Relevant bibliographies by topics / Navigation satellite system

Academic literature on the topic 'Navigation satellite system'

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Published: 30 May 2022
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Journal articles on the topic "Navigation satellite system"

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Чичкало-Кондрацька, Ірина Борисівна, Вікторія Вікторівна Добрянська, and Володимир Тарасович Мірошниченко. "SATELLITE NAVIGATION SYSTEM MARKETING." ЕКОНОМІКА І РЕГІОН Науковий вісник, no. 3(64) (June 7, 2017): 76–83. http://dx.doi.org/10.26906/eir.2017.3(64).879.

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UDC 69.003:658.8 Chychkalo-Kondratska, D.Sc. (Economics),Professor. V. Dobryanskaya, PhD (Technical),Associate Professor. V. Miroshnichenko, Senior Lecturer. Poltava National Technical Yurii Kondratyuk University. Satellite navigation system marketing. Satellite navigation system was developed as a defense project, but in recent decades, has formed a global market of users of satellite navigation systems, and manufacturers of navigational equipment. The article is devoted to analysis of market prospects by the European satellite navigation system Galileo. Conducted SWOT-analysis, allowed to conclude that the project «Galileo» has advantages and problems. The main problem is the complexity of creating a satellite constellation, because Europe does not have its own reliable and cheap launch vehicles. The solution may be the inclusion in the draft of Ukraine, who has processed technology of rocketry. Keywords: marketing, the global market, investment project, satellite navigation systems, launch vehicles, SWOT-analysis, marketing of the project.
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Bodhare, Hemant Gautam, and Asst Prof Gauri Ansurkar. "LEO based Satellite Navigation and Anti-Theft Tracking System for Automobiles." International Journal for Research in Applied Science and Engineering Technology 10, no. 4 (April 30, 2022): 557–63. http://dx.doi.org/10.22214/ijraset.2022.41316.

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Abstract: GPS and Inertial Navigation Systems (INS) are used today in automobile navigation and tracking systems to locate themselves in Four Dimensions (latitude, longitude, altitude, time). However, GNSS or GPS still has its own bottleneck, such as the long initialization period of Precise Point Positioning (PPP) without dense reference network. For navigation, a number of selected LEO satellites can be equipped with a transmitter to transmit similar navigation signals to land users, so they can act like GNSS satellites but with much faster geometric change to enhance GNSS capability, which is named as LEO constellation enhanced GNSS (LeGNSS). This paper focuses on Low Earth Orbit navigation and anti-theft tracking system in automobiles that represents a framework which enables a navigating vehicle to aid its Inertial Navigation System when GNSS or GPS signal becomes unusable. Over the course of following years LEO satellite constellation will be available globally at ideal geometric locations. LEO Satellite aided Inertial navigation system with periodically transmitted satellite positions has the potential to achieve meter-level-accurate location. Keywords: LEO constellation, LEO enhanced GNSS (LeGNSS), Precise Point Positioning (PPP), Inertial Navigation System (INS), Precise Orbit Determination (POD)
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Yakushenkov, A. "Satellite Navigation Systems for the USSR Merchant Marine." Journal of Navigation 38, no. 1 (January 1, 1985): 118–22. http://dx.doi.org/10.1017/s0373463300038236.

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When the satellite era commenced more than a quarter of a century ago, one could hardly foresee the world wide revolution it heralded in the development of aids to navigation for merchant shipping. However, early investigations into the possible application of satellites to maritime needs led to an understanding of the powerful potential of satellite techniques for navigation. It became clear that if the international maritime community was really interested in a global all-weather, high-precision and commercially viable navigation system; such a system could only be satellite-based. This is evident from the situation that has recently arisen in IMO, where after exhaustive discussion on the mandatory carriage of electronic position-fixing equipment on ships in designated areas, the organization could not express a preference for any particular aid, until it was decided that efforts should be made to develop a global satellite navigation system capable of meeting a new standard of navigational accuracy. Moreover, in preparing the navigational accuracy standard, account was taken of experience gained with existing satellite navigation systems.
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Zhang, Lei, and Bo Xu. "Navigation Performance of the Libration Point Satellite Navigation System in Cislunar Space." Journal of Navigation 68, no. 2 (September 18, 2014): 367–82. http://dx.doi.org/10.1017/s0373463314000617.

