Gps History, Chronology, and Budgets
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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. -
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 ................................................................................................................. -
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. -
GPS Applications in Space
Space Situational Awareness 2015: GPS Applications in Space James J. Miller, Deputy Director Policy & Strategic Communications Division May 13, 2015 GPS Extends the Reach of NASA Networks to Enable New Space Ops, Science, and Exploration Apps GPS Relative Navigation is used for Rendezvous to ISS GPS PNT Services Enable: • Attitude Determination: Use of GPS enables some missions to meet their attitude determination requirements, such as ISS • Real-time On-Board Navigation: Enables new methods of spaceflight ops such as rendezvous & docking, station- keeping, precision formation flying, and GEO satellite servicing • Earth Sciences: GPS used as a remote sensing tool supports atmospheric and ionospheric sciences, geodesy, and geodynamics -- from monitoring sea levels and ice melt to measuring the gravity field ESA ATV 1st mission JAXA’s HTV 1st mission Commercial Cargo Resupply to ISS in 2008 to ISS in 2009 (Space-X & Cygnus), 2012+ 2 Growing GPS Uses in Space: Space Operations & Science • NASA strategic navigation requirements for science and 20-Year Worldwide Space Mission space ops continue to grow, especially as higher Projections by Orbit Type* precisions are needed for more complex operations in all space domains 1% 5% Low Earth Orbit • Nearly 60%* of projected worldwide space missions 27% Medium Earth Orbit over the next 20 years will operate in LEO 59% GeoSynchronous Orbit – That is, inside the Terrestrial Service Volume (TSV) 8% Highly Elliptical Orbit Cislunar / Interplanetary • An additional 35%* of these space missions that will operate at higher altitudes will remain at or below GEO – That is, inside the GPS/GNSS Space Service Volume (SSV) Highly Elliptical Orbits**: • In summary, approximately 95% of projected Example: NASA MMS 4- worldwide space missions over the next 20 years will satellite constellation. -
Bob Farquhar
1 2 Created by Bob Farquhar For and dedicated to my grandchildren, their children, and all humanity. This is Copyright material 3 Table of Contents Preface 4 Conclusions 6 Gadget 8 Making Bombs Tick 15 ‘Little Boy’ 25 ‘Fat Man’ 40 Effectiveness 49 Death By Radiation 52 Crossroads 55 Atomic Bomb Targets 66 Acheson–Lilienthal Report & Baruch Plan 68 The Tests 71 Guinea Pigs 92 Atomic Animals 96 Downwinders 100 The H-Bomb 109 Nukes in Space 119 Going Underground 124 Leaks and Vents 132 Turning Swords Into Plowshares 135 Nuclear Detonations by Other Countries 147 Cessation of Testing 159 Building Bombs 161 Delivering Bombs 178 Strategic Bombers 181 Nuclear Capable Tactical Aircraft 188 Missiles and MIRV’s 193 Naval Delivery 211 Stand-Off & Cruise Missiles 219 U.S. Nuclear Arsenal 229 Enduring Stockpile 246 Nuclear Treaties 251 Duck and Cover 255 Let’s Nuke Des Moines! 265 Conclusion 270 Lest We Forget 274 The Beginning or The End? 280 Update: 7/1/12 Copyright © 2012 rbf 4 Preface 5 Hey there, I’m Ralph. That’s my dog Spot over there. Welcome to the not-so-wonderful world of nuclear weaponry. This book is a journey from 1945 when the first atomic bomb was detonated in the New Mexico desert to where we are today. It’s an interesting and sometimes bizarre journey. It can also be horribly frightening. Today, there are enough nuclear weapons to destroy the civilized world several times over. Over 23,000. “Enough to make the rubble bounce,” Winston Churchill said. The United States alone has over 10,000 warheads in what’s called the ‘enduring stockpile.’ In my time, we took care of things Mano-a-Mano. -
National Reconnaissance Office Review and Redaction Guide
