Gnss 101 – Era of Integration

Total Page:16

File Type:pdf, Size:1020Kb

Load more

2/4/2020 GNSS 101 – ERA OF INTEGRATION Wisconsin Society of Land Surveyors Conference Wisconsin Dells, 2020 1 PRESENTATION OUTLINE A general overview of GNSS today GPS USA • Physical Layer • Data Layer Global GLONASS RUSSIA Navigation • Application Layers Satellite BEIDOU • Integrations Systems CHINA • Other Interesting GNSS Applications GALILEO EU 2 BEFORE WE GET STARTED A few abbreviations to learn ANTCAL Antenna Calibration Format GDOP Geometric diluation of precision PPS Precision positioning service ANTEX Antenna Exchange Format GEO Geostationary Earth orbit PRN Pseudo-random noise ARP Antenna Reference Point GLONASS Global'naya Navigatsionnaya Sputnikova Sistema QZSS Quasi-Zenith Satellite System AS Anti-Spoofing GNSS Global Navigation Satellite System RAIM Receiver Autonomous Integrity Monitoring ATOM Adaptive Transmission of Optimized Messages GPS Global Positioning System RINEX Receiver Independent Exchange AUSPOS Australian Positioning Service GRS Geodetic Reference System RMS Root Mean Square BDS Beidou Satellite System HDOP Horizontal dilution of precision RTCA Radio Technical Commission for Aeronautics BINEX Binary Exchange Format IGS International GNSS Service RTCM Radio Technical Commission for Maritime Services BKG Bundesamt für Kartographie und Geodäsie IGSO Inclined geo-synchronous orbit RTK Real-time kinematic BPSK Binary phase-shift keying IOV In-orbit validation RTX Satellite and IP delivered corrections by Trimble CDMA Code division multiple access IRNSS Indian Regional Navigation Satellite System SA Selective Availability CEP Circular Error Probable ITRF International Terrestrial Reference Frame SAASM Selective Availability Anti-Spoofing Module CMR Compacted Measurement Record LLH Latitude Longitude Height SBAS Satellite-based augmentation system COM Center of Mass MEO Medium Earth orbit SDCM System for Differential Corrections and Monitoring CORS Continuously Operating Reference Station MGEX Multi-GNSS Experiment SINEX Solution Independent Exchange DGNSS Differential GNSS MSAS Multi-Function Satellite Augmentation System SPS Standard Positioning Service DGPS Differential GPS NAD North American Datum SSR State Space Representation DIP Direct Internet Protocol NGS National Geodetic Survey SVN Satellite vehicle number ECEF Earth-centered Earth-fixed NMEA National Marine Electronics Association TDOP Time dilution of precision EGNOS European Geostationary Navigation Overlay Service NRCAN National Resources Canada TEC Total electron count EPSG European Petroleum Survey Group NSAS Nigerian Satellite Augmentation System UHF Ultra-high frequency ESA European Space Agency NTRIP Network Transport of RTK via Internet Protocol UNAVCO University NAVSTAR Consortium ESRI Environmental Systems Research Institute OPUS Online Positioning User Service UTM Universal Transverse Mercator FDMA Frequency division multiple access PCV Phase Center Variation VDOP Vertical dilution of precision FOC Full operational capability PDOP Position dilution of precision VHF Very-high frequency GAGAN GPS-aided GEO Augmented Navigation PNT Positioning, navigation and timing WAAS Wide Area Augmentation System GATBP Geoscience Australia Test Bed Project PPP