The Origins of GPS
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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 -
Owner's Manual
OWNER’S MANUAL M197WD M227WD M237WD Make sure to read the Safety Precautions before using the product. Keep the User's Guide(CD) in an accessible place for furture reference. See the label attached on the product and give the information to your dealer when you ask for service. Trade Mark of the DVB Digital Video Broadcasting Project (1991 to 1996) ID Number(s): 5741 : M227WD 5742 : M197WD 5890 : M237WD PREPARATION FRONT PANEL CONTROLS I This is a simplified representation of the front panel. The image shown may be somewhat different from your set. INPUT INPUT Button MENU MENU Button OK OK Button VOLUME VOL Buttons PROGRAMME PR Buttons Power Button Headphone Button 1 PREPARATION <M197WD/M227WD> BACK PANEL INFORMATION I This is a simplified representation of the back panel. The image shown may be somewhat different from your set. 1 2 3 4 5 6 7 COMPONENT AV-IN 3 AUDIO IN IN (RGB/DVI) AV 1 AV 2 OPTICAL Y DIGITAL AV 1 AV 2 AUDIO OUT VIDEO AUDIO 1 B P VIDEO HDMI RGB IN (PC) (MONO) AC IN 2 PR L DVI-D ANTENNA L IN AC IN SERVICE R AUDIO ONLY RS-232C IN (CONTROL & SERVICE) R S-VIDEO 8 9 10 11 12 13 14 1 PCMCIA (Personal Computer Memory Card 7 Audio/Video Input International Association) Card Slot Connect audio/video output from an external device (This feature is not available in all countries.) to these jacks. 2 Power Cord Socket 8 SERVICE ONLY PORT This set operates on AC power. The voltage is indicat- ed on the Specifications page. -
50 Satellite Formation-Flying and Rendezvous
Parkinson, et al.: Global Positioning System: Theory and Applications — Chap. 50 — 2017/11/26 — 19:03 — page 1 1 50 Satellite Formation-Flying and Rendezvous Simone D’Amico1) and J. Russell Carpenter2) 50.1 Introduction to Relative Navigation GNSS has come to play an increasingly important role in satellite formation-flying and rendezvous applications. In the last decades, the use of GNSS measurements has provided the primary method for determining the relative position of cooperative satellites in low Earth orbit. More recently, GNSS data have been successfully used to perform formation-flying in highly elliptical orbits with apogees at tens of Earth radii well above the GNSS constellations. Current research aims at dis- tributed precise relative navigation between tens of swarming nano- and micro-satellites based on GNSS. Similar to terrestrial applications, GNSS relative navigation benefits from a high level of common error cancellation. Furthermore, the integer nature of carrier phase ambiguities can be exploited in carrier phase differential GNSS (CDGNSS). Both aspects enable a substantially higher accuracy in the estimation of the relative motion than can be achieved in single-spacecraft navigation. Following historical remarks and an overview of the state-of-the-art, this chapter addresses the technology and main techniques used for spaceborne relative navigation both for real-time and offline applications. Flight results from missions such as the Space Shuttle, PRISMA, TanDEM-X, and MMS are pre- sented to demonstrate the versatility and broad range of applicability of GNSS relative navigation, from precise baseline determination on-ground (mm-level accuracy), to coarse real-time estimation on-board (m- to cm-level accuracy). -
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 -
2008 Annual Report
