Global Positioning System
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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 -
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 -
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. -
The Navy Navigation Satellite System (Transit)
ROBERT J. DANCHIK THE NAVY NAVIGATION SATELLITE SYSTEM (TRANSIT) This article provides an update on the status of the Navy Navigation Satellite System (TRANSIT). Some insights are provided on the evolution of the system into its current configuration, as well as a discussion of future plans. BACKGROUND sign goal was never achieved for long in those early In 1958, research scientists at APL solved the orbit days because the satellites had short operational life of the first Russian satellite, Sputnik-I, by analysis of times. The failures largely resulted from inadequate the observed Doppler shift of its transmitted signal. component quality and the large number of wiring in This led immediately to the concept of satellite navi terconnections. However, after OSCAR 2 10 and OS gation and the development of the U.S. Navy Navi CAR 12 were launched in 1966 and 1967, respectively, gation Satellite System (TRANSIT) by APL, under the enough data on the failure mechanisms became avail sponsorship of the Navy's Special Projects Office, to able to APL to achieve the desired advances in reli provide position fixes for the Fleet Ballistic Missile ability. The integrated circuit introduced in OSCAR Weapon System submarines. (The articles in Ref. 1, 10 significantly extended the satellite lifetime by im a previous issue of the fohns Hopkins APL Techni proving component reliability and reducing the num cal Digest devoted to TRANSIT, give the principles ber of interconnections. Subsequently, the last major of operation and early history of the system.) Now, design change made to the solar cell interconnections, 26 years after its conception, the system is mature. -
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. -
Overview of the BDS III Signals
2018/11/17 13th Stanford PNT Symposium Overview of the BDS III Signals Mingquan Lu Tsinghua University November 8, 2018 Outline 1. Introduction The Three-step Development Plan A Brief History of BDS Development The Evolution of BDS Signals Current Status 2. Brief Description of BDS III 3. New Signals of BDS III 4. Conclusion 1 2018/11/17 The Three-step Development Plan BDS program began in the 1990s. In order to overcome various difficulties, China formulated the following three- step development plan for BDS, from active to passive, from regional to global. BDS I BDS II BDS III Experimental System Regional System Global System 2000 IOC, 2003 FOC 2010 IOC, 2012 FOC 2018 IOC, 2020 FOC 3GEO 5GEO+5IGSO+4MEO 3GEO+3IGSO+24MEO Regional Coverage Regional Coverage Global Coverage RDSS Service RDSS/RNSS Service RDSS/RNSS/SBAS Service 3 The Three-step Development Plan Step 3 (BDS III) Start the development of Step 2 (BDS II) the BDS Global System (BDS III) in 2013 to Start the development of achieve global passive Step 1 (BDS I) the BDS Regional System PNT capability by (BDS II, also known as approximately 2020. Start the development of BD-II in earlier times) in the BDS Experimental 2004 to achieve regional System (BDS I, also passive PNT capability by known as BD-I in earlier 2012. times) in 1994 to achieve regional active PNT capability by 2000. 4 2 2018/11/17 A Brief History of BDS Development The Early Active System BDS I——BDS Experimental System BDS I BDS I was established in 2000 as the first Experimental System generation of China’s navigation satellite system. -
Technological Principles and the Policy Challenges of the Global Positioning System
