Balancing the Position in Space Between GPS and Galileo
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MSM Feb2020 Review2
SATCOM for Net-Centric Warfare MilsatMagazineFebruary 2020 issue This issue... SMC: Year of Success Kratos: Countering Threats from Space Maxar: Leveraging Commercial Innovation WTA: Hacking the Hacker Dispatches United States Space Command Kratos Defense L3Harris Get SAT 2nd SOPS Orbit Communications Comtech EF Data Maxar Technologies Booz Allen Hamilton Raytheon Schriever AFB Cover image is courtesy of Kratos Defense and Security Cover SNIPE Ad Publishing Operations Features Silvano Payne, Publisher + Executive Writer Dispatches Simon Payne, Chief Technical Officer Hartley G. Lesser, Editorial Director United States Space Command .................................................................................4 Pattie Lesser, Executive Editor Kratos Defense & Security Solutions .........................................................................6 Donald McGee, Production Manager Andy Bernard, Sales Director L3Harris................................................................................................................7 + 9 Teresa Sanderson, Operations Director Get SAT .....................................................................................................................8 Sean Payne, Business Development Director Space & Missile Systems Center...............................................................................10 Dan Makinster, Technical Advisor 2nd SOPS .................................................................................................................11 Wendy Lewis, Contributing Editor -
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. -
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. -
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 ........................................................................................................................ -
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. -
ONSITE PROGRAM July 8–11, 2019 Tutorials: July 8 Show Dates: July 9–10 Hyatt Regency, Long Beach, California Classified Session: July 11, the Aerospace Corporation
JOINT NAVIGATION CONFERENCE 2019 Positioning, Navigation and Timing Technologies: The Foundation for Military Ops and Homeland Security ONSITE PROGRAM July 8–11, 2019 Tutorials: July 8 Show Dates: July 9–10 Hyatt Regency, Long Beach, California Classified Session: July 11, The Aerospace Corporation Sponsored by the Military Division of the Institute of Navigation www.ion.org/jncwww.ion.org/jnc Technical Program Overview Track A: Beacon A Track B: Shoreline Ballroom Track C: Seaview Ballroom Track D: Beacon B TRACK AND CHAIR: David Wolfe Dr. David Chapman Elliott Kaplan Dr. Greg Reynolds USCG NAVCEN AFRL Space Vehicles Directorate The MITRE Corporation US Army MONDAY, JULY 8: TUTORIALS Advanced Celestial Navigation Systems 10:30 a.m. - 12:00 p.m. Precise Timekeeping and Applications DOD PNT Architecture (PNTA) Standard GPS 101 for Warfighter Platforms Lunch is on Your Own: 12:00 p.m. - 1:30 p.m. An Introduction to Cryptography with 1:30 p.m. - 3:00 p.m. GPS Resilience for the Warfighter DOD PNT Architecture (PNTA) Standard PNT Gaps for Autonomous Applications Attention to Navigation Break: 3:00 p.m. - 3:30 p.m. D1: Multi-GNSS Receivers for Military 3:30 p.m. – 5:00 p.m. A1: Autonomous Systems and PNT B1: PNT Requirements and Solutions C1: GPS Modernization Applications TUESDAY, JULY 9: FOUO SESSIONS A2: Complementary PNT 1: Naturally 8:30 a.m. – 10:00 a.m. B2: Modeling and Simulation 1 C2: Military GPS User Equipment 1 D2: Inertial Measurement Unit (IMU) 1 Occurring Measurement Sources Break in Exhibit Hall: 10:00 a.m. -
Nov 2019 Advisory Board Minutes
NATIONAL SPACE-BASED POSITIONING, NAVIGATION, AND TIMING ADVISORY BOARD Twenty-Fourth Meeting November 20-21, 2019 November 20-21, 2019 Hilton Oceanfront Cocoa Beach, Florida ADM (Ret. USCG) Thad Allen, Chair Mr. James J. Miller, Executive Director (page intentionally left blank) 2 Agenda (https://www.gps.gov/governance/advisory/meetings/2019-11/) WEDNESDAY, NOVEMBER 20, 2019 8:30 - 8:35 BOARD CONVENES Call to Order, Logistics, & Announcements Mr. James J. Miller, Executive Director, National Space-Based PNT Advisory Board, NASA Headquarters 8:35 - 9:30 Welcome & Kick-Off of 24th PNTAB Meeting Priorities & Proposed Topic Focus Areas Concise Roundtable Discussion VIEW PDF (3 MB) ADM Thad Allen, Chair; Hon. John Stenbit, Deputy Chair; Dr. Bradford Parkinson, 1st Vice- Chair; Governor Jim Geringer, 2nd Vice-Chair 9:30 - 9:45 National Coordination Office (NCO) for Space-based Positioning, Navigation, and Timing (PNT) PNT Policy Activity Update VIEW PDF (554 KB) Mr. Harold 'Stormy' Martin, Director, National Coordination Office for Space-Based PNT 9:45 - 10:00 Update on Air Force Space Command Reorganization Activities Role of GPS Integration Office VIEW PDF (992 KB) Lt Gen David Thompson, Vice-Commander, Air Force Space Command 10:00 - 10:30 GPS Program Status & Modernization Milestones IIIF, OCX, & Emerging Capabilities for Users VIEW PDF (1 MB) Lt Col Ken McDougall, Chief, GPS Integration Branch, GPS Integration Office, Space and Missile Systems Center (SMC) 10:30 - 10:45 BREAK 10:45 - 11:10 U.S. Dept. of Transportation (DOT) Developments on PNT Resiliency VIEW PDF (2 MB) Dr. Andrew Hansen, DOT Liaison to the GPS Program Office 11:10 - 11:35 3 DHS S&T PNT Program and Conformance Framework Science & Technology Directorate (S&T) Update VIEW PDF (630 KB) Mr. -
