ABAS), Satellite-Based Augmentation System (SBAS), Or Ground-Based Augmentation System (GBAS
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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 -
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 -
Flight Inspection History Written by Scott Thompson - Sacramento Flight Inspection Office (May 2008)
Flight Inspection History Written by Scott Thompson - Sacramento Flight Inspection Office (May 2008) Through the brief but brilliant span of aviation history, the United States has been at the leading edge of advancing technology, from airframe and engines to navigation aids and avionics. One key component of American aviation progress has always been the airway and navigation system that today makes all-weather transcontinental flight unremarkable and routine. From the initial, tentative efforts aimed at supporting the infant air mail service of the early 1920s and the establishment of the airline industry in the 1930s and 1940s, air navigation later guided aviation into the jet age and now looks to satellite technology for direction. Today, the U.S. Federal Aviation Administration (FAA) provides, as one of many services, the management and maintenance of the American airway system. A little-seen but still important element of that maintenance process is airborne flight inspection. Flight inspection has long been a vital part of providing a safe air transportation system. The concept is almost as old as the airways themselves. The first flight inspectors flew war surplus open-cockpit biplanes, bouncing around with airmail pilots and watching over a steadily growing airway system predicated on airway light beacons to provide navigational guidance. The advent of radio navigation brought an increased importance to the flight inspector, as his was the only platform that could evaluate the radio transmitters from where they were used: in the air. With the development of the Instrument Landing System (ILS) and the Very High Frequency Omni-directional Range (VOR), flight inspection became an essential element to verify the accuracy of the system. -
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). -
Microwave Landing System Autoland System Analysis
//t/- o_, / _/_1_ NASA Contractor Report CR- 189551 (NASA-CR-I89551) MICROWAVE LANnING SYSTEM N92-15060 AUTOLAND SYSTEM ANALYSIS Final _eport (Oouglas Aircraft Co.) 62 p CSCL 17G Unclas G3104 0061512 Microwave Landing System Autoland System Analysis J. B. Feather B. K. Craven _elI Douglas Corporation Douglas Aircraft Company Long Beach, California December 1991 Prepared for NASA-Langley Research Center Under Contract NAS 1-18028 NationalAeronautics and S-paceAdministration NASA Contractor Report CR- 189551 Microwave Landing System Autoland System Analysis J. B. Feather B. K. Craven McDonnell Douglas Corporation Douglas Aircraft Company Long Beach, Califomia December 1991 Prepared for NASA-Langley Research Center Under Contract NAS 1-18028 IXl/k.. A National Aeronautics and Space Administration ACKNOWLEDGEMENT The study described herein was the result of a team effort in which many different technical disciplines were represented. In particular, the participation of the following coworkers greatly contributed to the program: MD-80 Program: Vinh Bui Leo Christofferson Ha Nguyen Tracy Ton Jessie Turner Flight Control Technology: Steve Goldthorpe Timm Ortman Flight Operations: Frank Anderson Bear Smith CONTENTS Section Page 1 EXECUTIVE SUMMARY .......................................... 1 2 CONCLUSIONS AND RECOMMENDATIONS ........................ 3 2.1 Conclusions ........................ "........................ 3 2.2 Recommendations ........................................... 3 2.2.1 Follow-on Studies .................................... -
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. -
GLONASS Spacecraft
INNO V AT IO N The task of designing and developing the GLONASS GLONASS spacecraft fell to the Scientific Production Association of Applied Mechan ics (Nauchno Proizvodstvennoe Ob"edinenie Spacecraft Prikladnoi Mekaniki or NPO PM) , located near Krasnoyarsk in Siberia. This major aero Nicholas L. Johnson space industrial complex was established in 1959 as a division of Sergei Korolev 's Kaman Sciences Corporation Expe1imental Design Bureau (Opytno Kon struktorskoe Byuro or OKB). (Korolev , among other notable achievements , led the Fourteen years after the launch of the effort to develop the Soviet Union's first first test spacecraft, the Russian Global Nav launch vehicle - the A launcher - which igation Satellite System (Global 'naya Navi placed Sputnik 1 into orbit.) The founding gatsionnaya Sputnikovaya Sistema or and current general director and chief GLONASS) program