The Global Positioning System Geodesy Odyssey
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Navigation and the Global Positioning System (GPS): the Global Positioning System
Navigation and the Global Positioning System (GPS): The Global Positioning System: Few changes of great importance to economics and safety have had more immediate impact and less fanfare than GPS. • GPS has quietly changed everything about how we locate objects and people on the Earth. • GPS is (almost) the final step toward solving one of the great conundrums of human history. Where the heck are we, anyway? In the Beginning……. • To understand what GPS has meant to navigation it is necessary to go back to the beginning. • A quick look at a ‘precision’ map of the world in the 18th century tells one a lot about how accurate our navigation was. Tools of the Trade: • Navigations early tools could only crudely estimate location. • A Sextant (or equivalent) can measure the elevation of something above the horizon. This gives your Latitude. • The Compass could provide you with a measurement of your direction, which combined with distance could tell you Longitude. • For distance…well counting steps (or wheel rotations) was the thing. An Early Triumph: • Using just his feet and a shadow, Eratosthenes determined the diameter of the Earth. • In doing so, he used the last and most elusive of our navigational tools. Time Plenty of Weaknesses: The early tools had many levels of uncertainty that were cumulative in producing poor maps of the world. • Step or wheel rotation counting has an obvious built-in uncertainty. • The Sextant gives latitude, but also requires knowledge of the Earth’s radius to determine the distance between locations. • The compass relies on the assumption that the North Magnetic pole is coincident with North Rotational pole (it’s not!) and that it is a perfect dipole (nope…). -
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 -
Geodetic Surveying, Earth Modeling, and the New Geodetic Datum of 2022
Geodetic Surveying, Earth Modeling, and the New Geodetic Datum of 2022 PDH330 3 Hours PDH Academy PO Box 449 Pewaukee, WI 53072 (888) 564-9098 www.pdhacademy.com [email protected] Geodetic Surveying Final Exam 1. Who established the U.S. Coast and Geodetic Survey? A) Thomas Jefferson B) Benjamin Franklin C) George Washington D) Abraham Lincoln 2. Flattening is calculated from what? A) Equipotential surface B) Geoid C) Earth’s circumference D) The semi major and Semi minor axis 3. A Reference Frame is based off how many dimensions? A) two B) one C) four D) three 4. Who published “A Treatise on Fluxions”? A) Einstein B) MacLaurin C) Newton D) DaVinci 5. The interior angles of an equilateral planar triangle adds up to how many degrees? A) 360 B) 270 C) 180 D) 90 6. What group started xDeflec? A) NGS B) CGS C) DoD D) ITRF 7. When will NSRS adopt the new time-based system? A) 2022 B) 2020 C) Unknown due to delays D) 2021 8. Did the State Plane Coordinate System of 1927 have more zones than the State Plane Coordinate System of 1983? A) No B) Yes C) They had the same D) The State Plane Coordinate System of 1927 did not have zones 9. A new element to the State Plane Coordinate System of 2022 is: A) The addition of Low Distortion Projections B) Adjoining tectonic plates C) Airborne gravity collection D) None of the above 10. The model GRAV-D (Gravity for Redefinition of the American Vertical Datum) created will replace _____________ and constitute the new vertical height system of the United States A) Decimal degrees B) Minutes C) NAVD 88 D) All of the above Introduction to Geodetic Surveying The early curiosity of man has driven itself to learn more about the vastness of our planet and the universe. -
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. -
Geodesy in the 21St Century
