GPS Versus Galileo
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GLONASS System As a Tool for Space Weather Monitoring
GLONASS System as a tool for space weather monitoring V.V. Alpatov, S.N. Karutin, А.Yu. Repin Institute of Applied Geophysics, Roshydromet TSNIIMASH, Roscosmos BAKU-2018 PLAN OF PRESENTATION General information about GLONASS Goals Organization and Management Technical information about GLONASS Space Weather Effects On Space Systems On Ground based Systems Possible Opportunities of GLONASS for Monitoring Space Weather Effects Russian Monitoring System for Monitoring Space Weather Effects with Use Opportunities of GLONASS 2 GENERAL INFORMATION ABOUT GLONASS NATIONAL SATELLITE NAVIGATION POLICY AND ORGANIZATION Presidential Decree of May 17, 2007 No. 638 On Use of GLONASS (Global Navigation Satellite System) for the Benefit of Social and Economic Development of the Russian Federation Federal Program on GLONASS Sustainment, Development and Use for 2012-2020 – planning and budgeting instrument for GLONASS development and use Budget planning for the forthcoming decade – up to 2030 GLONASS Program governance: Roscosmos State Space Corporation Government Contracting Authority – Program Coordinator Government Contracting Authorities Program Scientific and Coordination Board GLONASS Program Goals: Improving GLONASS performance – its accuracy and integrity Ensuring positioning, navigation and timing solutions in restricted visibility of satellites, interference and jamming conditions Enhancing current application efficiency and broadening application domains 3 CHARACTERISTICS IMPROVEMENT PLAN Accuracy Improvement by means of: . Ground Segment -
GPS and GLONASS Vector Tracking for Navigation in Challenging Signal Environments
GPS and GLONASS Vector Tracking for Navigation in Challenging Signal Environments Tanner Watts, Scott Martin, and David Bevly GPS and Vehicle Dynamics Lab – Auburn University October 29, 2019 2 GPS Applications (GAVLAB) Truck Platooning Good GPS Signal Environment Autonomous Vehicles Precise Timing UAVs 3 Challenging Signal Environments • Navigation demand increasing in the following areas: • Cites/Urban Areas • Forests/Dense Canopies • Blockages (signal attenuation) • Reflections (multipath) 4 Contested Signal Environments • Signal environment may experience interference • Jamming . Transmits “noise” signals to receiver . Effectively blocks out GPS • Spoofing . Transmits fake GPS signals to receiver . Tricks or may control the receiver 5 Contested Signal Environments • These interference devices are becoming more accessible GPS Jammers GPS Simulators 6 Traditional GPS Receiver Signals processed individually: • Known as Scalar Tracking • Delay Lock Loop (DLL) for Code • Phase Lock Loop (PLL) for Carrier 7 Traditional GPS Receiver • Feedback loops fail in the presence of significant noise • Especially at high dynamics Attenuated or Distorted Satellite Signal 8 Vector Tracking Receiver • Process signals together through the navigation solution • Channels track each other’s signals together • 2-6 dB improvement • Requires scalar tracking initially 9 Vector Tracking Receiver Vector Delay Lock Loop (VDLL) • Code tracking coupled to position navigation • DLL discriminators inputted into estimator • Code frequencies commanded by predicted pseudoranges -
GNSS Applications Workshop: Seminar on GNSS Spectrum Protection and Interference Detection and Mitigation
GNSS Applications Workshop: Seminar on GNSS Spectrum Protection and Interference Detection and Mitigation Course Introduction 20-21 March 2018 Satellite Navigation in the 1950s 1950 1951 1952 1953 1954 1955 1956 1957 1958 1959 4 Oct 1957 Dec 1958 Sputnik I The U.S. Launched Navy Navigation Satellite System (Transit) Approved and Funded 2 Satellite Navigation in the 1960s 1960 1961 1962 1963 1964 1965 1966 1967 1968 1969 13 April 1960 First Successful 5 Dec 1963 Jan 1964 Other Successful July 1967 Transit First Transit Experimental Transit Experimental Operational Became Satellites: Released Satellite (1B) Satellite Operational 2A, 22 Jun 1960 for 3B, 21 Feb 1961 Commercial 4A, 29 Jun 1961 Use 4B, 15 Nov 1961 - - - - Establishing U.S. Dual Use SatNav Policy Operational Transit Satellite 3 Satellite Navigation in the 1970s 1970 1971 1972 1973 1974 1975 1976 1977 1978 1979 1978 GPS Launches April 1973 22 Feb, 13 May, Formation of the GPS 7 Oct, 11 Dec Joint Program Office (JPO) 1971 First Timation Receiver 1975 for the Naval Research First Concept Validation GPS Lab (NRL) Navigator, the GPS X-Set 4 Satellite Navigation in the 1980s 1980 1981 1982 1983 1984 1985 1986 1987 1988 1989 9 Oct ‘85 28 Jan ‘86 14 Feb ‘89 Last Block I Challenger Launches Launch Disaster Resume 1984 Commercial 5 Channel GPS Navigator 1986 6 Channel GPS Navigator 1985 1986 GPS + Transit + Omega WM101 GPS Satellite Surveying Set 5 Satellite Navigation in the 1990s 1990 1991 1992 1993 1994 1995 1996 1997 1998 1999 4 Apr ‘91 8 Dec ‘93 27 Apr ‘95 S/A Turned GPS IOC GPS -