Precise point positioning WGS World Geodetic System 3 1 2/4/2020 BEFORE WE GET STARTED Abbreviations reorganized Positioning Space Messaging Systems Organizational Communications Mathematics Domain Component ANTCAL AS ATOM BDSBAS BKG BPSK CEP ANTEX SA CMR EGNOS CORS CDMA RMS ARP FOC RTX GAGAN EPSG DIP GDOP ECEF GEO DGNSS GLONASS ESA FDMA HDOP LLH IGSO DGPS GNSS ESRI NTRIP PDOP PCV MEO NMEA GPS GATBP RAIM TDOP PNT IOV PPP IRNSS IGS SAASM VDOP PRN PPS BINEX MSAS MGEX UHF COM SVN SPS RINEX NSAS NGS VHF GRS TEC SINEX QZSS NRCAN NAD SBAS OPUS UTM SDCM SSR WGS WAAS UNAVCO 4 PHYSICAL LAYER Physical properties of GNSS 5 PHYSICAL LAYER What is GNSS? • Ground Segment • Space Component •Users 6 2 2/4/2020 PHYSICAL LAYER GNSS Players • Global Services • SBAS Regional Services • GPS ~ 30 satellites • WAAS – USA ~ 3 satellites • GLONASS ~ 23 satellites • EGNOS – EU ~ 3 satellites • GALILEO ~ 22 satellites • BDSBAS – China ~ 3 satellites • BEIDOU ~ 35 satellites • MSAS – Japan ~ 2 satellites • Orbital Regional Services • GAGAN – India ~ 2 satellites • QZSS – Japan ~ 4 satellites • SDCM – Russia ~ 3 satellites • IRNSS – India ~ 8 satellites At least 138 navigation satellites in space 7 PHYSICAL LAYER GNSS Update • GPS III* • SV01 and SV02 in space • SV03, SV04 and SV05 awaiting launch • SV07, SV08 and SV09 are on the assembly line SV06 undergoing testing and validation in vacuum chamber 8 PHYSICAL LAYER GNSS Status • Beidou • 49 satellites | 24 are BDS III • Inter-satellite link capabilities • New generation rubidium and hydrogen maser clocks • 27 satellites in Medium Earth Orbit • 5 satellites in Geostationary Orbit • 3 satellites are inclined Geostationary Orbit 9 3 2/4/2020 PHYSICAL LAYER GNSS Status • Galileo designed as a 24 satellite constellation in 3 circular MEO orbits • Open Service signals currently available • Search and Rescue Service currently available • When fully operational, three additional services will be available • Public Regulated (Government) • Safety of Life • Commercial (Professional) 10 PHYSICAL LAYER GNSS Status • Glonass launched its most recent "M" class satellite December 11, 2019 from the Plesetsk cosmodrome. A January 2020 launch is also planned • Glonass and Beidou sign agreement to cooperate on the "Peaceful use of GNSS BDS and Glonass" • Glonass focuses on users by maintaining continuous services and stable performance 11 PHYSICAL LAYER Frequency Summary Frequencies in MegaHertz 1176.450 1207.140 1227.600 1246.000 1278.750 1561.098 1575.420 1602.000 GPS L5 L2 L1 GLO L2 L1 GAL E5a E5b E6 E1 BDS E5 E2 QZSS L5 L2 L1 SBAS L1 12 4 2/4/2020 PHYSICAL LAYER Radio Signal Characteristics GPS L5 GPS L2 GPS L1 13 PHYSICAL LAYER Mission Planning as a learning tool • Allows visualization of the physical layer • https://www.gnssplanningonline.com/#/maps 14 PHYSICAL LAYER Mission Planning as a learning tool • Allows visualization of the physical layer • Wisconsin Dells, Wisconsin | January 29th, 2020 @ 12:20 PM 15 5 2/4/2020 PHYSICAL LAYER Mission Planning as a learning tool • Allows visualization of the physical layer • Sentosa Island, Singapore | January 29th, 2020 @ 12:20 PM 16 PHYSICAL LAYER Expanding User Segment • GNSS assisted approaches for airplanes (LPV) is replacing the single-legged ILS landing method • Autonomy