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Based on the candidate architectures of the libration point satellite navigation system proposed in our previous work, a navigation performance study is conducted in this paper to verify the cislunar navigation ability of the proposed system. Using scalar satellite-to-satellite range measurement between the user and libration point navigation satellites, a virtual lunar exploration mission scenario is developed to verify the navigation performance of the candidate Earth-Moon L1,2,4,5 four-satellite constellations. The simulation results indicate that the libration point satellite navigation system is available for cislunar navigation and the navigation accuracy of a few tens of metres can be achieved for both the trans-lunar cruise and lunar orbit phase. Besides that, it is also found that the navigation accuracy of the libration point satellite navigation system is sensitive to the orbit of the L1 satellite. Once the L1 navigation satellite is located in the Halo orbit or vertical Lyapunov orbit, the proposed system can present a better navigation performance in cislunar space.
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Loh, Robert. "GPS Wide Area Augmentation System (WAAS)." Journal of Navigation 48, no. 2 (May 1995): 180–91. http://dx.doi.org/10.1017/s0373463300012649.

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Today, no single technology has more broad-reaching potential for worldwide civil aviation than the future applications of satellite technology. These applications represent the greatest opportunity to enhance aviation system capacity, efficiency and safety since the introduction of radio-based navigation systems more than 50 years ago. The foundation for this optimism is the Global Positioning System (GPS), a satellite-based radio navigation system operated and controlled by the United States Department of Defense (DoD). In December 1993, DoD declared GPS to be in initial operational capability (10c), which means 24 satellites are now in orbit, available and usable for satellite navigation. The Federal Aviation Agency (FAA) responded to this potential through initiation of a comprehensive satellite programme involving government, industry and users to expedite research, development and field implementation of satellite-based navigation services.
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Bornemann, Wilfried. "Navigation satellite system Galileo." Acta Astronautica 54, no. 11-12 (June 2004): 821–23. http://dx.doi.org/10.1016/j.actaastro.2004.01.028.

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Siejka, Zbigniew. "Validation of the Accuracy and Convergence Time of Real Time Kinematic Results Using a Single Galileo Navigation System." Sensors 18, no. 8 (July 25, 2018): 2412. http://dx.doi.org/10.3390/s18082412.

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For the last two decades, the American GPS and Russian GLONASS were the basic systems used in global positioning and navigation. In recent years, there has been significant progress in the development of positioning systems. New regional systems have been created, i.e., the Japanese Quasi-Zenith Satellite System (QZSS) and Indian Regional Navigational Satellite System (IRNSS). A plan to build its own regional navigation system named Korean Positioning System (KPS) was announced South Korea on 5 February 2018. Currently, two new global navigation systems are under development: the European Galileo and the Chinese BeiDou. The full operability of both systems by 2020 is planned. The paper deals with a possibility of determination of the user’s position from individual and independent global navigation satellite system (GNSS). The article is a broader concept aimed at independent determination of precise position from individual GPS, GLONASS, BeiDou and Galileo systems. It presents real time positioning results (Real Time Kinematic-RTK) using signals from Galileo satellites only. During the test, 14 Galileo satellites were used and the number of simultaneously observed Galileo satellites varied from five to seven. Real-time measurements were only possible in certain 24-h observation windows. However, their number was completed within 6 days at the end of 2017 and beginning of 2018, so there was possible to infer about the current availability, continuity, convergence time and accuracy of the RTK measurements. In addition, the systematic errors were demonstrated for the Galileo system.
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Zavalishin, O. I. "ABOUT TWO-STAR GBAS." Civil Aviation High TECHNOLOGIES 21, no. 3 (July 3, 2018): 37–46. http://dx.doi.org/10.26467/2079-0619-2018-21-3-37-46.

