • 120 million passengers per year; • 1.2 million tons of shipping cargo per year; • 4,430 Ha. (6 times bigger tan the current airport); • 6 runways operating simultaneously; • 1st airport outside Europe with a neutral carbon footprint; • Largest airport in Latin America; • 11.3 billion USD investment (aprox.); • Operational in 2020 (expected). “State-of-the-art navigation systems are as important –or more- than having world class civil engineering and a stunning arquitecture” Air Navigation Systems: A. In-land deployed systems - Are the most common, based on ground stations emitting radiofrequency signals received by on-board equipments to calculate flight position. B. Satellite navigation systems – First stablished by U.S. in 1959 called TRANSIT (by the time Russia developed TSIKADA); in 1967 was open to civil navigation; 1973 GPS was developed by U.S., then GLONASS, then GALILEO. C. Inertial navigation systems – Autonomous navigation systems based on inertial forces, providing constant information on the position of the flight and parameters of speed and direction (e.g. when flying above the ocean and there are no ground segments to provide support). Requirements for performance of Navigation Systems: According to the International Civil Aviation Organization (ICAO) there are four main requirements: • The accuracy means the level of concordance between the estimated position of an aircraft and its real position. • The availability is the portion of time during which the system complies with the performance requirements under certain conditions. • The integrity is the function of a system that warns the users in an opportune way when the system should not be used. -
Multi-GNSS Working Group Technical Report 2018
Multi-GNSS Working Group Technical Report 2018 P. Steigenberger1, O. Montenbruck1 1 Deutsches Zentrum für Luft- und Raumfahrt (DLR) German Space Operations Center (GSOC) Münchener Straße 20 82234 Weßling, Germany E-mail: [email protected] 1 Introduction The Multi-GNSS Working Group (MGWG) is coordinating the activities of the Multi- GNSS Pilot Project (MGEX). MGEX is providing multi-GNSS products focusing on the global systems Galileo and BeiDou as well as the regional QZSS and IRNSS (NavIC). A few changes of membership of the MGWG occurred during the reporting period: Lars Prange succeeded Rolf Dach as representative of CODE • Shuli Song joined the MGWG representing SHAO • Sebastian Strasser of TU Graz joined the working group • Ahmed ElMowafy, Heinz Habrich, and Rene Warnant left the working group • 2 GNSS Evolution The numerous 2018 satellite launches of the four global systems GPS, GLONASS, Galileo, and BeiDou as well as the regional IRNSS are listed in Table1. Altogether 16 BeiDou-3 medium Earth orbit (MEO) satellites and one BeiDou-3 geostationary Earth orbit (GEO) satellite have been launched. The Interface Control Document (ICD) for the BeiDou open service signal B3I transmitted by BeiDou-2 and BeiDou-3 satellites has been published in February 2018 (CSNO, 2018). Based on a constellation of 18 BeiDou-3 MEO satellites, global services were declared on 27 December 2018. The Galileo quadruple launch in July 2018 completed the nominal Galileo constella- tion paving the road for full operational capability with now 26 satellites in orbit. Two 191 Multi–GNSS Working Group Table 1: GNSS satellite launches in 2018. -
Differential Global Positioning System Navigation Using High-Frequency Ground Wave Transmissions
J. R. VETTER AND W. A. SELLERS TEST AND EVALUATION Differential Global Positioning System Navigation Using High-Frequency Ground Wave Transmissions Jerome R. Vetter and William A. Sellers Since 1992, the Strategic Systems Department of the Applied Physics Laboratory has been investigating the use of high-frequency (HF) ground wave transmissions in the upper HF band for sea-based communications. This effort has examined the optimization of shipboard antennas for two-way communications with ground stations. This article describes early tests using differential Global Positioning System navi- gation for investigating the accuracy of determining a ship’s position from a base station using HF ground wave transmissions. (Keywords: Differential GPS, HF signal transmissions, Kalman filtering, Navigation.) INTRODUCTION In late 1990, the U.S. Coast Guard undertook a reference and remote stations into the system was comprehensive data link study to determine which RF costly. Although the system could provide broadcasts broadcast systems could be used to support differential beyond LOS, it was affected by poor performance due Global Positioning System (DGPS) correction trans- to propagation variations in spite of a predicted 700- missions over the continental United States (CO- km sky wave mode range. NUS) and to determine which radio systems were The purpose of APL’s early high-frequency ground appropriate for a given operating area. The broadcast wave (HFGW) experiments at sea was to improve constraints for the system design had to meet accura- two-way voice and data communications between cies of ±3 m at data rates of 100 bits/s with data submerged submarines and surface ships; previous latencies of less than 4 s. -
Labsat Flyer
GNSS Simulator RECORDS Real world GNSS signals REPLAYS GPS, Galileo, GLONASS, BeiDou, SBAS & QZSS RF data SIMULATES User defined scenarios anywhere The most affordable, portable, and versatile multi-constellation Global Navigation Satellite Simulator on the market. If you are selling, testing or developing products How does it work? incorporating satellite navigation chipsets, then you’ll receives the signal from a standard satellite find makes your job easier, quicker and antenna, but instead of processing each of the received more cost effective. signals to calculate a position fix, digitises and stores the original satellite signals at a very high Why use a Simulator? bandwidth onto a removable SD card or USB disk. records and replays real world data, allowing realistic and repeatable testing to be carried out under The RF output of the is then connected to controlled conditions. Signal artefacts including the antenna input of the device under test and the multipath, ionospheric effects and signal dropouts are recorded data is replayed back as an RF signal. The reproduced and there are no limits to the number of device under test will then start to track the satellites as satellites used in the test. though it was travelling along the same path taken by the during the original recording. Conventional testing usually requires driving the same route multiple times, where conditions vary and satellite How easy is it to use? constellations change between tests. This can make it One touch record/replay makes extremely very challenging to reproduce and fault find software simple to operate. With its rugged construction, built in errors or reception issues with the device under test. -