explosion – planes, trains, automobiles, drone deliveries, automated tasks, safety of life • Accurate positioning via GNSS is now an assumption worldwide – global infrastructure 17 PHYSICAL LAYER GNSS Receivers and Satellite Tracking Technology • GPS and Glonass are not perceived to be good enough - BDS and Galileo are expected • Combined signals from multiple constellations and frequencies are called X-Signals • The International GNSS Service (IGS) is conducting a pilot project called MGEX (Multi-GNSS Experiment) to study the X-Signals 18 6 2/4/2020 PHYSICAL LAYER GNSS antennas vary Magellan 111406 L1 Offset – 6.01 cm (2.37”) • PCV = Phase Center Variation • ARP = Antenna Reference Point Spectra Epoch 35 L1 Offset – 9.97 cm (3.93”) 90° 90° Phase Center Phase Center 0° 0° Spectra SP60 Antenna Reference Point Antenna Reference Point L1 Offset – 5.05 cm (1.99”) Phase Meter Phase Meter +π +π 0.f λ 0.f λ -π -π Elevation Elevation Ashtech 111661 (Imaginary) Ideal Antenna Real Antenna Pattern L1 Offset – 5.72 cm (2.25”) 19 PHYSICAL LAYER Leap Seconds – IERS • Precise Time is TAI (International Atomic Time) • GNSS uses TAI • Imprecise Time is known as UT1 • Varies due to long-term slowdown in the Earth's rotation • Normal clocks use some offset of UTC time which is referenced to TAI • Leap seconds are announced by the IERS to align UT1 and UTC • The GPS epoch began at midnight, January 6, 1980 • At that time, TAI – UTC = -19 seconds • Today, TAI – UTC = -37 seconds • Thus, GPS time is offset from UTC by 18 seconds ((TAI – UTC) + 19) 1972 1980 1990 2000 2010 2020 20 PHYSICAL LAYER GPS Week Number Roll-Over (WNRO) • The GPS epoch began at midnight on the cusp between January 5 & 6, 1980 • GPS uses a 10-binary counter to represent the week number • Every 19.7 years, this counter reaches its limit and rolls back to zero • April 6, 2019 was the second WNRO event in the GPS epoch 21 7 2/4/2020 PHYSICAL LAYER Sky Occlusion – GNSS Needs Sky • At least 4 visible satellites are required to compute a 3D position 22 PHYSICAL LAYER Clock Technologies and Timing • NASA Deep Space Clocks • The first GPS-like clock designed for deep space • Will allow spacecraft to navigate themselves versus relying on directions from Earth • The mercury-ion clock loses one second every 10 million years https://m.phys.org/news/2019-08-nasa-deep-space-atomic-clock.html 23 PHYSICAL LAYER Spoofing and Jamming • "Protect yourself from Interference with the Spirent GSS900 Series" • "U.S. officials warn of Iranian threats to commercial vessels including GPS interference" * • "Modeling jammed and spoofed signals to protect critical systems" – Orolia Defense Systems • Jamming and spoofing are becoming more prevalent, not just for the military but also for consumers – Cast Navigation, LLC • Protecting PNT | Anti-jam receivers protect data, mitigate navigation warfare threats – GPSWorld cover story, December 2019 • As the threat of jamming and spoofing increases, the receiver industry will have to develop counter measures and mitigation strategies – Cyrelle Gernot, Syntony GNSS *https://nypost.com/2019/08/07/us-officials-warn-of-iranian-threats-to-commercial-vessels-including-gps-interference/
Recommended publications
  • Robotic Forest Harvesting Process Using GNSS