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The problem of accurate navigation support for landing systems is of great importance in our time in connection with the constantly increasing intensity of air traffic in major airports. At present, there is a trend towards a transition to navigational identification of aircraft by satellite radio navigation systems. Currently, two global navigation satellite systems, composed of navigational spacecraft – the Russian GLONASS system and the USA GPS system – operate in full. Moreover, to provide the necessary accuracy of positioning and data integrity the additional means are used – differential corrections. The article gives evidence of increasing the accuracy of positioning using the GBAS system. It is shown that the positioning with using GBAS ensures data integrity, corresponding to the category of «critical data» in accordance with ICAO requirements. The technical advantages of the Russian GBAS station are given. A comparative analysis of GBAS and the ILS landing system has been carried out. The article proves the urgency of the functional augmentation development of multi-frequency multi-system terrestrial systems. To calculate the characteristics of the maintenance continuity of the GBAS system, the complex technical systems effectiveness method of evaluation was used. Numerical data are presented on the probability of solving the navigation problem in the differential mode for the nominal mode. The calculation of the maintenance continuity characteristics of the GBAS system based on the complex technical systems effectiveness method of evaluation was carried out. The advantages of using the mobile version of the GBAS LKKS-A-2000 station are substantiated to provide the helicopters with an instrument approach for landing on unprepared sites. The figure shows the implementation of coordinates estimation errors in the differential mode in solving the navigation problem using 5 navigation satellites of the GPS system. The figure shows the implementation of estimation errors for the same record in using all visible and navigational satellites. The figure shows the number of visible navigation satellites.
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Bhardwaj, Ashutosh. "Terrestrial and Satellite-Based Positioning and Navigation Systems—A Review with a Regional and Global Perspective." Engineering Proceedings 2, no. 1 (November 14, 2020): 41. http://dx.doi.org/10.3390/ecsa-7-08262.

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Satellite-based navigation techniques have revolutionized modern-day surveying with unprecedented accuracies along with the traditional and terrestrial-based navigation techniques. However, the satellite-based techniques gain popularity due to their ease and availability. The position and attitude sensors mounted on satellites, aerial, and ground-based platforms as well as different types of equipment play a vital role in remote sensing providing navigation and data. The presented review in this paper describes the terrestrial (LORAN-C, Omega, Alpha, Chayka) and satellite-based systems with their major features and peculiar applications. The regional and global navigation satellite systems (GNSS) can provide the position of a static object or a moving object i.e., in Kinematic mode. The GNSS systems include the NAVigation Satellite Timing And Ranging Global Positioning System (NAVSTAR GPS), of the United States of America (USA); the Globalnaya navigatsionnaya sputnikovaya sistema (GLObal NAvigation Satellite System, GLONASS), of Russia; BEIDOU, of China; and GALILEO, of the European Union (EU). Among the initial satellite-based regional navigation systems included are the TRANSIT of the US and TSYKLON of what was then the USSR which became operational in the 1960s. Regional systems developed in the last decade include the Quasi-Zenith Satellite System (QZSS) and the Indian Regional Navigation Satellite System (IRNSS). Currently, these global and regional satellite-based systems provide their services with accuracies of the order of 10–20 m using the trilateration method of surveying for civil use. The terrestrial and satellite-based augmented systems (SBAS) were further developed along with different surveying techniques to improve the accuracies up to centimeters or millimeter levels for precise applications.
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Tanaka, Toshiki, Takuji Ebinuma, Shinichi Nakasuka, and Heidar Malki. "A Comparative Analysis of Multi-Epoch Double-Differenced Pseudorange Observation and Other Dual-Satellite Lunar Global Navigation Systems." Aerospace 8, no. 7 (July 15, 2021): 191. http://dx.doi.org/10.3390/aerospace8070191.

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In this study, dual-satellite lunar global navigation systems that consist of a constellation of two navigation satellites providing geo-spatial positioning on the lunar surface were compared. In our previous work, we proposed a new dual-satellite relative-positioning navigation method called multi-epoch double-differenced pseudorange observation (MDPO). While the mathematical model of the MDPO and its behavior under specific conditions were studied, we did not compare its performance with other dual-satellite relative-positioning navigation systems. In this paper, we performed a comparative analysis between the MDPO and other two dual-satellite navigation methods. Based on the difference in their mathematical models, as well as numerical simulation results, we developed useful insights on the system design of dual-satellite lunar global navigation systems.
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Dissertations / Theses on the topic "Navigation satellite system"

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Štefanisko, Ivan. "Integration of inertial navigation with global navigation satellite system." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2015. http://www.nusl.cz/ntk/nusl-221167.