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. -
Robotic Forest Harvesting Process Using GNSS
RNI: DELENG/2005/15153 No: DL(E)-01/5079/17-19 Publication: 15th of every month Licensed to post without pre-payment U(E) 28/2017-19 Posting: 19th/20th of every month at NDPSO Rs.150 ISSN 0973-2136 Volume XV, Issue 5, May 2019 THE MONTHLY MAGAZINE ON POSITIONING, NAVIGATION AND BEYOND Robotic forest harvesting process using GNSS Soil moisture retrieval using NavIC-GPS-SBAS receiver Rethinking asset management. At 172 megapixels per full-spherical image, the UltraCam Panther Reality Capture System lets you capture your production plant in more detail, with superior sharpness and in higher fidelity than ever before. ULTRACAM PANTHER KEY FEATURES Indoor and outdoor Multitude of use Easy to deploy, mapping even cases through operate and without GPS modular design maintain Discover more on www.vexcel-imaging.com i50 GNSS RTK Brings speed and accuracy in Rethinking one easy-to-use GNSS solution asset management. At 172 megapixels per full-spherical image, the UltraCam Panther Reality Capture System lets you capture your production plant in more detail, with superior sharpness and in higher fidelity than ever before. ULTRACAM PANTHER KEY FEATURES Full GNSS technology Extended connectivity GPS+Glonass+Beidou+Galileo Internal UHF and 4G modems for robust data quality for optimized field operations Indoor and outdoor Multitude of use Easy to deploy, mapping even cases through operate and Preset work modes Rugged and compact without GPS modular design maintain Select configurations in a few Industrial design to withstand seconds for higher productivity -
Tianwen-1: China's Mars Mission
Tianwen-1: China's Mars Mission drishtiias.com/printpdf/tianwen-1-china-s-mars-mission Why In News China will launch its first Mars Mission - Tianwen-1- in July, 2020. China's previous ‘Yinghuo-1’ Mars mission, which was supported by a Russian spacecraft, had failed after it did not leave the earth's orbit and disintegrated over the Pacific Ocean in 2012. The National Aeronautics and Space Administration (NASA) is also going to launch its own Mars mission in July, the Perseverance which aims to collect Martian samples. Key Points The Tianwen-1 Mission: It will lift off on a Long March 5 rocket, from the Wenchang launch centre. It will carry 13 payloads (seven orbiters and six rovers) that will explore the planet. It is an all-in-one orbiter, lander and rover system. Orbiter: It is a spacecraft designed to orbit a celestial body (astronomical body) without landing on its surface. Lander: It is a strong, lightweight spacecraft structure, consisting of a base and three sides "petals" in the shape of a tetrahedron (pyramid- shaped). It is a protective "shell" that houses the rover and protects it, along with the airbags, from the forces of impact. Rover: It is a planetary surface exploration device designed to move across the solid surface on a planet or other planetary mass celestial bodies. 1/3 Objectives: The mission will be the first to place a ground-penetrating radar on the Martian surface, which will be able to study local geology, as well as rock, ice, and dirt distribution. It will search the martian surface for water, investigate soil characteristics, and study the atmosphere. -
INPE) MCTI Çp ' Acordo Operação Técnica COPERNICUS Entre ESA,AEB E INPE (0026237) SEI 01350.001611/2018-03 / Pg
ORIGINAL N° 1 Copernicus Space Component Technical Operating Arrangement ESA - Brazilian Space Agency and INPE (INPE) MCTI çp ' Acordo Operação Técnica COPERNICUS entre ESA,AEB E INPE (0026237) SEI 01350.001611/2018-03 / pg. 1 Table of Contents 1 INTRODUCTION....................................................................................... 4 1.1 Background....................................................................................................................... 4 1.2 Purpose and objectives ..................................................................................................... 4 1.3 Scope................................................................................................................................. 6 1.4 References......................................................................................................................... 6 2 EUROPEAN ACCESS TO BRAZILIAN EO MISSIONS AND CALIBRATION DATA AND PARTNER IN-SITU DATA ............................................................. 7 3 ARRANGEMENT OF TECHNICAL INTERFACES ....................................... 8 3.1 Technical Arrangement Types.......................................................................................... 8 4 INTERNATIONALARCHIVING AND DISSEMINATION CENTRES, MIRRORSITE ................................................................................................ 9 4.1 Invohred Entities............................................................................................................... 9 4.2 INPE Activity -
