Relevant bibliographies by topics / Satellite system

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Satellite system'

Author: Grafiati
Published: 4 June 2021
Last updated: 5 March 2023

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Journal articles on the topic "Satellite system"

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Saiko, Volodymyr, Teodor Narytnyk, Valeriy Gladkykh, and Natalia Sivkova. "INNOVATIVE SOLUTION FOR LEO-SYSTEM WITH DISTRIBUTED SATELLITE ARCHITECTURE." Information systems and technologies security, no. 1 (2) (2020): 77–83. http://dx.doi.org/10.17721/ists.2020.1.77-83.

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An innovative solution for practical implementation in a LEO system with a "distributed satellite" architecture that can be used to provide low-orbital spacecraft communications with ground stations and users of 5G / IoT satellite services is proposed. The essence of the proposed development in the system of low-orbital satellite communication with FC-architecture is that to reduce the delay in signaling to consumers and the probability of overloading the network into a prospective system of low-orbital satellite communication, which contains artificial Earth satellites, each of which functions in Earth orbit and equipped with onboard repeaters, inter-satellite communications, a network of ground-based communication and control systems for artificial satellites of the Earth, a grouping of low-orbiting space their devices (LEO-system), which includes the grouping of root (leading) satellites and satellites-repeaters (slave), around each root satellite is formed micro-grouping of satellites-repeaters, and functions of the root satellite in the selected orbital phase of the orbital -or micro-satellites that are connected to the annular network by communication lines between satellites, and - functions of satellites-repeaters - kubsat, new is the introduction of a multilevel boundary cloud system, which is a heterogeneity distributed computing cloud structure. At the same time, the boundary clouds of the multilevel system are connected by ultra-high-speed wireless terahertz radio lines and wireless optical communication systems. The technique of estimation of access time in the proposed structure of "fog computing" on the basis of the model of access in "fog computing" with the resolution of collisions of data sources implementing the survey mode is presented.
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Utami, Vi Bauty Riska, Imam MPB, and Shinta Romadhona. "Analysis the impact of sun outage and satellite orbit at performance of the telkom 3S satellite communication system." JURNAL INFOTEL 13, no. 3 (August 31, 2021): 134–42. http://dx.doi.org/10.20895/infotel.v13i3.626.

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Satellites of communication are located at altitude of thousands kilometers above the earth's surface, so the signal is transmitted by satellite to earth station is very susceptible to interference. Every March and September equinox or when the sun crosses the Earth's equator for several days, earth station occurs a naturally interference called by sun outage. At this time, satellite and the sun reach the closest distance because satellite's position is same direction with the sun. This interference makes the signal received by earth station weaken and even disappears due to temperature noise which increases drastically. Loss of signal on the downlink side caused by noise greatly affects to the performance of satellite communication system. This study aims to analyze the effect of sun outage and satellite orbit to determine sun outage period on the performance of Telkom 3S satellite communication system. The results obtained that indicate the signal quality is represented by degradation in the Carrier to Noise Ratio (C/N) from 14,777 dB to 6,0 dB, Energy bits per Noise Ratio (Eb/No) from 11,515 dB to 2,738 dB, and increase the Bit Error Rate (BER) from 8,29×10-7 to 11,08×10-3. In addition, sun outage makes lost of satellite communication traffic and affecting link availability to 99,855324%. Meanwhile, the result from satellite orbit calculation for sun outage period based on ITU-R S.1525 standard and based by satellite’s handbook. Keywords – Telkom 3S satellite, sun outage, C/N, Eb/No, BER, link availability, sun outage period.
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Zheng, Jun Hua, and Chang Ju Wu. "Design of Moving System for Pico-Satellite Deployer." Applied Mechanics and Materials 325-326 (June 2013): 1009–13. http://dx.doi.org/10.4028/www.scientific.net/amm.325-326.1009.

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Pico-satellite’s potential use is increasingly gaining nation’s recognition. Because of its small volume and light weight, it is necessary to develop the special deployer. The key technologies of Zhejiang University Pico-Satellite Deployer (ZDPSD) are, cutter unlocking the door, conical spring driving the pico-satellite, oriented rail restricting the direction and locking shaft fixing the door. In September 2010, the two pico-satellites were launched and deployed successfully at the predetermined orbit. The paper includes designing and analyzing of the moving system, mode analyzing of the deployer and the experiments on ground and in-orbit. The key process of the development is summarized, which can be regarded as reference for the further developing.
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Klaes, K. Dieter, Marc Cohen, Yves Buhler, Peter Schlüssel, Rosemary Munro, Juha-Pekka Luntama, Axel von Engeln, et al. "An Introduction to the EUMETSAT Polar system." Bulletin of the American Meteorological Society 88, no. 7 (July 1, 2007): 1085–96. http://dx.doi.org/10.1175/bams-88-7-1085.

