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50 Satellite Formation-Flying and Rendezvous
Parkinson, et al.: Global Positioning System: Theory and Applications — Chap. 50 — 2017/11/26 — 19:03 — page 1 1 50 Satellite Formation-Flying and Rendezvous Simone D’Amico1) and J. Russell Carpenter2) 50.1 Introduction to Relative Navigation GNSS has come to play an increasingly important role in satellite formation-flying and rendezvous applications. In the last decades, the use of GNSS measurements has provided the primary method for determining the relative position of cooperative satellites in low Earth orbit. More recently, GNSS data have been successfully used to perform formation-flying in highly elliptical orbits with apogees at tens of Earth radii well above the GNSS constellations. Current research aims at dis- tributed precise relative navigation between tens of swarming nano- and micro-satellites based on GNSS. Similar to terrestrial applications, GNSS relative navigation benefits from a high level of common error cancellation. Furthermore, the integer nature of carrier phase ambiguities can be exploited in carrier phase differential GNSS (CDGNSS). Both aspects enable a substantially higher accuracy in the estimation of the relative motion than can be achieved in single-spacecraft navigation. Following historical remarks and an overview of the state-of-the-art, this chapter addresses the technology and main techniques used for spaceborne relative navigation both for real-time and offline applications. Flight results from missions such as the Space Shuttle, PRISMA, TanDEM-X, and MMS are pre- sented to demonstrate the versatility and broad range of applicability of GNSS relative navigation, from precise baseline determination on-ground (mm-level accuracy), to coarse real-time estimation on-board (m- to cm-level accuracy). -
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 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 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). -
Galileo FOC-M7 SAT 19-20-21-22
LAUNCH KIT December 2017 VA240 Galileo FOC-M7 SAT 19-20-21-22 VA240 Galileo FOC-M7 SAT 19-20-21-22 ARIANESPACE’S SECOND ARIANE 5 LAUNCH FOR THE GALILEO CONSTELLATION AND EUROPE For its 11th launch of the year, and the sixth Ariane 5 liftoff from the Guiana Space Center (CSG) in French Guiana during 2017, Arianespace will orbit four more satellites for the Galileo constellation. This mission is being performed on behalf of the European Commission under a contract with the European Space Agency (ESA). For the second time, an Ariane 5 ES version will be used to orbit satellites in Europe’s own satellite navigation system. At the completion of this flight, designated Flight VA240 in Arianespace’s launcher family numbering system, 22 Galileo spacecraft will have been launched by Arianespace. Arianespace is proud to deploy its entire family of launch vehicles to address Europe’s needs and guarantee its independent access to space. Galileo, an iconic European program Galileo is Europe’s own global navigation satellite system. Under civilian control, Galileo offers guaranteed high-precision positioning around the world. Its initial services began in December CONTENTS 2016, allowing users equipped with Galileo-enabled devices to combine Galileo and GPS data for better positioning accuracy. The complete Galileo constellation will comprise a total of 24 operational satellites (along with > THE LAUNCH spares); 18 of these satellites already have been orbited by Arianespace. ESA transferred formal responsibility for oversight of Galileo in-orbit operations to the GSA VA240 mission (European GNSS Agency) in July 2017. Page 3 Therefore, as of this launch, the GSA will be in charge of the operation of the Galileo satellite Galileo FOC-M7 satellites navigation systems on behalf of the European Union. -
D5.2: Process Map for Autonomous Navigation
Grant Agreement number: 314286 Project acronym: MUNIN Project title: Maritime Unmanned Navigation through Intelligence in Networks Funding Scheme: SST.2012.5.2‐5: E‐guided vessels: the 'autonomous' ship D5.2: Process map for autonomous navigation Due date of deliverable: 2013‐07‐31 Actual submission date: Start date of project: 2012‐09‐01 Project Duration: 36 months Lead partner for deliverable: Fraunhofer CML Distribution date: 2013‐09‐27 Document revision: 1.0 Project co‐funded by the European Commission within the Seventh Framework Programme (2007‐2013) Dissemination Level PU Public Public PP Restricted to other programme participants (including the Commission Services) RE Restricted to a group specified by the consortium (including the Commission Services) CO Confidential, only for members of the consortium (including the Commission Services) MUNIN – FP7 GA‐No 314286 D5.2 ‐ Print date: 14/01/07 Document summary information Deliverable D5.2: Process map for autonomous navigation Classification PU (public) Initials Author Organization Role WB Wilko Bruhn CML Editor HCB Hans‐Christoph Burmeister CML Editor LW Laura Walther CML Contributor JM Jonas Moræus APT Contributor ML Matt Long APT Contributor MS Michèle Schaub HSW Contributor EF Enrico Fentzahn MsoftContributor Rev. Who Date Comment 0.1 WB 2013‐08‐01 First draft 0.2 ØJR 2013‐08‐12 Partner review 0.3 AV 2013‐08‐13 Partner review 0.4 BS 2013‐08‐13 Partner review 0.5 WB 2013‐08‐30 Second draft after comments 1.0 HCB 2013‐08‐27 Formating Internal review needed: [ X ] yes [ ] no Initials Reviewer Approved Not approved FS Fariborz Safari X AV Ari Vésteinsson X Disclaimer The content of the publication herein is the sole responsibility of the publishers and it does not necessarily represent the views expressed by the European Commission or its services. -