Starfire™ GNSS: the Next Generation Starfire Global Satellite Based Augmentation System
StarFire™ GNSS: The Next Generation StarFire Global Satellite Based Augmentation System Chaochao Wang and Ronald Hatch NavCom Technology, Inc. ABSTRACT StarFire receiver hardware and software. NavCom Technology has made numerous advancements in NavCom’s next generation StarFire GNSS system Satellite Based Augmentation Systems (SBAS) over performance is described in this paper. The StarFire the past 15 years and has continued to improve GNSS system is a Global Satellite Based receiver performance to a customer base that now Augmentation System (GSBAS) developed entirely consists of multiple thousands of users. The first by NavCom Technology. Significant improvements StarFire Wide Area Differential GPS correction have been made to each component of the system service, originally named Wide Area Correction including the ground reference network, new Transform (WCT), was introduced by NavCom in proprietary real-time orbit and clock generation, dual 1998. Like the current system it used dual- redundant delivery of corrections via commercial frequency GPS measurements for navigation and communication satellites, and the GNSS receiver precise point positioning. This continental WADGPS navigation software. Among the most significant StarFire system delivered better than 30cm position improvements is the incorporation of orbit and clock accuracy for users in North America. corrections for GLONASS satellites. At the same time, the orbital and clock correction accuracy for In 2002, NavCom introduced a truly global StarFire GPS satellites has been dramatically improved and GPS augmentation service. Using a global reference the receiver navigation software has been modified receiver network and an enhanced version of the to take advantage of both the GLONASS satellites Real-Time GIPSY (RTG) clock and orbital correction and the improved orbit and clock accuracy for GPS. -
Of 6 UNAVCO Geodetic Data Services Plan for GNSS Modernization
UNAVCO Geodetic Data Services Plan for GNSS Modernization: Data Formats and Preprocessing Tools March 2016 Modernization of GNSS New GPS signals (L2C, L5) and additional GNSS constellations (Galileo, GLONASS, Beidou/Compass, QZSS, SBAS, IRNSS) are changing the landscape For UNAVCO’s data handling moving into the future. The transition to utilizing GNSS within the global geodesy community and the UNAVCO community is in its very early stages. However, the need to move ahead has been recognized: The PBO Futures workshop Final report includes recommendations that UNAVCO: “Move to GNSS by 2018 to maintain relevancy oF network.” and “Upgrade a limited number oF GPS stations to Full GNSS in strategic target areas oF high scientific value, those that support large user communities, and For collection oF data For UNAVCO and community-driven development and testing eFForts.” UNAVCO’s Geodetic Data Services (GDS) division must prepare to manage, archive, and deliver this data. In addition, a model For Future support for GNSS data preprocessing tools used by UNAVCO Archive operations and provided to the global community needs to be Formulated. The challenges that face GDS in this transition, and our proposed response are the subject oF this white paper. Current and Emerging Formats RINEX 2.11 The current standard Format recognized and disseminated by the International GNSS Service (IGS) is RINEX version 2.11. UNAVCO archives several hundred gigabytes oF GPS level 0/1 standard rate (15 s or 30 s sample interval) data per month and delivers approximately Five times that to data processors via anonymous ftp. Data are archived in a variety of receiver-speciFic raw Formats, plus BINEX, RINEX 1, and RINEX 2. -
Augmented GNSS: Fundamentals and Keys to Integrity and Continuity
ION GNSS 2011 TUTORIAL Augmented GNSS: Fundamentals and Keys to Integrity and Continuity Sam Pullen Department of Aeronautics and Astronautics Stanford University, Stanford, CA. 94305-4035 USA Tuesday, Sept. 20, 2011 1:30 – 5:00 PM Oregon Convention Center, Portland, Oregon (last updated 9/16/11) Acknowledgements: B. Belabbas, J. Blanch, R. Braff, M. Brenner, J. Burns, B. Clark, K. Class, S. Datta-Barua, P. Enge, M. Harris, R. Kelly, R. Key, J. Lee, M. Luo, A. Mitelman, T. Murphy, Y.S. Park, B. Parkinson, B. Pervan, R.E. Phelts, J. Rife, C. Rodriguez, J. Scheitlin, C. Shively, K. Suzuki, R. Swider, F. van Graas, T. Walter, J. Warburton, G. Xie, G. Zhang, and more… ©2011 by Sam Pullen Outline • Augmented GNSS Terminology • Introduction to GNSS and GNSS Augmentation – Differential GNSS (DGNSS) • GBAS and SBAS System Architectures • Aviation Applications and Requirements • Principles of Integrity and Continuity • Specific Examples: – Nominal Error Bounding – Signal Deformation Monitoring – Ephemeris Monitoring – Ionospheric Anomaly Mitigation • Summary 20 September 2011 Augmented GNSS: Integrity and Continuity 2 Augmented GNSS Terminology • GPS: Global Positioning System • GNSS: Global Navigation Satellite Systems • DGPS: Differential GPS (or GNSS) • L(A)DGPS: Local-Area Differential GPS • WADGPS: Wide-Area Differential GPS • CDGPS: Carrier-Phase Differential GPS (usually a subset of Local-Area DGPS) • LAAS: Local Area Augmentation System (FAA) • GBAS: Ground-Based Augmentation System (international; includes LAAS) • WAAS: Wide Area Augmentation