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The European Organisation for the Exploitation of Meteorological Satellites (EUMETSAT) Polar System is the European contribution to the European–U.S. operational polar meteorological satellite system (Initial Joint Polar System). It serves the midmorning (a.m.) orbit 0930 Local Solar Time (LST) descending node. The EUMETSAT satellites of this new polar system are the Meteorological Operational Satellite (Metop) satellites, jointly developed with ESA. Three Metop satellites are foreseen for at least 14 years of operation from 2006 onward and will support operational meteorology and climate monitoring. The Metop Programme includes the development of some instruments, such as the Global Ozone Monitoring Experiment, Advanced Scatterometer, and the Global Navigation Satellite System (GNSS) Receiver for Atmospheric Sounding, which are advanced instruments of recent successful research missions. Core components of the Metop payload, common with the payload on the U.S. satellites, are the Advanced Very High Resolution Radiometer and the Advanced Television Infrared Observation Satellite (TIROS) Operational Vertical Sounder (ATOVS) package, composed of the High Resolution Infrared Radiation Sounder (HIRS), Advanced Microwave Sounding Unit A (AMSU-A), and Microwave Humidity Sounder (MHS). They provide continuity to the NOAA-K, -L, -M satellite series (in orbit known as NOAA-15, -16 and -17). MHS is a EUMETSAT development and replaces the AMSU-B instrument in the ATOVS suite. The Infrared Atmospheric Sounding Interferometer (IASI) instrument, developed by the Centre National d'Etudes Spatiales, provides hyperspectral resolution infrared sounding capabilities and represents new technology in operational satellite remote sensing.
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Sochacki, Mateusz, and Janusz Narkiewicz. "Propulsion System Modelling for Multi-Satellite Missions Performed by Nanosatellites." Transactions on Aerospace Research 2018, no. 4 (December 1, 2018): 58–67. http://dx.doi.org/10.2478/tar-2018-0030.

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Abstract Progress in miniaturization of satellite components allows complex missions to be performed by small spacecraft. Growing interest in the small satellite sector has led to development of standards such as CubeSat, contributing to lower costs of satellite development and increasing their service competitiveness. Small satellites are seen now as a prospective replacement for conventional sized satellites in the future, providing also services for demanding users. New paradigms of multi-satellite missions such as fractionation and federalization also open up new prospects for applications of small platforms. To perform a comprehensive simulation and analysis of future nanosatellite missions, an adequate propulsion system model must be used. Such model should account for propulsion solutions which can be implemented on nanosatellites and used in multi-satellite missions. In the paper, concepts of distributed satellite systems (constellations, formations, fractionated and federated) are described with a survey of past, on-going and planned multi-satellite nanosatellites missions. Currently developed propulsion systems are discussed and the models of propulsion systems embedded in the WUT satellite simulation model are presented.
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Machida, Kazuo, and Toshiaki Iwata. "Development of Space Environment Preservation System Using Robot." Journal of Robotics and Mechatronics 18, no. 1 (February 20, 2006): 67–75. http://dx.doi.org/10.20965/jrm.2006.p0067.

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We propose the concept of a robot-oriented space system called the “Space Environment Preservation System” that maintains a satellite constellation and orbit, and develop the basic technologies. A space maintenance vehicle carries and assembles modularized satellites, and places them in orbit. It captures and diagnoses them and replaces malfunctioning modules, to increase the reliability and life of the satellite constellation. It also collects, disassembles and removes satellites from orbit at the end of a mission, helping to preserve the space environment. In order to realize the system, the modularized satellite that can be easily assembled, maintained and disassembled by a robot must be devised. We developed the ground model of such a satellite, as well as the multifunctional space maintenance vehicle that functions as an in-orbit satellite assembly plant, diagnostic station, and satellite captor. These functions were demonstrated on a space simulated testbed.
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Papiya, Sumaiya Janefar, Dr Bobby Barua, and Mehnaz Hossain. "Prospects Challenges of Bangabandhu Satellite-2." International Journal of Advanced Networking and Applications 14, no. 02 (2022): 5342–52. http://dx.doi.org/10.35444/ijana.2022.14204.