Technological Principles and the Policy Challenges of the Global Positioning System Marlee Chong Spring 2013 Contents 1 Introduction 3 2 History 4 2.1 Location . .4 2.2 LORAN . .5 2.3 GPS Predecessors . .5 2.4 Developing GPS . .6 3 Technology 8 3.1 User Segment . .8 3.2 Control Segment . .8 3.3 Space Segment . .9 3.4 Signal . 10 3.5 Pseudoranging . 11 3.6 Errors and Accuracy . 12 3.6.1 Clock Errors . 12 3.6.2 Atmospheric Errors . 13 3.6.3 System Noise . 13 3.6.4 Multipath Errors . 13 3.6.5 Dilution of Precision . 14 3.6.6 Accuracy . 14 3.7 Vulnerabilities . 15 4 Applications 16 4.1 Military: Smart Bombs . 16 4.2 Positioning: Fault Monitoring . 16 4.3 Navigation: Mobile Phones . 17 4.4 Timing: Stock Exchanges . 17 4.5 Satellites: Nuclear Test Detection . 18 4.6 Signals: Weather Forecasting . 18 5 Policy 19 5.1 Domestic Governance . 19 5.1.1 Defense . 19 1 CONTENTS 2 5.1.2 Civil . 20 5.1.3 Privacy Issues . 21 5.2 Competing Systems . 21 5.2.1 USSR and Russia . 22 5.2.2 European Union . 22 5.2.3 China . 22 5.2.4 Japan . 23 5.2.5 India . 23 5.2.6 International Cooperation . 23 5.3 Modernization . 23 5.3.1 Space Segment . 24 5.3.2 Control Segment . 24 5.3.3 Replacement . 24 5.4 Future and Recommendations . 25 6 Conclusion 26 7 Acknowledgements 27 Chapter 1 Introduction The Global Positioning System (GPS) has become a part of everyday life. -
An Overview of Global Positioning System (GPS)
Technical Article February 2012 | page 1 An Overview of Global Positioning System (GPS) The Global Positioning System (GPS) is a satellite–based radio–navigation system. GPS provides reliable positioning, navigation, and timing services to users on a continuous worldwide basis. The satellite system was built by the United States, but its services are freely available to everyone on the planet. For anyone with a GPS receiver, the system provides location and time. GPS provides accurate location and time information for an unlimited number of people in all weather, day or night, anywhere in the world. The GPS is made up of three parts: satellites orbiting the Earth; control and monitoring stations on Earth; and the GPS receivers (either stand–alone devices or integrated sub–systems) operated by users. GPS satellites broadcast continuous signals which are picked up and identified by GPS receivers. Each GPS receiver then provides three–dimensional location information (latitude, longitude, and altitude), plus the current time. Equipped with a GPS receiver, any user can accurately locate where they are and easily navigate to where they want to go, whether walking, driving, flying, or boating. GPS has become an important part of transportation systems worldwide, providing navigation for aviation, ground, and maritime operations. Disaster relief and emergency service agencies depend upon GPS for location and timing capabilities in their life–saving missions. Everyday activities such as banking, mobile phone operations, and even the control of power grids, are facilitated by the accurate timing provided by GPS. Farmers, surveyors, geologists and countless others perform their work more efficiently, safely, economically, and accurately using the free and open GPS signals. -
Missions Objectives of the Doris System
MISSIONS OF THE DORIS SYSTEM Luis RUIZ , Pierre SENGENES, Pascale ULTRE-GUERARD Centre National d’Etudes Spatiales RESUME – Ce document a pour objet de donner un aperçu des applications du système DORIS, principalement dans les domaines de l’altimétrie océanographique et de la géodésie. Il indique quelles sont les missions opérationnelles qui utilisent DORIS et celles pour lesquelles DORIS est candidat. Il décrit succinctement les principes de fonctionnement du système et en donne les principales performances. ABSTRACT - The purpose of this paper is to provide an overview of the DORIS applications in support of radar altimetry or geodetic missions. It mentions the operational programs currently using the DORIS system as well as the future programs for which DORIS is a candidate payload. 1- HISTORY : The DORIS (Doppler Orbitography and Radiopositioning Integrated by Satellite) was designed and developed by CNES, the Groupe de Recherche Spatiale GRGS (CNES/CNRS/Université Paul Sabatier) and IGN in 1982 to cover new requirements concerning precise orbit determination. As such, DORIS was proposed in support of POSEIDON oceanographic altimetric experiment and was embarked on the TOPEX satellite (launched in August 92). DORIS is then part of the scientific payload, and is a primary sensor for the orbit determination which requires an accuracy in the order of 2 to 3 cm to achieve the large scale ocean monitoring needed for the altimetric mission. The in-flight validation of DORIS was achieved before the TOPEX/POSEIDON experiment, by flying an experimental DORIS payload on board the observation satellite SPOT 2 (launched in 1990). 2- MISSIONS : Although the DORIS system was originally designed to perform very precise orbit determination of low Earth orbiting satellites for ocean altimetry experiments, many applications have been developed since. -