    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
  • Gnss and Avionics Simulation for Rohde & Schwarz Signal Generators

    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

    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).
  • Leica Viva Series White Paper Beidou Integration

    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.
  • Part V: the Global Positioning System ______

    Part V: the Global Positioning System ______

    PART V: THE GLOBAL POSITIONING SYSTEM ______________________________________________________________________________ 5.1 Background The Global Positioning System (GPS) is a satellite based, passive, three dimensional navigational system operated and maintained by the Department of Defense (DOD) having the primary purpose of supporting tactical and strategic military operations. Like many systems initially designed for military purposes, GPS has been found to be an indispensable tool for many civilian applications, not the least of which are surveying and mapping uses. There are currently three general modes that GPS users have adopted: absolute, differential and relative. Absolute GPS can best be described by a single user occupying a single point with a single receiver. Typically a lower grade receiver using only the coarse acquisition code generated by the satellites is used and errors can approach the 100m range. While absolute GPS will not support typical MDOT survey requirements it may be very useful in reconnaissance work. Differential GPS or DGPS employs a base receiver transmitting differential corrections to a roving receiver. It, too, only makes use of the coarse acquisition code. Accuracies are typically in the sub- meter range. DGPS may be of use in certain mapping applications such as topographic or hydrographic surveys. DGPS should not be confused with Real Time Kinematic or RTK GPS surveying. Relative GPS surveying employs multiple receivers simultaneously observing multiple points and makes use of carrier phase measurements. Relative positioning is less concerned with the absolute positions of the occupied points than with the relative vector (dX, dY, dZ) between them. 5.2 GPS Segments The Global Positioning System is made of three segments: the Space Segment, the Control Segment and the User Segment.
  • Reference Systems for Surveying and Mapping Lecture Notes

    Reference Systems for Surveying and Mapping Lecture Notes

    Delft University of Technology Reference Systems for Surveying and Mapping Lecture notes Hans van der Marel ii The front cover shows the NAP (Amsterdam Ordnance Datum) ”datum point” at the Stopera, Amsterdam (picture M.M.Minderhoud, Wikipedia/Michiel1972). H. van der Marel Lecture notes on Reference Systems for Surveying and Mapping: CTB3310 Surveying and Mapping CTB3425 Monitoring and Stability of Dikes and Embankments CIE4606 Geodesy and Remote Sensing CIE4614 Land Surveying and Civil Infrastructure February 2020 Publisher: Faculty of Civil Engineering and Geosciences Delft University of Technology P.O. Box 5048 Stevinweg 1 2628 CN Delft The Netherlands Copyright ©2014­2020 by H. van der Marel The content in these lecture notes, except for material credited to third parties, is licensed under a Creative Commons Attributions­NonCommercial­SharedAlike 4.0 International License (CC BY­NC­SA). Third party material is shared under its own license and attribution. The text has been type set using the MikTex 2.9 implementation of LATEX. Graphs and diagrams were produced, if not mentioned otherwise, with Matlab and Inkscape. Preface This reader on reference systems for surveying and mapping has been initially compiled for the course Surveying and Mapping (CTB3310) in the 3rd year of the BSc­program for Civil Engineering. The reader is aimed at students at the end of their BSc program or at the start of their MSc program, and is used in several courses at Delft University of Technology. With the advent of the Global Positioning System (GPS) technology in mobile (smart) phones and other navigational devices almost anyone, anywhere on Earth, and at any time, can determine a three–dimensional position accurate to a few meters.
  • (GNSS) Based Augmentation System Low Latitude Threat Model