remains viable and designer is Mikhail Fyodorovich Reshetnev, essentially on schedule despite the economic one of only two still-active chief designers and political turmoil surrounding the final from Russia's fledgling 1950s-era space years of the Soviet Union and the emergence program. of the Commonwealth of Independent States A closed facility until the early 1990s, (CIS). By the summer of 1994, a total of 53 NPO PM has been responsible for all major GLONASS spacecraft had been successfully Russian operational communications, navi Despite the significant economic hardships deployed in nearly semisynchronous orbits; gation, and geodetic satellite systems to associated with the breakup of the Soviet Union of the 53 , nearly 12 had been normally oper date. Serial (or assembly-line) production of and the transition to a modern market economy, ational since the establishment of the Phase I some spacecraft, including Tsikada and Russia continues to develop its space programs, constellation in 1990. -
Leica Viva Series White Paper Beidou Integration
New Systems, New Signals Providing BeiDou Integration Technical literature December 2013 P. Fairhurst, X. Luo, J. Aponte, B. Richter, Leica Geosystems AG Switzerland Heerbrugg, Schweiz 2 | Technical literature New Systems, New Signals, New Positions – Providing BeiDou Integration Abstract In December 2012, the China Satellite Navigation Leica Geosystems is a world leader in GNSS Office (CSNO) released the official Signal-in-Space positioning and in utilizing innovative methods Interface Control Document (ICD; ICD-BeiDou, for providing high precision GNSS solutions. With 2012) and announced the system operability over new GNSS such as BeiDou and other signals and the Asia-Pacific region. regional systems providing a significant increase in satellite availability, new methods are required to The ICD release prompted Leica Geosystems to fully realize the potential benefits of these additi- release software to fully support the BeiDou cons- onal GNSS constellations. tellation in the Leica Viva GNSS technologies: However, before the potential of these new sys- n Leica SmartTrack tems can be fully realized, we must first under- n Leica SmartCheck stand what advantages they can provide when n Leica xRTK being used in a high precision GNSS solution. Leica Geosystems’ previous leading-edge work on These technologies form the basis of Leica Geo- GLONASS observation interoperability showed that systems GNSS RTK performance. Leica SmartTrack there are many challenges involved with incorpora- technology guarantees the most accurate signal ting new GNSS constellation into a position soluti- tracking. It is future proof and ensures compa- on, and careful evaluation needs to be carried out tibility with all GNSS systems today and tomor- to understand the behaviour and characteristics of row. -
GNSS Performance Monitoring
GNSS PERFORMANCE Monitoring SiS AVAILABILITY PARAMETER DEfiNITION AND EVALUATION M. DE Groot Master THESIS Geoscience & Remote Sensing GNSS Performance Monitoring SiS availability parameter definition and evaluation by M. de Groot to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Wednesday September 27, 2017 Student number: 4089456 Project duration: May 1, 2016 – July 1, 2017 Thesis committee: Prof. dr. ir. R. F.Hanssen, TU Delft Graduation supervisor Dr. ir. H. van der Marel, TU Delft Daily supervisor Ir. A. van den Berg, CGI Daily supervisor Ir. W. J. F. Simons, TU Delft Co-reader An electronic version of this thesis is available at http://repository.tudelft.nl/. Preface This thesis forms the end of my period at the TU Delft. I enjoyed studying the bachelor of civil engineering and the master track of geoscience & remote sensing. The track contained several interesting topics in which GNSS had my attention from the start. Many people make use of GNSS on a daily basis without actually knowing how it works. Position, velocity and timing results are obtained using satellites at 20000 kilometres above the Earth. Good performance is usually taken for granted, but performance monitoring is essential for any system. Using a monitoring tool with substantiated parameters can give the system more trust and can lead to new insights. I would like to thank my daily supervisors, Axel van den Berg and Hans van der Marel, for introducing me to this topic. Both were really helpful with all their knowledge, experience and feedback. I would also like to thank the people of the space department of CGI the Netherlands with their input and for giving me a place to work on the project. -
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. -
Orbital Debris: a Chronology
NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................