Eos, Vol. 90, No. 18, 5 May 2009 VOLUME 90 NUMBER 18 5 MAY 2009 EOS, TRANSACTIONS, AMERICAN GEOPHYSICAL UNION PAGES 153–164 geophysical discoveries, the basic under- Geodesy in the 21st Century standing of earthquake mechanics known as the “elastic rebound theory” [Reid, 1910], PAGES 153–155 Geodesy and the Space Era was established by analyzing geodetic mea- surements before and after the 1906 San From flat Earth, to round Earth, to a rough Geodesy, like many scientific fields, is Francisco earthquakes. and oblate Earth, people’s understanding of technology driven. Over the centuries, it In 1957, the Soviet Union launched the the shape of our planet and its landscapes has developed as an engineering discipline artificial satellite Sputnik, ushering the world has changed dramatically over the course because of its practical applications. By the into the space era. During the first 5 decades of history. These advances in geodesy— early 1900s, scientists and cartographers of the space era, space geodetic technolo- the study of Earth’s size, shape, orientation, began to use triangulation and leveling mea- gies developed rapidly. The idea behind and gravitational field, and the variations surements to record surface deformation space geodetic measurements is simple: Dis- of these quantities over time—developed associated with earthquakes and volcanoes. tance or phase measurements conducted because of humans’ curiosity about the For example, one of the most important between Earth’s surface and objects in Earth and because of geodesy’s application to navigation, surveying, and mapping, all of which were very practical areas that ben- efited society. -
NASA Space Geodesy Program: Catalogue of Site Information
NASA Technical Memorandum 4482 NASA Space Geodesy Program: Catalogue of Site Information M. A. Bryant and C. E. Noll March 1993 N93-2137_ (NASA-TM-4482) NASA SPACE GEODESY PROGRAM: CATALOGUE OF SITE INFORMATION (NASA) 688 p Unclas Hl146 0154175 v ,,_r NASA Technical Memorandum 4482 NASA Space Geodesy Program: Catalogue of Site Information M. A. Bryant McDonnell Douglas A erospace Seabro'ok, Maryland C. E. Noll NASA Goddard Space Flight Center Greenbelt, Maryland National Aeronautics and Space Administration Goddard Space Flight Center Greenbelt, Maryland 20771 1993 . _= _qum_ Table of Contents Introduction .......................................... ..... ix Map of Geodetic Sites - Global ................................... xi Map of Geodetic Sites - Europe .................................. xii Map of Geodetic Sites - Japan .................................. xiii Map of Geodetic Sites - North America ............................. xiv Map of Geodetic Sites - Western United States ......................... xv Table of Sites Listed by Monument Number .......................... xvi Acronyms ............................................... xxvi Subscription Application ..................................... xxxii Site Information ............................................. Site Name Site Number Page # ALGONQUIN 67 ............................ 1 AMERICAN SAMOA 91 ............................ 5 ANKARA 678 ............................ 9 AREQUIPA 98 ............................ 10 ASKITES 674 ........................... , 15 AUSTIN 400 ........................... -
State Plane Coordinate System
Wisconsin Coordinate Reference Systems Second Edition Published 2009 by the State Cartographer’s Office Wisconsin Coordinate Reference Systems Second Edition Wisconsin State Cartographer’s Offi ce — Madison, WI Copyright © 2015 Board of Regents of the University of Wisconsin System About the State Cartographer’s Offi ce Operating from the University of Wisconsin-Madison campus since 1974, the State Cartographer’s Offi ce (SCO) provides direct assistance to the state’s professional mapping, surveying, and GIS/ LIS communities through print and Web publications, presentations, and educational workshops. Our staff work closely with regional and national professional organizations on a wide range of initia- tives that promote and support geospatial information technologies and standards. Additionally, we serve as liaisons between the many private and public organizations that produce geospatial data in Wisconsin. State Cartographer’s Offi ce 384 Science Hall 550 North Park St. Madison, WI 53706 E-mail: [email protected] Phone: (608) 262-3065 Web: www.sco.wisc.edu Disclaimer The contents of the Wisconsin Coordinate