2008 Annual Report NATIONAL ACADEMY OF ENGINEERING ENGINEERING THE FUTURE 1 Letter from the President 3 In Service to the Nation 3 Mission Statement 4 Program Reports 4 Engineering Education 4 Center for the Advancement of Scholarship on Engineering Education 6 Technological Literacy 6 Public Understanding of Engineering Developing Effective Messages Media Relations Public Relations Grand Challenges for Engineering 8 Center for Engineering, Ethics, and Society 9 Diversity in the Engineering Workforce Engineer Girl! Website Engineer Your Life Project Engineering Equity Extension Service 10 Frontiers of Engineering Armstrong Endowment for Young Engineers-Gilbreth Lectures 12 Engineering and Health Care 14 Technology and Peace Building 14 Technology for a Quieter America 15 America’s Energy Future 16 Terrorism and the Electric Power-Delivery System 16 U.S.-China Cooperation on Electricity from Renewables 17 U.S.-China Symposium on Science and Technology Strategic Policy 17 Offshoring of Engineering 18 Gathering Storm Still Frames the Policy Debate 20 2008 NAE Awards Recipients 22 2008 New Members and Foreign Associates 24 2008 NAE Anniversary Members 28 2008 Private Contributions 28 Einstein Society 28 Heritage Society 29 Golden Bridge Society 29 Catalyst Society 30 Rosette Society 30 Challenge Society 30 Charter Society 31 Other Individual Donors 34 The Presidents’ Circle 34 Corporations, Foundations, and Other Organizations 35 National Academy of Engineering Fund Financial Report 37 Report of Independent Certified Public Accountants 41 Notes to Financial Statements 53 Officers 53 Councillors 54 Staff 54 NAE Publications Letter from the President Engineering is critical to meeting the fundamental challenges facing the U.S. economy in the 21st century. -
Galileo FOC-M7 SAT 19-20-21-22
LAUNCH KIT December 2017 VA240 Galileo FOC-M7 SAT 19-20-21-22 VA240 Galileo FOC-M7 SAT 19-20-21-22 ARIANESPACE’S SECOND ARIANE 5 LAUNCH FOR THE GALILEO CONSTELLATION AND EUROPE For its 11th launch of the year, and the sixth Ariane 5 liftoff from the Guiana Space Center (CSG) in French Guiana during 2017, Arianespace will orbit four more satellites for the Galileo constellation. This mission is being performed on behalf of the European Commission under a contract with the European Space Agency (ESA). For the second time, an Ariane 5 ES version will be used to orbit satellites in Europe’s own satellite navigation system. At the completion of this flight, designated Flight VA240 in Arianespace’s launcher family numbering system, 22 Galileo spacecraft will have been launched by Arianespace. Arianespace is proud to deploy its entire family of launch vehicles to address Europe’s needs and guarantee its independent access to space. Galileo, an iconic European program Galileo is Europe’s own global navigation satellite system. Under civilian control, Galileo offers guaranteed high-precision positioning around the world. Its initial services began in December CONTENTS 2016, allowing users equipped with Galileo-enabled devices to combine Galileo and GPS data for better positioning accuracy. The complete Galileo constellation will comprise a total of 24 operational satellites (along with > THE LAUNCH spares); 18 of these satellites already have been orbited by Arianespace. ESA transferred formal responsibility for oversight of Galileo in-orbit operations to the GSA VA240 mission (European GNSS Agency) in July 2017. Page 3 Therefore, as of this launch, the GSA will be in charge of the operation of the Galileo satellite Galileo FOC-M7 satellites navigation systems on behalf of the European Union. -
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. -
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. -
Creating Intelligent Machines at Deere &
THE 2018 CT HALL OF FAME CES 2019 PREVIEW NOVEMBERDECEMBER 2018 BLOCKCHAIN NEW WAYS TO TRANSACT SMART CARS MONITORING DRIVERS TECH CONNECTING DOCTORS WITH PATIENTS SENIOR VP, INTELLIGENT SOLUTIONS GROUP John Stone Creating Intelligent Machines at Deere & Co. i3_1118_C1_COVER_layout.indd 1 10/24/18 3:50 PM MEET THE MOST IRRESISTIBLE NEW POWER COUPLE EVERYBODY’S TALKING Sharp’s all-new, modern and elegant, built-in wall oven features an edge-to-edge black glass and stainless steel design. The SWA3052DS pairs beautifully with our new SMD2480CS Microwave DrawerTM, the new power couple of style and performance. This 5.0 cu. ft. 240V. built-in wall oven uses True European Convection to cook evenly and heat effi ciently. The 8 pass upper-element provides edge-to-edge performance. Sharp’s top-of-the-line Microwave Drawer™ features Easy Wave Open for touchless