GNSS Satellite-Based Augmentation Systems for Australia
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(Gnss) in View of Progress Made in Gagan
INDIA LIABILITY IN CONTEXT TO THE AIR NAVIGATION SERVICE PROVIDER + By Ranjana Kaul* The Global Navigation Satellite System1 is poised to be one of the most critical technologies in the twenty-first century. Like most other technologies, GNSS was first developed for military application, and arguably, like other dual use technologies, it is a double edged sword. The 1990 Gulf War demonstrated how GNSS can be successfully deployed as a military force multiplier. Equally civilian applications of GNSS have brought lucrative returns2 and incremental developmental benefits to countries around the world3. In specific context to @ copyright Ranjana Kaul + This paper is the expanded version of Ranjana Kaul ‟s presentation on ”INDIA: LIABILITY IN CONTEXT TO THE AIR NAVIGATION SERVICE PROVIDER‟ made at the International Conference on Contemporary Issues in Air Transport, Air Law & Regulation, New Delhi, India, 23-25 April 2008. * B.A.( Bombay University); MA; PhD. (University of Poona) LLB ( University of Delhi); LL.M (Institute of Air & Space Law, Faculty of Law, Mc Gill University, Montreal, Canada); Partner, Dua Associates, (Advocates & Solicitors) , New Delhi, India. 1 Global Navigation Satellite System (GNSS) is the standard generic term for satellite navigation systems that provide autonomous geo-spatial positioning with global coverage. A GNSS allows small electronic receivers to determine their location (longitude, latitude, and altitude) to within a few metres using time signals transmitted along a line of sight by radio from satellites. Receivers on the ground with a fixed position can also be used to calculate the precise time as a reference for scientific experiments. As of 2007, the United States NAVSTAR Global Positioning System (GPS) is the only fully operational GNSS. -
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. -
Issue #1 – 2012 October
TTSIQ #1 page 1 OCTOBER 2012 Introducing a new free quarterly newsletter for space-interested and space-enthused people around the globe This free publication is especially dedicated to students and teachers interested in space NEWS SECTION pp. 3-22 p. 3 Earth Orbit and Mission to Planet Earth - 13 reports p. 8 Cislunar Space and the Moon - 5 reports p. 11 Mars and the Asteroids - 5 reports p. 15 Other Planets and Moons - 2 reports p. 17 Starbound - 4 reports, 1 article ---------------------------------------------------------------------------------------------------- ARTICLES, ESSAYS & MORE pp. 23-45 - 10 articles & essays (full list on last page) ---------------------------------------------------------------------------------------------------- STUDENTS & TEACHERS pp. 46-56 - 9 articles & essays (full list on last page) L: Remote sensing of Aerosol Optical Depth over India R: Curiosity finds rocks shaped by running water on Mars! L: China hopes to put lander on the Moon in 2013 R: First Square Kilometer Array telescopes online in Australia! 1 TTSIQ #1 page 2 OCTOBER 2012 TTSIQ Sponsor Organizations 1. About The National Space Society - http://www.nss.org/ The National Space Society was formed in March, 1987 by the merger of the former L5 Society and National Space institute. NSS has an extensive chapter network in the United States and a number of international chapters in Europe, Asia, and Australia. NSS hosts the annual International Space Development Conference in May each year at varying locations. NSS publishes Ad Astra magazine quarterly. NSS actively tries to influence US Space Policy. About The Moon Society - http://www.moonsociety.org The Moon Society was formed in 2000 and seeks to inspire and involve people everywhere in exploration of the Moon with the establishment of civilian settlements, using local resources through private enterprise both to support themselves and to help alleviate Earth's stubborn energy and environmental problems. -
System Analysis and Design of the Geostationary Earth Orbit All-Electric Communication Satellites