Reference Systems (2nd edition) handbook are made available by the Wisconsin State Cartographer’s offi ce at the University of Wisconsin-Madison (Uni- versity) for the convenience of the reader. This handbook is provided on an “as is” basis without any warranties of any kind. While every possible effort has been made to ensure the accuracy of information contained in this handbook, the University assumes no responsibilities for any damages or other liability whatsoever (including any consequential damages) resulting from your selection or use of the contents provided in this handbook. Revisions Wisconsin Coordinate Reference Systems (2nd edition) is a digital publication, and as such, we occasionally make minor revisions to this document. -
Solar Radiation Pressure Models for Beidou-3 I2-S Satellite: Comparison and Augmentation
remote sensing Article Solar Radiation Pressure Models for BeiDou-3 I2-S Satellite: Comparison and Augmentation Chen Wang 1, Jing Guo 1,2 ID , Qile Zhao 1,3,* and Jingnan Liu 1,3 1 GNSS Research Center, Wuhan University, 129 Luoyu Road, Wuhan 430079, China; [email protected] (C.W.); [email protected] (J.G.); [email protected] (J.L.) 2 School of Engineering, Newcastle University, Newcastle upon Tyne NE1 7RU, UK 3 Collaborative Innovation Center of Geospatial Technology, Wuhan University, 129 Luoyu Road, Wuhan 430079, China * Correspondence: [email protected]; Tel.: +86-027-6877-7227 Received: 22 December 2017; Accepted: 15 January 2018; Published: 16 January 2018 Abstract: As one of the most essential modeling aspects for precise orbit determination, solar radiation pressure (SRP) is the largest non-gravitational force acting on a navigation satellite. This study focuses on SRP modeling of the BeiDou-3 experimental satellite I2-S (PRN C32), for which an obvious modeling deficiency that is related to SRP was formerly identified. The satellite laser ranging (SLR) validation demonstrated that the orbit of BeiDou-3 I2-S determined with empirical 5-parameter Extended CODE (Center for Orbit Determination in Europe) Orbit Model (ECOM1) has the sun elongation angle (# angle) dependent systematic error, as well as a bias of approximately −16.9 cm. Similar performance has been identified for European Galileo and Japanese QZSS Michibiki satellite as well, and can be reduced with the extended ECOM model (ECOM2), or by using the a priori SRP model to augment ECOM1. In this study, the performances of the widely used SRP models for GNSS (Global Navigation Satellite System) satellites, i.e., ECOM1, ECOM2, and adjustable box-wing model have been compared and analyzed for BeiDou-3 I2-S satellite. -
Position Errors Caused by GPS Height of Instrument Blunders Thomas H
University of Connecticut OpenCommons@UConn Department of Natural Resources and the Thomas H. Meyer's Peer-reviewed Articles Environment July 2005 Position Errors Caused by GPS Height of Instrument Blunders Thomas H. Meyer University of Connecticut, [email protected] April Hiscox University of Connecticut Follow this and additional works at: https://opencommons.uconn.edu/thmeyer_articles Recommended Citation Meyer, Thomas H. and Hiscox, April, "Position Errors Caused by GPS Height of Instrument Blunders" (2005). Thomas H. Meyer's Peer-reviewed Articles. 4. https://opencommons.uconn.edu/thmeyer_articles/4 Survey Review, 38, 298 (October 2005) SURVEY REVIEW No.298 October 2005 Vol.38 CONTENTS (part) Position errors caused by GPS height of instrument blunders 262 T H Meyer and A L Hiscox This paper was published in the October 2005 issue of the UK journal, SURVEY REVIEW. This document is the copyright of CASLE. Requests to make copies should be made to the Editor, see www.surveyreview.org for contact details. The Commonwealth Association of Surveying and Land Economy does not necessarily endorse any opinions or recommendations made in an article, review, or extract contained in this Review nor do they necessarily represent CASLE policy CASLE 2005 261 Survey Review, 38, 298 (October 2005 POSITION ERRORS CAUSED BY GPS HEIGHT OF INSTRUMENT BLUNDERS POSITION ERRORS CAUSED BY GPS HEIGHT OF INSTRUMENT BLUNDERS T. H. Meyer and A. L. Hiscox Department of Natural Resources Management and Engineering University of Connecticut ABSTRACT Height of instrument (HI) blunders in GPS measurements cause position errors. These errors can be pure vertical, pure horizontal, or a mixture of both. -