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This paper deals with study of inertial navigation, global navigation satellite system, and their fusion into the one navigation solution. The first part of the work is to calculate the trajectory from accelerometers and gyroscopes measurements. Navigation equations calculate rotation with quaternions and remove gravity sensed by accelerometers. The equation’s output is in earth centred fixed navigation frame. Then, inertial navigation errors are discussed and focused to the bias correction. Theory about INS/GNSS inte- gration compares different integration architecture. The Kalman filter is used to obtain navigation solution for attitude, velocity and position with advantages of both systems.
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Tetewsky, Avram Ross Jeff Soltz Arnold Vaughn Norman Anszperger Jan O'Brien Chris Graham Dave Craig Doug Lozow Jeff. "Making sense of inter-signal corrections : accounting for GPS satellite calibration parameters in legacy and modernized ionosphere correction algorithms /." [Eugene, Ore. : Gibbons Media & Research], 2009. http://www.insidegnss.com/auto/julyaug09-tetewsky-final.pdf.

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"Author biographies are available in the expanded on-line version of this article [http://www.insidegnss.com/auto/julyaug09-tetewsky-final.pdf]"
"July/August 2009." Web site title: Making Sense of GPS Inter-Signal Corrections : Satellite Calibration Parameters in Legacy and Modernized Ionosphere Correction Algorithms.
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Liu, Langtao. "An intelligent differential GPS navigation system." Thesis, Brunel University, 1997. http://bura.brunel.ac.uk/handle/2438/5219.

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This thesis describes an Intelligent Differential GPS Navigation System developed for a PhD research project. The first part of the work was to apply differential technology to Global Positioning System to locate the current position of the user with an improved positioning accuracy. The essential part of this Differential GPS system is a Differential GPS Reference Station. This DGPS Reference Station includes a DGPS mathematical model and the corresponding algorithms, which calculates the differential correction messages. These messages are then transmitted to a mobile GPS receiver by a radio data link. By using these corrections, the mobile GPS receiver's positioning accuracy can be improved from about 100 m to 4 m. This DGPS Reference station has been used to implement system software for this research. Differential correction algorithms were modified, characteristics of system components were changed, and different digital filters were also applied at different locations to investigate the impact on system performance. Besides all these capabilities which are needed for the research purpose, this DGPS Reference Station has all the standard functions, and can be used as a standard DGPS Reference Station. The second part of the work was to combine this Differential GPS system with a suitable digital map to form a navigation system. A suitable digital map database was chosen and modified, and the content of the map was then reproduced on the mobile GPS receiver's host PC screen. This digital map, combined with the current location of the user, provides the basic navigational information for the user to reach a desired destination. To help the user further and demonstrate the potential use of the system, an intelligent route-planing algorithm that can produce the optimum route automatically was also designed. The system integration was achieved by the design of the mobile navigation unit and the combination of this mobile navigation unit with the constructed DGPS Reference Station. The final system consists of a DGPS Reference Station, a UHF radio data transmitter, a mobile GPS receiver, a digital map system, a route searching and planing algorithm and a UHF radio data receiver. Field trials were carried out to test the system static and dynamic performances. Repeated experiments showed that both the static and dynamic positioning accuracies were within the range of 4 meters. The constructed system is a prototype navigation system which incorporates the basic navigational functions. It is envisaged that this system can be directly used, or further developed to suit a special need, as required. A typical application of the system would be to guide a user to a desired destination. Other examples include: aircraft autolanding control system, car self-driving, taxi fleet control, criminal tracing and personal navigation systems.
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Blunt, Paul. "Advanced global navigation satellite system receiver design." Thesis, University of Surrey, 2007. http://epubs.surrey.ac.uk/842714/.