https://doi.org/10.1590/jatm.v13.1205 REVIEW ARTICLE System Analysis and Design of the Geostationary Earth Orbit All-Electric Communication Satellites Parsa Abbasrezaee1,* , Ali Saraaeb2 1.Sapienza University of Rome – Aerospace Engineering School – Rome – Italy. 2.Khaje Nasir Toosi University of Technology – Aerospace department – Tehran – Iran. *Corresponding author: [email protected] ABSTRACT With the help of gathered data and formulas extracted from a previous conference paper, the all-electric geostationary Earth orbit (GEO) communication satellite statistical design was conducted and further studied with analytic hierarchy process (AHP) and technique for order of preference by similarity to ideal solution (TOPSIS) methods. Moreover, with the help of previously determined system parameters, the orbital ascension, orbital maintenance and deorbiting specifications, calculations and simulations were persuaded. Furthermore, a parametric subsystem design was conducted to test the methods reliability and prove the feasibility of such approach. The parametric subsystem design was used for electrical power subsystem (EPS), attitude determination and control system (ADCS), electric propulsion, telemetry, tracking and control (TT&C) in conceptual subsystem design level, which highly relies on the satellite type and other specifications, were concluded in this paper; other subsystem designs were not of a significant difference to hybrid and chemical satellites. Eventually, the verification of the mentioned subsystems has been evaluated by contrasting the results with the Space mission engineering: the new SMAD, and subsystem design book reference. Keywords: All-electric; GEO; AHP and TOPSIS Method; Maintenance; Deorbiting; Parametric. INTRODUCTION From the previous conference paper, the contrast between all-electric geostationary Earth orbit (GEO) communication and other hybrid and chemical satellite design has shown that using all-electric satellite design has many advantages. -
Space Technology and Telecommunication" Cluster of the Skolkovo Foundation
STRATEGIC DIRECTIONS AND PRIORITY AREAS OF DEVELOPMENT FOR "S PACE TECHNOLOGY AND TELECOMMUNICATION " CLUSTER OF THE SKOLKOVO FOUNDATION 2012 Strategic Directions and Priority Areas of Development for "Space Technology and Telecommunication" Cluster of the Skolkovo Foundation The present document describes the results of methodology development and evaluation of strategic directions and priority areas for "Space Technology and Telecommunication" Cluster of the Skolkovo Fund. The first iteration was obtained by ST&T expert group with assistance of leading space R&D institutes using the Federal Space Agency materials. The Strategic Directions will be subsequently specified under the foresight research based on the contract between the Skolkovo Fund and one of the leading R&D and consulting organizations in the field of space activity and its results' commercialization. The Glossary can be found at the end of the document EXECUTIVE SUMMARY: PRIORITIES ST&T Cluster ensures search for, attraction and selection of potential subjects of innovative process in the field of development and target use of spacecrafts operation and diversification of rocket and space industry potential, facilitates their cooperation and provides the environment for full cycle innovation process establishment, based on the Strategic directions and priority areas of development, initially defined by this document and regularly updated considering opinion of sci-tech and business community that is identified in process of foresight procedure. At the moment, the Cluster finds it necessary, along with comprehensive support for innovative activity of the Skolkovo Fund participants and applicants, to focus on proactive implementation of several priority areas which particularly include: Establishing national infrastructure of full cycle microsatellite technology which involves leading universities. -
Space Business Review