Global Navigation Satellite Systems and Their Applications Dr
ISSN (Print): 2279-0063 International Association of Scientific Innovation and Research (IASIR) (An Association Unifying the Sciences, Engineering, and Applied Research) ISSN (Online): 2279-0071 International Journal of Software and Web Sciences (IJSWS) www.iasir.net Global Navigation Satellite Systems and Their Applications Dr. G. Manoj Someswar1, T. P. Surya Chandra Rao2, Dhanunjaya Rao. Chigurukota3 1Principal and Professor, Department of CSE, AUCET, Vikarabad, A.P. 2Associate Professor in Department of CSE 3Associate Professor in Nasimhareddy Engineering Collge ABSTRACT: Global Navigation Satellite System (GNSS) plays a significant role in high precision navigation, positioning, timing, and scientific questions related to precise positioning. Ofcourse in the widest sense, this is a highly precise, continuous, all-weather and a real-time technique. This Research Article is devoted to presenting recent results and developments in GNSS theory, system, signal, receiver, method and errors sources such as multipath effects and atmospheric delays. To make it more elaborative, this varied GNSS applications are demonstrated and evaluated in hybrid positioning, multi- sensor integration, height system, Network Real Time Kinematic (NRTK), wheeled robots, status and engineering surveying. This research paper provides a good reference for GNSS designers, engineers, and scientists as well as the user market. I. USE AND APPLICATIONS OF GLOBAL NAVIGATION SATELLITE SYSTEMS In the year 2001, pursuant to the Third United Nations Conference on the Exploration and Peaceful Uses of Outer Space (UNISPACE-III), the United Nations Committee on the Peaceful Uses of Outer Space (COPUOS) established the Action Team on Global Navigation Satellite Systems (GNSS) under the leadership of the United States and Italy and with the voluntary participation of 38 Member States and 15 organizations. -
A History of Maritime Radio- Navigation Positioning Systems Used in Poland
THE JOURNAL OF NAVIGATION (2016), 69, 468–480. © The Royal Institute of Navigation 2016 This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted re-use, distribution, and reproduction in any medium, provided the original work is properly cited. doi:10.1017/S0373463315000879 A History of Maritime Radio- Navigation Positioning Systems used in Poland Cezary Specht, Adam Weintrit and Mariusz Specht (Gdynia Maritime University, Gdynia, Poland) (E-mail: [email protected]) This paper describes the genesis, the principle of operation and characteristics of selected radio-navigation positioning systems, which in addition to terrestrial methods formed a system of navigational marking constituting the primary method for determining the location in the sea areas of Poland in the years 1948–2000, and sometimes even later. The major ones are: maritime circular radiobeacons (RC), Decca-Navigator System (DNS) and Differential GPS (DGPS), as well as solutions forgotten today: AD-2 and SYLEDIS. In this paper, due to its limited volume, the authors have omitted the description of the solutions used by the Polish Navy (RYM, BRAS, JEMIOŁUSZKA, TSIKADA) and the global or continental systems (TRANSIT, GPS, GLONASS, OMEGA, EGNOS, LORAN, CONSOL) - described widely in world literature. KEYWORDS 1. Radio-Navigation. 2. Positioning systems. 3. Decca-Navigator System (DNS). 4. Maritime circular radiobeacons (RC). 5. AD-2 system. 6. SYLEDIS. 7. Differential GPS (DGPS). Submitted: 21 June 2015. Accepted: 30 October 2015. First published online: 11 January 2016. 1. INTRODUCTION. Navigation is the process of object motion control (Specht, 2007), thus determination of position is its essence.