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The research described by this thesis was undertaken at a very timely moment in the development of global navigation satellite systems (GNSS). During the course of this work the signal structure of an entirely new generation of GNSS signals was been defined. The first satellites producing a new range of different coding and modulation schemes have been launched, initiating the modernisation of the American GPS and the introduction of the European Galileo system. An important aspect of the new signal structure for both GPS modernisation and Galileo is an entirely new kind of modulation called BOC (Binary Offset Carrier). Despite certain advantages this modulation comes with the notorious characteristic of a multi-peaked correlation function. In our view all known receivers, or receiver principles, have problems with this: either because the receiver is not fail safe and is potentially unreliable (the so-called bump-jumping receiver); or the multi-peaks are eliminated at the very substantial cost in much degraded accuracy. During my research under Dr Hodgart what seems to be an entirely new and original method has been developed which entirely solves the problem of tracking BOC. The problem of multi-peaks goes away and there is no loss of potential accuracy. This thesis describes in detail this invention and the first experimental results. This research was carried out at the University of Surrey under the joint supervision of Surrey Space Centre and Surrey Satellite Technology Ltd. Shortly before this work began SSTL achieved a contract to design and build the first ever test satellite (Giove- A) of the Galileo signals and technology. This research contributed to the design and manufacture of a Galileo signal generator which was flown on-board the satellite (launched December 2005). Expanding upon SSTL's existing designs this work enabled the design and creation appropriate receivers to monitor the transmissions both in ground based emulations and real live tests after launch. These designs are intended to be the core of future SSTL space receivers. This thesis describes in detail the creation of both transmitter and receiver architectures for the testing and evaluation of GNSS signals.
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Andrade, Alessandra Arrojado Lisbôa de. "Navigating into the new millennium : the global navigation satellite system regulatory framework." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp03/MQ64258.pdf.

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Cheng, Chao-heh. "Calculations for positioning with the Global Navigation Satellite System." Ohio : Ohio University, 1998. http://www.ohiolink.edu/etd/view.cgi?ohiou1176839268.

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Park, Jihye. "IONOSPHERIC MONITORING BY THE GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS)." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1339715308.

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Macedo, Scavuzzi Dos Santos Juliana. "The liability of global navigation satellite system (GNSS) used for air navigation in Brazil." Thesis, McGill University, 2013. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=119329.

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The use of Global Navigation Satellite System (GNSS) for air navigation brings important advantages to aviation since it is able to reduce routes, save fuel and diminish greenhouse gas emissions. It is also a more flexible and precise navigational aid that improves flight operations at critical moments such approach, landing and take-off. However, the GNSS signal may fail; and depending on the moment of this failure, its failure could cause an accident. Therefore, air navigation service providers' liability in using GNSS is a concern. Since there is no international treaty that responds to the liability of the GNSS and of air navigation service providers, national solutions appear as a practical and necessary answer to liability claims. Brazil has already started using GNSS in air navigation, and it has a Ground Based Augmentation System (GBAS) that is being tested at Rio de Janeiro International Airport. Therefore, it is important to study the Brazilian liability regime in order to determine if its general liability rules, especially its governmental liability system could apply to the civil liability of the air navigation service providers using GNSS in case of an accident caused by a signal failure. These claims are mostly governed by government liability in Brazil and the legal system in place is able to respond to them. However, since there is much controversy regarding government liability under the Brazilian doctrine, a specific legislation that would be able to balance the different interests at stake seems a reasonable option.
L'utilisation du Système de positionnement par satellites (GNSS) pour la navigation aérienne offre de nombreux avantages à l'aviation puisqu'il est en mesure de réduire les itinéraires, d'économiser de l'essence et de diminuer les émissions de gaz à effet de serre. Il constitue également une aide à la navigation plus flexible et plus précise qui améliore les opérations de vol à des moments critiques tels que l'approche, l'atterrissage, et le décollage. Cependant, le signal GNSS pourrait être défectueux. Dépendamment du moment de la défaillance du signal, celle-là pourrait causer un accident. Ainsi donc, la responsabilité des fournisseurs de services de navigation aérienne est sujette à préoccupation. Puisqu'aucun traité international ne se penche sur la question de la responsabilité du GNSS et des fournisseurs de services de navigation aérienne, des solutions nationales apparaissent comme des réponses pratiques et nécessaires aux revendications de responsabilité. Le Brésil a déjà commencé à utiliser la GNSS en navigation aérienne, et a un Ground Based Augmentation System (GBAS) qui est en train d'être testé à l'aéroport international de Rio de Janeiro. Ainsi donc, il est important d'étudier le régime de responsabilité brésilien pour déterminer si ses règles générales de responsabilité – et plus particulièrement son système de responsabilité gouvernemental – pourraient également s'appliquer à la responsabilité civile des fournisseurs de services de navigation aérienne utilisant le GNSS dans le cas d'un accident causé par une défaillance de signal. Ces revendications sont en grande partie gouvernées par la responsabilité gouvernementale au Brésil et le système légal en place pour y répondre. Cependant, puisqu'il y a beaucoup de controverse entourant la responsabilité du gouvernement sous la doctrine brésilienne, une législation spécifique qui serait en mesure d'équilibrer les différents intérêts en jeu semble être une alternative raisonnable.
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Li, Jian. "Investigating the effect of the DGNSS SCAT-I data link on VOR signal reception." Ohio : Ohio University, 1996. http://www.ohiolink.edu/etd/view.cgi?ohiou1178220159.