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. -
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. -
Global Maritime Distress and Safety System (GMDSS) Handbook 2018 I CONTENTS
FOREWORD This handbook has been produced by the Australian Maritime Safety Authority (AMSA), and is intended for use on ships that are: • compulsorily equipped with GMDSS radiocommunication installations in accordance with the requirements of the International Convention for the Safety of Life at Sea Convention 1974 (SOLAS) and Commonwealth or State government marine legislation • voluntarily equipped with GMDSS radiocommunication installations. It is the recommended textbook for candidates wishing to qualify for the Australian GMDSS General Operator’s Certificate of Proficiency. This handbook replaces the tenth edition of the GMDSS Handbook published in September 2013, and has been amended to reflect: • changes to regulations adopted by the International Telecommunication Union (ITU) World Radiocommunications Conference (2015) • changes to Inmarsat services • an updated AMSA distress beacon registration form • changes to various ITU Recommendations • changes to the publications published by the ITU • developments in Man Overboard (MOB) devices • clarification of GMDSS radio log procedures • general editorial updating and improvements. Procedures outlined in the handbook are based on the ITU Radio Regulations, on radio procedures used by Australian Maritime Communications Stations and Satellite Earth Stations in the Inmarsat network. Careful observance of the procedures covered by this handbook is essential for the efficient exchange of communications in the marine radiocommunication service, particularly where safety of life at sea is concerned. Special attention should be given to those sections dealing with distress, urgency, and safety. Operators of radiocommunications equipment on vessels not equipped with GMDSS installations should refer to the Marine Radio Operators Handbook published by the Australian Maritime College, Launceston, Tasmania, Australia. No provision of this handbook or the ITU Radio Regulations prevents the use, by a ship in distress, of any means at its disposal to attract attention, make known its position and obtain help. -
The Navy Navigation Satellite System (Transit)
ROBERT J. DANCHIK THE NAVY NAVIGATION SATELLITE SYSTEM (TRANSIT) This article provides an update on the status of the Navy Navigation Satellite System (TRANSIT). Some insights are provided on the evolution of the system into its current configuration, as well as a discussion of future plans. BACKGROUND sign goal was never achieved for long in those early In 1958, research scientists at APL solved the orbit days because the satellites had short operational life of the first Russian satellite, Sputnik-I, by analysis of times. The failures largely resulted from inadequate the observed Doppler shift of its transmitted signal. component quality and the large number of wiring in This led immediately to the concept of satellite navi terconnections. However, after OSCAR 2 10 and OS gation and the development of the U.S. Navy Navi CAR 12 were launched in 1966 and 1967, respectively, gation Satellite System (TRANSIT) by APL, under the enough data on the failure mechanisms became avail sponsorship of the Navy's Special Projects Office, to able to APL to achieve the desired advances in reli provide position fixes for the Fleet Ballistic Missile ability. The integrated circuit introduced in OSCAR Weapon System submarines. (The articles in Ref. 1, 10 significantly extended the satellite lifetime by im a previous issue of the fohns Hopkins APL Techni proving component reliability and reducing the num cal Digest devoted to TRANSIT, give the principles ber of interconnections. Subsequently, the last major of operation and early history of the system.) Now, design change made to the solar cell interconnections, 26 years after its conception, the system is mature. -
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. -
Overview of the BDS III Signals
2018/11/17 13th Stanford PNT Symposium Overview of the BDS III Signals Mingquan Lu Tsinghua University November 8, 2018 Outline 1. Introduction The Three-step Development Plan A Brief History of BDS Development The Evolution of BDS Signals Current Status 2. Brief Description of BDS III 3. New Signals of BDS III 4. Conclusion 1 2018/11/17 The Three-step Development Plan BDS program began in the 1990s. In order to overcome various difficulties, China formulated the following three- step development plan for BDS, from active to passive, from regional to global. BDS I BDS II BDS III Experimental System Regional System Global System 2000 IOC, 2003 FOC 2010 IOC, 2012 FOC 2018 IOC, 2020 FOC 3GEO 5GEO+5IGSO+4MEO 3GEO+3IGSO+24MEO Regional Coverage Regional Coverage Global Coverage RDSS Service RDSS/RNSS Service RDSS/RNSS/SBAS Service 3 The Three-step Development Plan Step 3 (BDS III) Start the development of Step 2 (BDS II) the BDS Global System (BDS III) in 2013 to Start the development of achieve global passive Step 1 (BDS I) the BDS Regional System PNT capability by (BDS II, also known as approximately 2020. Start the development of BD-II in earlier times) in the BDS Experimental 2004 to achieve regional System (BDS I, also passive PNT capability by known as BD-I in earlier 2012. times) in 1994 to achieve regional active PNT capability by 2000. 4 2 2018/11/17 A Brief History of BDS Development The Early Active System BDS I——BDS Experimental System BDS I BDS I was established in 2000 as the first Experimental System generation of China’s navigation satellite system.