    (GNSS) Based Augmentation System Low Latitude Threat Model

    Effects Of Southern Hemisphere Ionospheric Activity On Global Navigation Satellite Systems (GNSS) Based Augmentation System Low Latitude Threat Model December 2014 Submitted to: Servicos de Defesa e Technologia de Processos (SDTP) And The U.S. Trade and Development Agency 1000 Wilson Boulevard, Suite 1600, Arlington, VA 22209-3901 Submitted by Mirus Technology LLC Prepared by the Mirus Technology, LLC (with Contributions from FAA, Stanford University, INPE, ICEA, Boston College, NAVTEC, and KAIST) Principal Investigator: Dr. Navin Mathur Executive Summary Ground-based Augmentation System (GBAS) augments the Global Positioning System (GPS) by increasing the accuracy to an appropriately equipped user. In addition to enhancing the accuracy of GPS derived accuracy, a GBAS provides the necessary integrity of accuracy (to a level defined by International Civil Aviation Organization, ICAO) required for a system that supports landing of an aircraft at an airport where GBAS is available. In addition, a GBAS system is designed to ensure the process of integrity and required continuity of GBAS operations and associated operational availability. The integrity of GBAS is threatened by several internal or external factors that can be broadly classified into three categories namely; Space Vehicle (SV) induced errors, environmental induced errors, and internally generated errors. Over the last decade, the US Federal Aviation Administration (FAA) has systematically defined, classified, characterized, and addressed each of the error sources in those categories that apply within CONUS. These efforts culminated in approval of several GBAS Category-I approaches within CONUS at various locations (such as Newark, Houston, etc.). Through the process of GBAS development for CONUS, the aviation and scientific communities realized that the Ionosphere is one of the key contributors to GBAS integrity threat.
  • World Geodetic System 1984

    World Geodetic System 1984

    World Geodetic System 1984 Responsible Organization: National Geospatial-Intelligence Agency Abbreviated Frame Name: WGS 84 Associated TRS: WGS 84 Coverage of Frame: Global Type of Frame: 3-Dimensional Last Version: WGS 84 (G1674) Reference Epoch: 2005.0 Brief Description: WGS 84 is an Earth-centered, Earth-fixed terrestrial reference system and geodetic datum. WGS 84 is based on a consistent set of constants and model parameters that describe the Earth's size, shape, and gravity and geomagnetic fields. WGS 84 is the standard U.S. Department of Defense definition of a global reference system for geospatial information and is the reference system for the Global Positioning System (GPS). It is compatible with the International Terrestrial Reference System (ITRS). Definition of Frame • Origin: Earth’s center of mass being defined for the whole Earth including oceans and atmosphere • Axes: o Z-Axis = The direction of the IERS Reference Pole (IRP). This direction corresponds to the direction of the BIH Conventional Terrestrial Pole (CTP) (epoch 1984.0) with an uncertainty of 0.005″ o X-Axis = Intersection of the IERS Reference Meridian (IRM) and the plane passing through the origin and normal to the Z-axis. The IRM is coincident with the BIH Zero Meridian (epoch 1984.0) with an uncertainty of 0.005″ o Y-Axis = Completes a right-handed, Earth-Centered Earth-Fixed (ECEF) orthogonal coordinate system • Scale: Its scale is that of the local Earth frame, in the meaning of a relativistic theory of gravitation. Aligns with ITRS • Orientation: Given by the Bureau International de l’Heure (BIH) orientation of 1984.0 • Time Evolution: Its time evolution in orientation will create no residual global rotation with regards to the crust Coordinate System: Cartesian Coordinates (X, Y, Z).
  • Terms for Coordinates Azimuth Angle Measured from North Clockwise

    Terms for Coordinates Azimuth Angle Measured from North Clockwise

    Terms for Coordinates Azimuth Angle measured from north clockwise. North is 0 degrees, east is 90 degrees etc. Three common forms of azimuth exist: true azimuth, magnetic azimuth, and grid azimuth. Angular Coordinates Latitude, Longitude, and Height can specify a location. This is called an angular frame. To obtain angular coordinates in a spherical earth system, only the radius is needed. This is needed only for the height. For an ellipsoidal earth the parameters of the ellipsoid must be specified to convert height and latitude. (To obtain geographic, or mean sea level, height the geoid is needed. Cartesian Coordinates Standard x-y-z coordinates. Three axes perpendicular to each other meet at the origin, or center of the coordinate system. The coordinates of a point are the projection of the location on these axes. Circle, Great A great circle is a circle on the earth whose center is the center of the earth. Alternately, it is the intersection of a plane and a sphere when the center of the sphere is on the plane. Shortest distance between two points on the earth in spherical model is a great circle. Meridians are great circles. Circle, Small A small circle is a circle on the earth whose center is not the center of the earth. Alternately, it is the intersection of a plane and a sphere when the center of the sphere is not on the plane. Parallels of latitude are small circles. Coordinate Frame In general this refers to a Cartesian system of coordinates. The location of the origin and the orientation of the axes with respect to the real earth are also included.
  • ABAS), Satellite-Based Augmentation System (SBAS), Or Ground-Based Augmentation System (GBAS