NRO Approved for Release 16 Dec 2010 —Tep-nm.T7ymqtmthitmemf- (u) National Reconnaissance Office Review and Redaction Guide For Automatic Declassification Of 25-Year-Old Information Version 1.0 2008 Edition Approved: Scott F. Large Director DECL ON: 25x1, 20590201 DRV FROM: NRO Classification Guide 6.0, 20 May 2005 NRO Approved for Release 16 Dec 2010 (U) Table of Contents (U) Preface (U) Background 1 (U) General Methodology 2 (U) File Series Exemptions 4 (U) Continued Exemption from Declassification 4 1. (U) Reveal Information that Involves the Application of Intelligence Sources and Methods (25X1) 6 1.1 (U) Document Administration 7 1.2 (U) About the National Reconnaissance Program (NRP) 10 1.2.1 (U) Fact of Satellite Reconnaissance 10 1.2.2 (U) National Reconnaissance Program Information 12 1.2.3 (U) Organizational Relationships 16 1.2.3.1. (U) SAF/SS 16 1.2.3.2. (U) SAF/SP (Program A) 18 1.2.3.3. (U) CIA (Program B) 18 1.2.3.4. (U) Navy (Program C) 19 1.2.3.5. (U) CIA/Air Force (Program D) 19 1.2.3.6. (U) Defense Recon Support Program (DRSP/DSRP) 19 1.3 (U) Satellite Imagery (IMINT) Systems 21 1.3.1 (U) Imagery System Information 21 1.3.2 (U) Non-Operational IMINT Systems 25 1.3.3 (U) Current and Future IMINT Operational Systems 32 1.3.4 (U) Meteorological Forecasting 33 1.3.5 (U) IMINT System Ground Operations 34 1.4 (U) Signals Intelligence (SIGINT) Systems 36 1.4.1 (U) Signals Intelligence System Information 36 1.4.2 (U) Non-Operational SIGINT Systems 38 1.4.3 (U) Current and Future SIGINT Operational Systems 40 1.4.4 (U) SIGINT -
Records of Prime Contracts Awarded by the Military Services And
""" "II" n "'1"1""" National Archives and Records Adlninistration 8601 Adelphi Road College Park, Maryland 2fJUO-6tJOl List ofDcicumentation Military Prime CQntractFile. 1966-1975 Records of the Office ofthe Secretary ofDefense, Record Group 330 Accession Number: NN1-330-79-003 I. Basic Documentation 1. List ofDocumentation 1 2. tis! ofProourement Manuals (prepared 1995) 1 3. User Note 1 1 4. Abstract (prepared 1988) 1 5. rntroduction (prepared 1988) 2 6. NARA prepared record layout (April 200 1) :3 7. Valjdatl'on Statement (prepared 1988) 2 8. User Note 2 1 9. Agency prepared record layouts (prepared 1970) 3 10. UserNote3 1 11. DD Form 350J i 97 t (source for MPCf) 1 12. Agency description ofDD Form 350 . 1 13. Agency description of ><FlXS" data variable t II. Additional Documentation L NARA Magnetic Tape Record Inventory (January 19(2) 3 2. NARAMagnetic Tape Record lnllentoty (February 1972) 3 3. DcpaIimcnt ofDefense Publil,:aiions 4. MPCF Procurement Coding Manual. FY 1966 59 5. MPCF Procurement Codlng Manual. FY 1967 65 6. MPCF Procurement Coding Manual, FY 1968 68 7. MPCF Procurement Coding Manual, FY 1969 73 8. MPCF Procurement Coding Manual, FY 1970 78 9, MPCF Procurement Coding Manual, FY 1971 81 10. MPCf Procurement Coding Manual, FY 1972 89 11. MPCF Procurement Coding Manual, FY 1913 101 12. MPCF Procurement Coding Manual, FY 1974 79 13, MPCF Procurement Coding Manual, FY 1975 80 m. Processing Materials 1. AERie Verification Reports 2. NARA Sample Dumps (prepared 1988) 3. Agency SampleDurnps (1966-1975) William P. Fischer April 22. 2002 NARA Reference Copy Page # 1 Me. -
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. -
The 22 September 1979 Vela Incident—Part II: Radionu- Clide and Hydroacoustic Evidence for a Nuclear Explosion”
SCIENCE & GLOBAL SECURITY ,VOL.,NO.,– https://doi.org/./.. The September Vela Incident: The Detected Double-Flash Christopher M. Wrighta and Lars-Erik De Geer b aUNSW Canberra, School of Physical, Environmental and Mathematical Sciences, Research Group on Science & Security, The Australian Defence Force Academy, Canberra BC, Australia; b(Retired) FOI, Swedish Defense Research Agency, and the Preparatory Commission for the Comprehensive Nuclear-Test-Ban Treaty Organisation, Flädervägen , Upplands Väsby, Sweden ABSTRACT ARTICLE HISTORY On 22 September 1979 two optical sensors on U.S. satellite Vela Received March 6911 detected a double-flash of light that appeared characteristic Accepted October of an atmospheric nuclear explosion conducted over the south- ern Atlantic or Indian Ocean. It became known as the Vela Inci- dent, Event 747, or Alert 747. An anomaly between the amplitude of the two signals during the second pulse led a U.S. govern- ment expert panel established to assess the event to conclude in mid-1980 that a more likely explanation was the impact of a small meteoroid on the satellite, the debris from which reflected sunlight into the sensors’ field of view. No model was presented to support the contention, and a similar anomaly—known as background modulation—was a given for the second pulse of all confirmed explosions detected by Vela, though beginning later. Nonetheless, this event has remained the subject of intense debate. This article reviews the evidence and presents an updated analysis of the original Vela signal based on recently declassi- fied literature and on modern knowledge of interplanetary dust and hyper velocity impact. Given the geometry of the satellite, and that the bulk of the surface comprised solar panels, much of the debris from any collision would be carried away from the sensors’ field of view. -
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.