History of the GPS Program the Global Positioning System
History of the GPS Program The Global Positioning System (GPS) is the principal component and the only fully operational element of the Global Navigation Satellite System (GNSS). The history of the GPS program pre-dates the space age. In 1951, Dr. Ivan Getting designed a three-dimensional, position-finding system based on time difference of arrival of radio signals. Shortly after the launch of Sputnik scientists confirmed that Doppler distortion could be used to calculate ephemerides, and, conversely, if a satellites position were know, the position of a receiver on earth could be determined. Within two years of the launch of Sputnik the first of five low-altitude “Transit” satellites for global navigation was launched. In 1967, the first of three “Timation” satellites demonstrated that highly accurate clocks could be carried in space. In parallel with these efforts, the 621B program was developing many of the characteristics of today’s GPS system. In 1973 these parallel efforts were brought together into the NAVSTAR-Global Positioning System, managed by a joint program office headed by then-colonel Dr. Brad Parkinson at the United States Air Force Space and Missile Systems Organization. This office developed the GPS architecture and initiated the development of the first satellites, the worldwide control segment and ten types of user equipment. Today, it continues to sustain the system as the Global Positioning System Directorate of the Space and Missile Systems Center. All performance parameters for the system were verified during ground testing by 1978. Ten development satellites were launched successfully between 1978 and 1985 and the initial ground segment that would provide the critical uploads to the satellites was also developed. -
A TSB Business Support Solution Delivered Through the Technology Programme
A TSB business Support Solution Delivered through the Technology Programme 1 Where to now with GNSS? A TSB business Support Solution Delivered through the Technology Programme Peter Lancaster Technology Translator Location & Timing KTN What is the Location & Timing KTN? Knowledge Transfer Networks are funded by the UK government, through the Technology Strategy Board. Our role is to stimulate innovation through knowledge transfer. Between industry, universities, researchers etc. Primarily within the UK, but also increasingly with Europe and worldwide. Our specific focus is on technologies and applications that identify or use location, and timing. 2 What’s up there now? A TSB business Support Solution Delivered through the Technology Programme • GPS – 31 operational, plus 1 launched last month. 7 x Block IIR-M have L2C & L1M, L2M Lockheed Martin Global Positioning Satellite IIRM Artist Impression Lockheed Martin Global Positioning Satellite IIRM 3 A TSB business Support Solution Delivered through the Technology Programme http://en.wikipedia.org/wiki/File:ConstellationGPS.gif 4 What’s up there now? A TSB business Support Solution Delivered through the Technology Programme • GLONASS – 20 operational, incl 3 launched on Christmas Day 2008, 6 have a predicted life of less than 1 year. FDMA signals. • Beidou-1 – Geo-stationary, 2-way communication method – so limited users & accuracy. 3 operational, (2 needed to cover SE Asia). – Compass-M1 launched Apr 07 Picture: NPO PM to secure frequencies, G2 launched 15 th Apr 2009 Glonass-M (Uragan-M) Glonass is the Russian system. Currently undergoing an programme to replace and update the constellation. Currently 20 satellites operational, but several have a short predicted life span (2 are due to go out of service about now). -
EGU2014-9860-2, 2014 EGU General Assembly 2014 © Author(S) 2014