January 2009 A monthly round-up of space industry developments for the information of our clients and friends. Intelsat Senior Notes Offering Swedish Space Corporation Acquires USN Intelsat, Ltd. announced on January 29 that Swedish Space Corporation (SSC) its subsidiary, Intelsat Subsidiary Holding announced on January 21 that it had Company, Ltd. (Intelsat Sub Holdco), priced reached an agreement to acquire all of the $400 million aggregate principal amount of shares of Universal Space Network (USN). 8.875% senior notes due 2015 at an issue The two companies have been collaborating price of 88.50%. The net proceeds of the notes for the last ten years in providing worldwide will be used to fund Intelsat Sub Holdco’s satellite tracking services via PrioraNet, a purchase of a portion of Intelsat, Ltd.’s global network of ground stations. The outstanding 7.625% Senior Notes due 2012 acquisition is subject to regulatory approvals and 6.50% Senior Notes due 2013 that are in the U.S., and upon closing, USN will tendered in Intelsat Sub Holdco’s cash offer. operate as a U.S.-based subsidiary of SSC. Launched on January 14, the tender offer China Great Wall to Replace NigComSat-1 initially contemplated the purchase of $200 Following the failure of the NigComSat-1 million maximum aggregate principal amount satellite in November 2008, it is reported that of notes, however was increased to $375 Nigerian Communications Satellite Ltd. million and ultimately doubled due to strong (NigComSat) and China Great Wall Industry demand. Goldman, Sachs & Co. acted as the Corporation reached an agreement in dealer manager for the notes offering, which is December 2008 for the manufacture and in- expected to close on February 12. -
Classification of Geosynchronous Objects
esoc European Space Operations Centre Robert-Bosch-Strasse 5 D-64293 Darmstadt Germany T +49 (0)6151 900 www.esa.int CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Produced with the DISCOS Database Prepared by T. Flohrer & S. Frey Reference GEN-DB-LOG-00195-OPS-GR Issue 18 Revision 0 Date of Issue 3 June 2016 Status ISSUED Document Type TN European Space Agency Agence spatiale europeenne´ Abstract This is a status report on geosynchronous objects as of 1 January 2016. Based on orbital data in ESA’s DISCOS database and on orbital data provided by KIAM the situation near the geostationary ring is analysed. From 1434 objects for which orbital data are available (of which 2 are outdated, i.e. the last available state dates back to 180 or more days before the reference date), 471 are actively controlled, 747 are drifting above, below or through GEO, 190 are in a libration orbit and 15 are in a highly inclined orbit. For 11 objects the status could not be determined. Furthermore, there are 50 uncontrolled objects without orbital data (of which 44 have not been cata- logued). Thus the total number of known objects in the geostationary region is 1484. In issue 18 the previously used definition of ”near the geostationary ring” has been slightly adapted. If you detect any error or if you have any comment or question please contact: Tim Flohrer, PhD European Space Agency European Space Operations Center Space Debris Office (OPS-GR) Robert-Bosch-Str. 5 64293 Darmstadt, Germany Tel.: +49-6151-903058 E-mail: tim.fl[email protected] Page 1 / 178 European Space Agency CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS Agence spatiale europeenne´ Date 3 June 2016 Issue 18 Rev 0 Table of contents 1 Introduction 3 2 Sources 4 2.1 USSTRATCOM Two-Line Elements (TLEs) . -
Failures in Spacecraft Systems: an Analysis from The
FAILURES IN SPACECRAFT SYSTEMS: AN ANALYSIS FROM THE PERSPECTIVE OF DECISION MAKING A Thesis Submitted to the Faculty of Purdue University by Vikranth R. Kattakuri In Partial Fulfillment of the Requirements for the Degree of Master of Science in Mechanical Engineering August 2019 Purdue University West Lafayette, Indiana ii THE PURDUE UNIVERSITY GRADUATE SCHOOL STATEMENT OF THESIS APPROVAL Dr. Jitesh H. Panchal, Chair School of Mechanical Engineering Dr. Ilias Bilionis School of Mechanical Engineering Dr. William Crossley School of Aeronautics and Astronautics Approved by: Dr. Jay P. Gore Associate Head of Graduate Studies iii ACKNOWLEDGMENTS I am extremely grateful to my advisor Prof. Jitesh Panchal