The Global Positioning System the Global Positioning System
The Global Positioning System The Global Positioning System 1. System Overview 2. Biases and Errors 3. Signal Structure and Observables 4. Absolute v. Relative Positioning 5. GPS Field Procedures 6. Ellipsoids, Datums and Coordinate Systems 7. Mission Planning I. System Overview ! GPS is a passive navigation and positioning system available worldwide 24 hours a day in all weather conditions developed and maintained by the Department of Defense ! The Global Positioning System consists of three segments: ! Space Segment ! Control Segment ! User Segment Space Segment Space Segment ! The current GPS constellation consists of 29 Block II/IIA/IIR/IIR-M satellites. The first Block II satellite was launched in February 1989. Control Segment User Segment How it Works II. Biases and Errors Biases GPS Error Sources • Satellite Dependent ? – Orbit representation ? Satellite Orbit Error Satellite Clock Error including 12 biases ? 9 3 Selective Availability 6 – Satellite clock model biases Ionospheric refraction • Station Dependent L2 L1 – Receiver clock biases – Station Coordinates Tropospheric Delay • Observation Multi- pathing Dependent – Ionospheric delay 12 9 3 – Tropospheric delay Receiver Clock Error 6 1000 – Carrier phase ambiguity Satellite Biases ! The satellite is not where the GPS broadcast message says it is. ! The satellite clocks are not perfectly synchronized with GPS time. Station Biases ! Receiver clock time differs from satellite clock time. ! Uncertainties in the coordinates of the station. ! Time transfer and orbital tracking. Observation Dependent Biases ! Those associated with signal propagation Errors ! Residual Biases ! Cycle Slips ! Multipath ! Antenna Phase Center Movement ! Random Observation Error Errors ! In addition to biases factors effecting position and/or time determined by GPS is dependant upon: ! The geometric strength of the satellite configuration being observed (DOP). -
Download/Pdf/Ps-Is-Qzss/Ps-Qzss-001.Pdf (Accessed on 15 June 2021)
remote sensing Article Design and Performance Analysis of BDS-3 Integrity Concept Cheng Liu 1, Yueling Cao 2, Gong Zhang 3, Weiguang Gao 1,*, Ying Chen 1, Jun Lu 1, Chonghua Liu 4, Haitao Zhao 4 and Fang Li 5 1 Beijing Institute of Tracking and Telecommunication Technology, Beijing 100094, China; [email protected] (C.L.); [email protected] (Y.C.); [email protected] (J.L.) 2 Shanghai Astronomical Observatory, Chinese Academy of Sciences, Shanghai 200030, China; [email protected] 3 Institute of Telecommunication and Navigation, CAST, Beijing 100094, China; [email protected] 4 Beijing Institute of Spacecraft System Engineering, Beijing 100094, China; [email protected] (C.L.); [email protected] (H.Z.) 5 National Astronomical Observatories, Chinese Academy of Sciences, Beijing 100094, China; [email protected] * Correspondence: [email protected] Abstract: Compared to the BeiDou regional navigation satellite system (BDS-2), the BeiDou global navigation satellite system (BDS-3) carried out a brand new integrity concept design and construction work, which defines and achieves the integrity functions for major civil open services (OS) signals such as B1C, B2a, and B1I. The integrity definition and calculation method of BDS-3 are introduced. The fault tree model for satellite signal-in-space (SIS) is used, to decompose and obtain the integrity risk bottom events. In response to the weakness in the space and ground segments of the system, a variety of integrity monitoring measures have been taken. On this basis, the design values for the new B1C/B2a signal and the original B1I signal are proposed, which are 0.9 × 10−5 and 0.8 × 10−5, respectively. -
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 .................................................................................................................