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Bhanot, Sunil. "Implementation and optimization of a Global Navigation Satellite System software radio." Ohio : Ohio University, 1998. http://www.ohiolink.edu/etd/view.cgi?ohiou1176840392.

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Books on the topic "Navigation satellite system"

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P, Andrews Angus, Bartone Chris, and ebrary Inc, eds. Global navigation satellite systems, inertial navigation, and integration. 3rd ed. Hoboken: John Wiley & Sons, 2013.

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Andrade, Alessandra A. L. The global navigation satellite system: Navigating into the new millennium. Aldershot: Ashgate, 2001.

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Antennas for global navigation satellite systems. Chichester, West Sussex, U.K: John Wiley & Sons, 2012.

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Toshiaki, Tsujii, ed. Digital satellite navigation and geophysics. Cambridge: Cambridge University Press, 2012.

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Great Britain. Parliament. House of Commons. European Standing Committee A. Global navigation satellite system , Monday 7 June 2004. London: Stationery Office, 2004.

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Great Britain. Parliament. House of Commons. European Standing Committee A. Global Navigation Satellite System, Thursday 2 December 2004. London: Stationery Office, 2004.

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French, Gregory T. Understanding the GPS: An introduction to the Global Positioning System : what it is and how it works. Bethesda, MD: GeoResearch, 1996.

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French, Gregory T. Understanding the GPS: An introduction to the Global Positioning System : what it is and how it works. Bethesda, MD: GeoResearch Inc., 1997.

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ADMINISTRATION, FEDERAL AVIATION. Airworthiness approval of global navigation satellite system (GNSS) equipment. [Washington, D.C.]: U.S. Dept. of Transportation, Federal Aviation Administration, 2003.

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Groves, Paul D. Principles of GNSS, inertial, and multisensor integrated navigation systems. Boston: Artech House, 2008.

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Book chapters on the topic "Navigation satellite system"

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Merino, M. Romay, A. Mozo García, C. Hernandez Medel, and R. Zandbergen. "Galileo System Test Bed Validation Algorithms." In Satellite Navigation Systems, 253–54. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0401-4_33.

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Schäfer, C., H. Trautenberg, and T. Weber. "Galileo System Architecture — Status and Concepts." In Satellite Navigation Systems, 53–61. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0401-4_7.

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Shi, Chuang, and Na Wei. "Satellite Navigation for Digital Earth." In Manual of Digital Earth, 125–60. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-32-9915-3_4.

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Abstract Global navigation satellite systems (GNSSs) have been widely used in navigation, positioning, and timing. China’s BeiDou Navigation Satellite System (BDS) would reach full operational capability with 24 Medium Earth Orbit (MEO), 3 Geosynchronous Equatorial Orbit (GEO) and 3 Inclined Geosynchronous Satellite Orbit (IGSO) satellites by 2020 and would be an important technology for the construction of Digital Earth. This chapter overviews the system structure, signals and service performance of BDS, Global Positioning System (GPS), Navigatsionnaya Sputnikovaya Sistema (GLONASS) and Galileo Navigation Satellite System (Galileo) system. Using a single GNSS, positions with an error of ~ 10 m can be obtained. To enhance the positioning accuracy, various differential techniques have been developed, and GNSS augmentation systems have been established. The typical augmentation systems, e.g., the Wide Area Augmentation System (WAAS), the European Geostationary Navigation Overlay Service (EGNOS), the global differential GPS (GDGPS) system, are introduced in detail. The applications of GNSS technology and augmentation systems for space-time geodetic datum, high-precision positioning and location-based services (LBS) are summarized, providing a reference for GNSS engineers and users.
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Walker, John, and Joseph L. Awange. "Global Navigation Satellite System." In Surveying for Civil and Mine Engineers, 147–56. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-53129-8_10.