operation. Hands full? Simply wave up-and-down near the motion sensor and the SMD2480CS glides open. It’s just the kind of elegant engineering, smart functionality and cutting-edge performance you’d expect from Sharp. NEW TOUCH GLASS CONTROL PANEL EDGE-TO-EDGE, BLACK GLASS & STAINLESS STEEL OPTIONAL 30" EXTENSION KIT SHOWN Simply Better Living www.SharpUSA.com © 2018 Sharp Electronics Corporation. All rights reserved. Sharp, Microwave Drawer™ Oven and all related trademarks are trademarks or regis- tered trademarks of Sharp Corporation and/or its affi liated entities. Product specifi cations and design are subject to change without notice. Internal capacity calculated by measuring maximum width, -
REM110 Universal Remote
Thank you for purchasing a Philips Magnavox 3 device univer- sal remote control. This universal remote control will operate your Television,Video Cassette Recorder, and Cable Converter Box. Before you can use your new remote control, you will need to program it to operate the specific components you wish to control. This remote features: • Channel Scan, a convenient way to "channel surf" by scanning channels. • Auto Scan code search to help program remote REM110 control for a variety of components, including Universal Remote older/discontinued models. • Built-in Sleep Timer. • Controls for basic functions, including Power, Channel Selection,Volume, Play and Record. KEYS AND FUNCTIONS 2 1 5 8 3 4 4 7 6 3 9 9 11 10 12 12 13 14 2 1 Red Indicator Light 9 Keypad Replacement and Code Saver The Red Indicator Light blinks Use the keypad (0-9) to to show that the remote con- directly enter in channels (for When the batteries need replacing the remote control will stop work- trol is working and also pro- example, 09 or 31). The key- ing and will require two (2) new "AA" alkaline batteries for continued vides feed back during pro- pad is also used for all pro- operation. Once you remove the old batteries, program settings and gramming sequences. gramming sequences, such as codes will be saved for 10 minutes, allowing adequate time to insert entering in your programming new ones. 2 Component Keys codes. Press TV,VCR or CBL once However, if you do not replace the batteries within the allotted time to select a home entertain- 10 SLEEP Key (e.g., 10 minutes), you will have to reprogram the remote control. -
L-G-0015436434-0054602840.Pdf
Position, Navigation, and Timing Technologies in the 21st Century IEEE Press 445 Hoes Lane Piscataway, NJ 08854 IEEE Press Editorial Board Ekram Hossain, Editor in Chief Jón Atli Benediktsson David Alan Grier Elya B. Joffe Xiaoou Li Peter Lian Andreas Molisch Saeid Nahavandi Jeffrey Reed Diomidis Spinellis Sarah Spurgeon Ahmet Murat Tekalp Position, Navigation, and Timing Technologies in the 21st Century Integrated Satellite Navigation, Sensor Systems, and Civil Applications Volume 1 Edited by Y. T. Jade Morton, University of Colorado Boulder Frank van Diggelen, Google James J. Spilker, Jr., Stanford University Bradford W. Parkinson, Stanford University Associate Editors: Sherman Lo, Stanford University Grace Gao, Stanford University Copyright © 2021 by The Institute of Electrical and Electronics Engineers, Inc. All rights reserved. Published by John Wiley & Sons, Inc., Hoboken, New Jersey. Published simultaneously in Canada. No part of this publication may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, recording, scanning, or otherwise, except as permitted under Section 107 or 108 of the 1976 United States Copyright Act, without either the prior written permission of the Publisher, or authorization through payment of the appropriate per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923, (978) 750-8400, fax (978) 750-4470, or on the web at www.copyright.com. Requests to the Publisher for permission should be addressed to the Permissions Department, John Wiley & Sons, Inc., 111 River Street, Hoboken, NJ 07030, (201) 748-6011, fax (201) 748-6008, or online at http://www.wiley.com/go/permissions. -
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.