Geophysical Research Abstracts Vol. 16, EGU2014-9860-2, 2014 EGU General Assembly 2014 © Author(s) 2014. CC Attribution 3.0 License. Observation and simulation of AGW in Space Vyacheslav Kunitsyn (1), Alexander Kholodov (2), Elena Andreeva (1), Ivan Nesterov (1), Artem Padokhin (1), and Artem Vorontsov (1) (1) M.V.Lomonosov Moscow State University, Moscow, Russia ([email protected]), (2) Moscow Institute of Physics and Technology, Moscow, 141700, Russia Examples are presented of satellite observations and imaging of AGW and related phenomena in space travel- ling ionospheric disturbances (TID). The structure of AGW perturbations was reconstructed by satellite radio tomography (RT) based on the signals of Global Navigation Satellite Systems (GNSS). The experiments use different GNSS, both low-orbiting (Russian Tsikada and American Transit) and high-orbiting (GPS, GLONASS, Galileo, Beidou). The examples of RT imaging of TIDs and AGWs from anthropogenic sources such as ground explosions, rocket launching, heating the ionosphere by high-power radio waves are presented. In the latter case, the corresponding AGWs and TIDs were generated in response to the modulation in the power of the heating wave. The natural AGW-like wave disturbances are frequently observed in the atmosphere and ionosphere in the form of variations in density and electron concentration. These phenomena are caused by the influence of the near-space environment, atmosphere, and surface phenomena including long-period vibrations of the Earth’s surface, earthquakes, explosions, temperature heating, seisches, tsunami waves, etc. Examples of experimental RT reconstructions of wave disturbances associated with the earthquakes and tsunami waves are presented, and RT images of TIDs caused by the variations in the corpuscular ionization are demonstrated. -
Understanding GPS: Principles and Applications/[Editors], Elliott Kaplan, Christopher Hegarty.—2Nd Ed
Understanding GPS Principles and Applications Second Edition For a listing of recent titles in the Artech House Mobile Communications Series, turn to the back of this book. Understanding GPS Principles and Applications Second Edition Elliott D. Kaplan Christopher J. Hegarty Editors a r techhouse. com Library of Congress Cataloging-in-Publication Data Understanding GPS: principles and applications/[editors], Elliott Kaplan, Christopher Hegarty.—2nd ed. p. cm. Includes bibliographical references. ISBN 1-58053-894-0 (alk. paper) 1. Global Positioning System. I. Kaplan, Elliott D. II. Hegarty, C. (Christopher J.) G109.5K36 2006 623.89’3—dc22 2005056270 British Library Cataloguing in Publication Data Kaplan, Elliott D. Understanding GPS: principles and applications.—2nd ed. 1. Global positioning system I. Title II. Hegarty, Christopher J. 629’.045 ISBN-10: 1-58053-894-0 Cover design by Igor Valdman Tables 9.11 through 9.16 have been reprinted with permission from ETSI. 3GPP TSs and TRs are the property of ARIB, ATIS, ETSI, CCSA, TTA, and TTC who jointly own the copyright to them. They are subject to further modifications and are therefore provided to you “as is” for informational purposes only. Further use is strictly prohibited. © 2006 ARTECH HOUSE, INC. 685 Canton Street Norwood, MA 02062 All rights reserved. Printed and bound in the United States of America. No part of this book may be reproduced or utilized in any form or by any means, electronic or mechanical, includ- ing photocopying, recording, or by any information storage and retrieval system, without permission in writing from the publisher. All terms mentioned in this book that are known to be trademarks or service marks have been appropriately capitalized. -
Performance Evaluation of Satellite Navigation and Safety Case Development
Bernd Tiemeyer PERFORMANCE EVALUATION OF SATELLITE NAVIGATION AND SAFETY CASE DEVELOPMENT PERFORMANCE EVALUATION OF SATELLITE NAVIGATION AND SAFETY CASE DEVELOPMENT eingereicht von Dipl.-Ing. Bernd Tiemeyer Vollständiger Abdruck der an der Fakultät für Bauingenieur- und Vermessungswesen der Universität der Bundeswehr München zur Erlangung des akademischen Grades eines Doktors der Ingenieurwissenschaften (Dr.-Ing.) eingereichten Dissertation. Vorsitzender: Univ.-Prof. Dr.-Ing. B. Eissfeller 1. Berichterstatter: Univ.-Prof. Dr.-Ing. G. W. Hein 2. Berichterstatter: Univ.-Prof. Dr.-Ing. R. Onken Die Dissertation wurde am 17. Mai 2001 bei der Universität der Bundeswehr München, Werner-Heisenberg-Weg 39, D-85577 Neubiberg, eingereicht. Tag der mündlichen Prüfung: 17. Januar 2002 To Katrin, Andrew and my Parents Who will never realise how much they contributed to this work. ” Together with people outside the field of aviation, we find ourselves moving in a vicious cycle, where the machine, which depend on modern man for its invention, has made modern man dependent on its constant improvement for his security - even for his live. “ Charles A. Lindbergh in “The Spirit of St. Louis”, 1953 PREFACE The present thesis was developed during my activities as Project Manager in the area of Satellite Navigation and Safety at the EUROCONTROL Experimental Centre, Brétigny-sur- Orge, France. I would like to express my gratitude to Univ.-Prof. Dr.-Ing. Günter W. Hein, Director of the Institute of Geodesy and Navigation of the University of the Federal Armed Forces Munich, who encouraged me to embark on writing this doctorate thesis, gave continuous support and advice during numerous discussions and looked after the administrative procedures which led to the successful completion of my doctorate.