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Walker, John, and Joseph Awange. "Global Navigation Satellite System." In Surveying for Civil and Mine Engineers, 281–94. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-45803-4_14.

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Cameron, Neil. "Global Navigation Satellite System." In Arduino Applied, 339–70. Berkeley, CA: Apress, 2018. http://dx.doi.org/10.1007/978-1-4842-3960-5_19.

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Wang, Bo, Xiangsheng Liu, and Yaqi Zhang. "Global Navigation Satellite System." In Internet of Things and BDS Application, 1–70. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-9194-2_1.

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Baumann, S., and W. Lechner. "A Combined Localisation/Communications System for Mountain Rescue Applications." In Satellite Navigation Systems, 237–38. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0401-4_25.

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Jolly, C. "Europe’s Challenges in Developing its Own Satellite Navigation System." In Satellite Navigation Systems, 63–70. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0401-4_8.

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Moreno, J. Manuel Garrido, and P. Rodríguez-Contreras Pérez. "The Advent of Galileo in the European Air Navigation System." In Satellite Navigation Systems, 195–202. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0401-4_21.

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Conference papers on the topic "Navigation satellite system"

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Dziadczyk, Emil, Wojciech Zabierowski, and Andrzej Napieralski. "Satellite Navigation System GPS." In 2007 9th International Conference - The Experience of Designing and Applications of CAD Systems in Microelectronics. IEEE, 2007. http://dx.doi.org/10.1109/cadsm.2007.4297633.

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Han, Chunhao. "The BeiDou navigation satellite system." In 2014 XXXIth URSI General Assembly and Scientific Symposium (URSI GASS). IEEE, 2014. http://dx.doi.org/10.1109/ursigass.2014.6929050.

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Lu, Xiaochun. "BeiDou: Navigation Satellite System Development." In 34th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GNSS+ 2021). Institute of Navigation, 2021. http://dx.doi.org/10.33012/2021.18147.

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"Section: Navigation and information systems. Global navigation satellite system (GLONASS)." In 2017 International Conference "Quality Management,Transport and Information Security, Information Technologies" (IT&QM&IS). IEEE, 2017. http://dx.doi.org/10.1109/itmqis.2017.8085755.

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Boyko, Sergey N., Alexander S. Kukharenko, and Yury S. Yaskin. "Miniaturization of satellite navigation system navigation equipment antenna modules." In 2013 Loughborough Antennas & Propagation Conference (LAPC). IEEE, 2013. http://dx.doi.org/10.1109/lapc.2013.6711861.

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Glebocki, Robert, and Mariusz Jacewicz. "Satellite formation flight vision navigation system." In 55th AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-1333.

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Ruf, Chris. "CYGNSS: Cyclone Global Navigation Satellite System." In 31st International Technical Meeting of The Satellite Division of the Institute of Navigation (ION GNSS+ 2018). Institute of Navigation, 2018. http://dx.doi.org/10.33012/2018.15996.

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Zhao, Guangyan, and Yufeng Sun. "The availability parameters system of satellite navigation system." In 2014 Annual Reliability and Maintainability Symposium (RAMS). IEEE, 2014. http://dx.doi.org/10.1109/rams.2014.6798526.

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Perrotta, G., S. Di Girolamo, G. Perrotta, and S. Di Girolamo. "INAVS - A ICO satellite constellation navigation system." In Guidance, Navigation, and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-3603.

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Li, Wen, and Lidong Zhu. "A novel satellite selecting algorithm for BeiDou navigation satellite system." In 2015 International Conference on Wireless Communications & Signal Processing (WCSP). IEEE, 2015. http://dx.doi.org/10.1109/wcsp.2015.7341049.

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Reports on the topic "Navigation satellite system"

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Ryerson, R. A. Global navigation satellite system augmentation models environmental scan. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 2015. http://dx.doi.org/10.4095/297405.