for his patient guidance throughout the two years of my studies. I am indebted to him for considering me to be a part of his research group and for providing this opportunity to work in the fields of systems engineering and mechanical design for a period of 2 years. Being a research and teaching assistant under him had been a rewarding experience. Without his valuable insights, this work would not only have been possible, but also inconceivable. I would like to thank my co-advisor Prof. Ilias Bilionis for his valuable inputs, timely guidance and extremely engaging research meetings. I thank my committee member, Prof. William Crossley for his interest in my work. I had a great opportunity to attend all three courses taught by my committee members and they are the best among all the courses I had at Purdue. I would like to thank my mentors Dr. Jagannath Raju of Systemantics India Pri- vate Limited and Prof. -
Space Security Index 2013
SPACE SECURITY INDEX 2013 www.spacesecurity.org 10th Edition SPACE SECURITY INDEX 2013 SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security Index 2013 ISBN: 978-1-927802-05-2 FOR PDF version use this © 2013 SPACESECURITY.ORG ISBN: 978-1-927802-05-2 Edited by Cesar Jaramillo Design and layout by Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Soyuz TMA-07M Spacecraft ISS034-E-010181 (21 Dec. 2012) As the International Space Station and Soyuz TMA-07M spacecraft were making their relative approaches on Dec. 21, one of the Expedition 34 crew members on the orbital outpost captured this photo of the Soyuz. Credit: NASA. Printed in Canada Printer: Pandora Print Shop, Kitchener, Ontario First published October 2013 Please direct enquiries to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 7708 Fax: 519-888-0018 Email: [email protected] Governance Group Julie Crôteau Foreign Aairs and International Trade Canada Peter Hays Eisenhower Center for Space and Defense Studies Ram Jakhu Institute of Air and Space Law, McGill University Ajey Lele Institute for Defence Studies and Analyses Paul Meyer The Simons Foundation John Siebert Project Ploughshares Ray Williamson Secure World Foundation Advisory Board Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research John Logsdon The George Washington University Lucy Stojak HEC Montréal Project Manager Cesar Jaramillo Project Ploughshares Table of Contents TABLE OF CONTENTS TABLE PAGE 1 Acronyms and Abbreviations PAGE 5 Introduction PAGE 9 Acknowledgements PAGE 10 Executive Summary PAGE 23 Theme 1: Condition of the space environment: This theme examines the security and sustainability of the space environment, with an emphasis on space debris; the potential threats posed by near-Earth objects; the allocation of scarce space resources; and the ability to detect, track, identify, and catalog objects in outer space. -
Dynamic Performance Evaluation of Various GNSS Receivers and Positioning Modes with Only One Flight Test
electronics Technical Note Dynamic Performance Evaluation of Various GNSS Receivers and Positioning Modes with Only One Flight Test Cheolsoon Lim 1, Hyojung Yoon 1, Am Cho 2, Chang-Sun Yoo 2 and Byungwoon Park 1,* 1 School of Aerospace Engineering, Sejong University, 209 Neungdong-ro, Gwangjin-gu, Seoul 05006, Korea; [email protected] (C.L.); [email protected] (H.Y.) 2 Future Aircraft Research Division, Korea Aerospace Research Institute, Daejeon 34133, Korea; [email protected] (A.C.); [email protected] (C.-S.Y.) * Correspondence: [email protected]; Tel.: +82-02-3408-4385 Received: 20 November 2019; Accepted: 7 December 2019; Published: 11 December 2019 Abstract: The performance of global navigation satellite system (GNSS) receivers in dynamic modes is mostly assessed using results obtained from independent maneuvering of vehicles along similar trajectories at different times due to limitations of receivers, payload, space, and power of moving vehicles. However, such assessments do not ensure valid evaluation because the same GNSS signal environment cannot be ensured in a different test session irrespective of how accurately it mimics the original session. In this study, we propose a valid methodology that can evaluate the dynamic performance of multiple GNSS receivers in various positioning modes with only one dynamic test. We used the record-and-replay function of RACELOGIC’s LabSat3 Wideband and developed a software that can log and re-broadcast Radio Technical Commission for Maritime Services (RTCM) messages for the augmented systems. A preliminary static test and a drone test were performed to verify proper operation of the system. -