    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.
  • GNSS Applications for Agricultural Practices by Guy Blanchard Ikokou, University of Cape Town

    GNSS Applications for Agricultural Practices by Guy Blanchard Ikokou, University of Cape Town

    Application technical GNSS applications for agricultural practices by Guy Blanchard Ikokou, University of Cape Town Global positioning systems are relatively new technologies when it comes to applications in agriculture. Applications in tractor guidance, variable rate supply of chemical inputs and field monitoring of crop yield were recently tested using GPS. This article studies the basic concepts of GPS as they apply to agricultural production and provides a detailed analysis of the recent developments in this area with a focus on functionality and efficiency. ver the past 30 years satellites are maintained within 24 information worldwide and provides agricultural machinery has circular orbital planes inclined 55° with support to military, civil and commercial Oreached high technical respect to the equator plane [1]. The applications. standards in order to improve system currently provides two user A total of 24 GLONASS satellites are agriculture production. Precision services: (i) the Standard Positioning actually operational with the latest agriculture or satellite agriculture is a Service (SPS), open to civil users is satellite placed into space on 26 April highly effective farming management available for civil applications such as 2013 with an inclination of 64,8° method that focuses on intra-field agricultural practice and farming, and and an altitude of 19 100 km [3]. variation in order to optimise (ii) the Precision Positioning Service, The system broadcasts two types of agriculture returns while conserving restricted to authorised users such navigation signals: (i) the standard environmental resources. It relies on as the United States military and accuracy signal mainly available to civil new technologies such as the Global their allies.
  • High-Precision GNSS: Methods, Open Problems and Geoscience Applications”

    High-Precision GNSS: Methods, Open Problems and Geoscience Applications”

    remote sensing Editorial Editorial for the Special Issue: “High-Precision GNSS: Methods, Open Problems and Geoscience Applications” Xingxing Li 1,*, Jacek Paziewski 2 and Mattia Crespi 3 1 School of Geodesy and Geomatics, Wuhan University, 129 Luoyu Road, Wuhan 430079, China 2 The Faculty of Geodesy, Geospatial and Civil Engineering Institute of Geodesy, University of Warmia and Mazury in Olsztyn (UWM), 10-719 Olsztyn, Poland; [email protected] 3 Geodesy and Geomatics Division—DICEA, Sapienza University of Rome, 00184 Rome, Italy; [email protected] * Correspondence: [email protected] Received: 17 April 2020; Accepted: 18 April 2020; Published: 18 May 2020 Keywords: GNSS; GPS; GLONASS; Galileo; BDS; precise point positioning; relative positioning; orbit determination; ionosphere sounding; troposphere sounding; geoscience applications; high-rate positioning; GNSS for geodynamics In the past two decades, the high-precision Global Positioning System (GPS) has significantly increased the range of geoscience applications and their precision. Currently, it is one of two fully operational Global Navigation Satellite Systems (GNSS), and two more are in the implementation stage. The new European Galileo and Chinese BeiDou Navigation Satellite System (BDS) already provide usable signals, and both GPS and GLONASS are currently undergoing significant modernization, which adds more capacity, more signals, better accuracy, and interoperability, etc. Meanwhile, there has been significant technological development in GNSS equipment (in some cases, even at low-cost), which is now able to collect measurements at much higher rates (up to 100 Hz), thus presenting new possibilities. On the one hand, the new developments in GNSS offer a broad range of new applications for solid and fluid Earth investigations, in both post-processing and real-time; on the other, this results in new problems and challenges in data processing that increase the need for GNSS research.