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Hysell, David L. Mission Support for the Communication/Navigation Outage Forecast System (C/NOFS) Satellite. Fort Belvoir, VA: Defense Technical Information Center, November 2007. http://dx.doi.org/10.21236/ada483238.

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Prévost, C., and H. P. White. Mer Bleue, Ontario, Arctic surrogate study site project, 2016: global navigation satellite system survey report. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 2017. http://dx.doi.org/10.4095/304278.

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Prévost, C., and H P White. Mer Bleue, Ontario, Arctic surrogate study-site project, 2019 update, global navigation satellite system survey report. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 2020. http://dx.doi.org/10.4095/326160.

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Prévost, C., and H. P. White. Mer Bleue, Ontario, Arctic surrogate study site project, 2018 update: global navigation satellite system survey report. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 2019. http://dx.doi.org/10.4095/314595.

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Wooden, William H., John A. Bangert, and J. M. Robinson. Investigation of Polar Motion from Doppler Tracking of the NNSS (Navy Navigation Satellite System) during the MERIT Campaign. Fort Belvoir, VA: Defense Technical Information Center, April 1986. http://dx.doi.org/10.21236/ada167565.

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Robert, J., and Michael Forte. Field evaluation of GNSS/GPS based RTK, RTN, and RTX correction systems. Engineer Research and Development Center (U.S.), September 2021. http://dx.doi.org/10.21079/11681/41864.

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This Coastal and Hydraulic Engineering Technical Note (CHETN) details an evaluation of three Global Navigation Satellite System (GNSS)/Global Positioning System (GPS) real-time correction methods capable of providing centimeter-level positioning. Internet and satellite-delivered correction systems, Real Time Network (RTN) and Real Time eXtended (RTX), respectively, are compared to a traditional ground-based two-way radio transmission correction system, generally referred to as Local RTK, or simply RTK. Results from this study will provide prospective users background information on each of these positioning systems and comparisons of their respective accuracies during in field operations.
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Huntley, D., P. Bobrowsky, R. Cocking, J. Joseph, P. Neelands, R. MacLeod, D. Rotheram-Clarke, R. Usquin, and F. Verluise. Installation, operation and evaluation of an innovative global navigation satellite system monitoring technology at Ripley Landslide and South Slide near Ashcroft, British Columbia. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 2020. http://dx.doi.org/10.4095/327125.

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SCHerbakov, V. V. Global Navigation Satellite Systems: Lecture Guide. OFERNIO, January 2021. http://dx.doi.org/10.12731/ofernio.2021.24749.

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Brodie, Katherine, Brittany Bruder, Richard Slocum, and Nicholas Spore. Simultaneous mapping of coastal topography and bathymetry from a lightweight multicamera UAS. Engineer Research and Development Center (U.S.), August 2021. http://dx.doi.org/10.21079/11681/41440.

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A low-cost multicamera Unmanned Aircraft System (UAS) is used to simultaneously estimate open-coast topography and bathymetry from a single longitudinal coastal flight. The UAS combines nadir and oblique imagery to create a wide field of view (FOV), which enables collection of mobile, long dwell timeseries of the littoral zone suitable for structure-from motion (SfM), and wave speed inversion algorithms. Resultant digital surface models (DSMs) compare well with terrestrial topographic lidar and bathymetric survey data at Duck, NC, USA, with root-mean-square error (RMSE)/bias of 0.26/–0.05 and 0.34/–0.05 m, respectively. Bathymetric data from another flight at Virginia Beach, VA, USA, demonstrates successful comparison (RMSE/bias of 0.17/0.06 m) in a secondary environment. UAS-derived engineering data products, total volume profiles and shoreline position, were congruent with those calculated from traditional topo-bathymetric surveys at Duck. Capturing both topography and bathymetry within a single flight, the presented multicamera system is more efficient than data acquisition with a single camera UAS; this advantage grows for longer stretches of coastline (10 km). Efficiency increases further with an on-board Global Navigation Satellite System–Inertial Navigation System (GNSS-INS) to eliminate ground control point (GCP) placement. The Appendix reprocesses the Virginia Beach flight with the GNSS–INS input and no GCPs.
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