Gnss and Avionics Simulation for Rohde & Schwarz Signal Generators
GNSS AND AVIONICS SIMULATION FOR ROHDE & SCHWARZ SIGNAL GENERATORS Specifications R&S®SMBV100B Vector Signal Generator R&S®SMW200A Vector Signal Generator Data Sheet Version 11.00 Version 11.00, February 2021 CONTENTS Definitions ....................................................................................................................................................................... 4 Overview .......................................................................................................................................................................... 5 Abbreviations ..................................................................................................................................................................................... 6 GNSS testing with the R&S®SMW200A ............................................................................................................................................. 6 Minimum instrument configuration for GNSS testing .......................................................................................................................... 7 Minimum instrument configuration for avionics testing ....................................................................................................................... 7 Global navigation satellite systems (GNSS) ................................................................................................................. 8 Addressed GNSS applications .......................................................................................................................................................... -
Antennas for High-Precision GNSS Applications
Antennas for High-Precision GNSS Applications Roshni Prasad Associate Engineer – RF & Connectivity Abracon, LLC Antennas for High-Precision GNSS Applications | Abracon LLC Abstract: The increasing interest in high-precision GNSS/GPS services has led to the development of novel antenna solutions to service various end-customer applications in markets such as agriculture, recreation, surveying & mapping, and timing. Multi-band receivers and antennas are required to derive a higher-precision rate on positioning. However, using dedicated antennas for widely separated multi- band support may introduce several challenges in the design, including increased occupancy in board space and coupling. This application note reviews how these challenges are addressed by employing a single multi-band antenna. The discussion primarily focuses on Abracon’s internal and external antenna solutions that can cover multiple GPS and/or GNSS bands as a single entity for precision positioning applications. Index Introduction to GNSS Antennas for Multi-band GNSS Receivers Types of Antennas for Multi-Band GNSS Receivers Integrating Antennas in GNSS Applications Key Factors in Determining Antenna Performance Advantages of Using Multi-band GNSS Conclusion References Page | 2 5101 Hidden Creek Ln Spicewood TX 78669 | 512.371.6159 | www.abracon.com Antennas for High-Precision GNSS Applications | Abracon LLC 1. Introduction to GNSS What is GNSS? Why is GNSS needed? What are the available constellations? Global Navigation Satellite System (GNSS) is a satellite-based navigation and positioning system that offers a prediction of coordinates in space, with respect to velocity and time, to assist in the navigation and positioning of receiver systems. The service is supported by various global constellations, including GPS (U.S.), GLONASS (Russia), Galileo (Europe), and regional constellations such as BeiDou (China), QZSS (Japan) and IRNSS (India). -
GLONASS & GPS HW Designs