Augmented GNSS: Fundamentals and Keys to Integrity and Continuity
ION GNSS 2011 TUTORIAL Augmented GNSS: Fundamentals and Keys to Integrity and Continuity Sam Pullen Department of Aeronautics and Astronautics Stanford University, Stanford, CA. 94305-4035 USA Tuesday, Sept. 20, 2011 1:30 – 5:00 PM Oregon Convention Center, Portland, Oregon (last updated 9/16/11) Acknowledgements: B. Belabbas, J. Blanch, R. Braff, M. Brenner, J. Burns, B. Clark, K. Class, S. Datta-Barua, P. Enge, M. Harris, R. Kelly, R. Key, J. Lee, M. Luo, A. Mitelman, T. Murphy, Y.S. Park, B. Parkinson, B. Pervan, R.E. Phelts, J. Rife, C. Rodriguez, J. Scheitlin, C. Shively, K. Suzuki, R. Swider, F. van Graas, T. Walter, J. Warburton, G. Xie, G. Zhang, and more… ©2011 by Sam Pullen Outline • Augmented GNSS Terminology • Introduction to GNSS and GNSS Augmentation – Differential GNSS (DGNSS) • GBAS and SBAS System Architectures • Aviation Applications and Requirements • Principles of Integrity and Continuity • Specific Examples: – Nominal Error Bounding – Signal Deformation Monitoring – Ephemeris Monitoring – Ionospheric Anomaly Mitigation • Summary 20 September 2011 Augmented GNSS: Integrity and Continuity 2 Augmented GNSS Terminology • GPS: Global Positioning System • GNSS: Global Navigation Satellite Systems • DGPS: Differential GPS (or GNSS) • L(A)DGPS: Local-Area Differential GPS • WADGPS: Wide-Area Differential GPS • CDGPS: Carrier-Phase Differential GPS (usually a subset of Local-Area DGPS) • LAAS: Local Area Augmentation System (FAA) • GBAS: Ground-Based Augmentation System (international; includes LAAS) • WAAS: Wide Area Augmentation -
Global Navigation Satellite Systems Performance Analysis And
Global navigation satellite systems performance analysis and augmentation strategies in aviation Roberto Sabatini1*, Terry Moore2 and Subramanian Ramasamy1 1RMIT University, School of Engineering – Aerospace Engineering and Aviation Discipline, Bundoora, VIC 3083, Australia 2University of Nottingham, Nottingham Geospatial Institute, Nottingham, NG7 2TU, United Kingdom ABSTRACT In an era of significant air traffic expansion characterised by a rising congestion of the radiofrequency spectrum and a widespread introduction of Unmanned Aircraft Systems (UAS), Global Navigation Satellite Systems (GNSS) are being exposed to a variety of threats including signal interferences, adverse propagation effects and challenging platform-satellite relative dynamics. Thus, there is a need to characterize GNSS signal degradations and assess the effects of interfering sources on the performance of avionics GNSS receivers and augmentation systems used for an increasing number of mission-essential and safety-critical aviation tasks (e.g., experimental flight testing, flight inspection/certification of ground-based radio navigation aids, wide area navigation and precision approach). GNSS signal deteriorations typically occur due to antenna obscuration caused by natural and man-made obstructions present in the environment (e.g., elevated terrain and tall buildings when flying at low altitude) or by the aircraft itself during manoeuvring (e.g., aircraft wings and empennage masking the on-board GNSS antenna), ionospheric scintillation, Doppler shift, multipath, jamming and spurious satellite transmissions. Anyone of these phenomena can result in partial to total loss of tracking and possible tracking errors, depending on the severity of the effect and the receiver characteristics. After designing GNSS performance threats, the various augmentation strategies adopted in the Communication, Navigation, Surveillance/Air Traffic Management and Avionics (CNS+A) context are addressed in detail.