GLONASS & GPS HW designs Recommendations with u-blox 6 GPS receivers Application Note Abstract This document provides design recommendations for GLONASS & GPS HW designs with u-blox 6 module or chip designs. u-blox AG Zürcherstrasse 68 8800 Thalwil Switzerland www.u-blox.com Phone +41 44 722 7444 Fax +41 44 722 7447 [email protected] GLONASS & GPS HW designs - Application Note Document Information Title GLONASS & GPS HW designs Subtitle Recommendations with u-blox 6 GPS receivers Document type Application Note Document number GPS.G6-CS-10005 Document status Preliminary This document and the use of any information contained therein, is subject to the acceptance of the u-blox terms and conditions. They can be downloaded from www.u-blox.com. u-blox makes no warranties based on the accuracy or completeness of the contents of this document and reserves the right to make changes to specifications and product descriptions at any time without notice. u-blox reserves all rights to this document and the information contained herein. Reproduction, use or disclosure to third parties without express permission is strictly prohibited. Copyright © 2011, u-blox AG. ® u-blox is a registered trademark of u-blox Holding AG in the EU and other countries. GPS.G6-CS-10005 Page 2 of 16 GLONASS & GPS HW designs - Application Note Contents Contents .............................................................................................................................. 3 1 Introduction ................................................................................................................. -
AVL Systems for Bus Transit
T R A N S I T C O O P E R A T I V E R E S E A R C H P R O G R A M SPONSORED BY The Federal Transit Administration TCRP Synthesis 24 AVL Systems for Bus Transit A Synthesis of Transit Practice Transportation Research Board National Research Council TCRP OVERSIGHT AND PROJECT TRANSPORTATION RESEARCH BOARD EXECUTIVE COMMITTEE 1997 SELECTION COMMITTEE CHAIRMAN OFFICERS MICHAEL S. TOWNES Peninsula Transportation District Chair: DAVID N. WORMLEY, Dean of Engineering, Pennsylvania State University Commission Vice Chair: SHARON D. BANKS, General Manager, AC Transit Executive Director: ROBERT E. SKINNER, JR., Transportation Research Board, National Research Council MEMBERS SHARON D. BANKS MEMBERS AC Transit LEE BARNES BRIAN J. L. BERRY, Lloyd Viel Berkner Regental Professor, Bruton Center for Development Studies, Barwood, Inc University of Texas at Dallas GERALD L. BLAIR LILLIAN C. BORRONE, Director, Port Department, The Port Authority of New York and New Jersey (Past Indiana County Transit Authority Chair, 1995) SHIRLEY A. DELIBERO DAVID BURWELL, President, Rails-to-Trails Conservancy New Jersey Transit Corporation E. DEAN CARLSON, Secretary, Kansas Department of Transportation ROD J. DIRIDON JAMES N. DENN, Commissioner, Minnesota Department of Transportation International Institute for Surface JOHN W. FISHER, Director, ATLSS Engineering Research Center, Lehigh University Transportation Policy Study DENNIS J. FITZGERALD, Executive Director, Capital District Transportation Authority SANDRA DRAGGOO DAVID R. GOODE, Chairman, President, and CEO, Norfolk Southern Corporation CATA DELON HAMPTON, Chairman & CEO, Delon Hampton & Associates LOUIS J. GAMBACCINI LESTER A. HOEL, Hamilton Professor, University of Virginia. Department of Civil Engineering SEPTA JAMES L. -
AEN-88: the Global Positioning System
AEN-88 The Global Positioning System Tim Stombaugh, Doug McLaren, and Ben Koostra Introduction cies. The civilian access (C/A) code is transmitted on L1 and is The Global Positioning System (GPS) is quickly becoming freely available to any user. The precise (P) code is transmitted part of the fabric of everyday life. Beyond recreational activities on L1 and L2. This code is scrambled and can be used only by such as boating and backpacking, GPS receivers are becoming a the U.S. military and other authorized users. very important tool to such industries as agriculture, transporta- tion, and surveying. Very soon, every cell phone will incorporate Using Triangulation GPS technology to aid fi rst responders in answering emergency To calculate a position, a GPS receiver uses a principle called calls. triangulation. Triangulation is a method for determining a posi- GPS is a satellite-based radio navigation system. Users any- tion based on the distance from other points or objects that have where on the surface of the earth (or in space around the earth) known locations. In the case of GPS, the location of each satellite with a GPS receiver can determine their geographic position is accurately known. A GPS receiver measures its distance from in latitude (north-south), longitude (east-west), and elevation. each satellite in view above the horizon. Latitude and longitude are usually given in units of degrees To illustrate the concept of triangulation, consider one satel- (sometimes delineated to degrees, minutes, and seconds); eleva- lite that is at a precisely known location (Figure 1). If a GPS tion is usually given in distance units above a reference such as receiver can determine its distance from that satellite, it will have mean sea level or the geoid, which is a model of the shape of the narrowed its location to somewhere on a sphere that distance earth.