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The development of the Bangabandhu Satellite-1 has changed the direction of Bangladesh's satellite communication research. Bangladesh's dream project was the Bangabandhu Satellite 1. This satellite's primary goal is to maintain effective internet and communication services in remote places. First of all, we must concentrate to the depth of satellite communication system and its process to reach any conclusion. Our main goal of the research is to recognize a feasibility review on Bangabandhu satellite-2. So, for the feasibility studies we reviewed the most promising technical parts of Bangabandhu satellite-1. Here, we only focused the certain parts of the satellite such as coding, modulation, battery, purpose of ground station and the benefits of the satellite communication system. Then we moved on the main parts of the Bangabandhu satellite-2. As, Bangabandhu satellite-1 was Geosynchronous equatorial orbit (GEO) communication satellite and Bangabandhu satellite-2 will be Low Earth Orbit (LEO) observation satellite (LEO) so, some of configurations between them might be changed. Furthermore, we largely focused on Facts, efficiency, performance and noticeable difference between two satellites.
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Ильченко, Михаил Ефимович, Теодор Николаевич Нарытник, Борис Михайлович Рассамакин, Владимир Ильич Присяжный, and Сергей Владимирович Капштык. "СОЗДАНИЕ АРХИТЕКТУРЫ «РАСПРЕДЕЛЕННОГО СПУТНИКА» ДЛЯ НИЗКООРБИТАЛЬНЫХ ИНФОРМАЦИОННО-ТЕЛЕКОММУНИКАЦИОННЫХ СИСТЕМ НА ОСНОВЕ ГРУППИРОВКИ МИКРО- И НАНОСПУТНИКОВ." Aerospace technic and technology, no. 2 (April 26, 2018): 33–43. http://dx.doi.org/10.32620/aktt.2018.2.05.

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Presented are the results of an analysis of the growing interest in the use of low Earth orbits (up to 1500 km high) for the introduction and development of the Internet of things (Internet of Things - IoT). Industrial Internet of things (Industrial Internet of Things-IIoT). Internet of things for remote areas (Remote Internet of Things - RioT, for the purposes of scientific research and economic use of natural resources, control of the development and operation of infrastructure projects, the operation of territorially distributed industrial production, transport infrastructure. Factors significantly limiting the further introduction of micro and nano satellites are given. The authors proposed to resolve this contradiction on the basis of the developed concept of creating the architecture of a "distributed satellite". As an example, the article considers possible applications of the distributed satellite architecture in two segments of the space information systems market: remote sensing of the Earth and telecommunication systems. The application of the "distributed satellite" in radar systems with synthesized aperture (SAR-system) was considered taking into account the requirements of the operators of satellite SAR-systems and consumers of their information. It is shown. that the use of the "distributed satellite" architecture in SAR-systems also makes it possible to realize the technology of multi-static radar with a "soft" interference base (from 200 m to 1 km). The scheme of organization and interaction of the "distributed satellite" in the satellite-transmitter on the platform of the micro satellite, which is the core of the satellite cluster, and several satellites-receivers on the cube-sat platform is presented. The functions performed by the satellite-transmitter, the inter-satellite radio link and the satellite-receiver are considered in detail. The work of the "distributed satellite" is illustrated by the presented structural diagram of the SAR-system for remote sensing of the Earth, a version of the architecture of the low-orbit satellite communication system and the scheme for constructing a satellite system for the provision of IoT services. In conclusion, it is noted that the architecture of the "distributed satellite" makes it possible to effectively use satellites of the class of micro/nano satellite (cube-sat) to create complex space-based information and telecommunication systems
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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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Midthassel, Rolv, and Harald Ernst. "A mobile multimedia satellite system reusing existing satellites." International Journal of Satellite Communications and Networking 26, no. 5 (September 2008): 445–61. http://dx.doi.org/10.1002/sat.904.

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Dissertations / Theses on the topic "Satellite system"

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Anderson, Jason Lionel. "Autonomous Satellite Operations For CubeSat Satellites." DigitalCommons@CalPoly, 2010. https://digitalcommons.calpoly.edu/theses/256.

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In the world of educational satellites, student teams manually conduct operations daily, sending commands and collecting downlinked data. Educational satellites typically travel in a Low Earth Orbit allowing line of sight communication for approximately thirty minutes each day. This is manageable for student teams as the required manpower is minimal. The international Global Educational Network for Satellite Operations (GENSO), however, promises satellite contact upwards of sixteen hours per day by connecting earth stations all over the world through the Internet. This dramatic increase in satellite communication time is unreasonable for student teams to conduct manual operations and alternatives must be explored. This thesis first introduces a framework for developing different Artificial Intelligences to conduct autonomous satellite operations for CubeSat satellites. Three different implementations are then compared using Cal Poly's CP6 CubeSat and the University of Tokyo's XI-IV CubeSat to determine which method is most effective.
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Brengesjö, Carl, and Martine Selin. "Tracking System : Suaineadh satellite experiment." Thesis, KTH, Skolan för informations- och kommunikationsteknik (ICT), 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-52906.

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The purpose of this bachelor thesis is to present a tracking system for the Suaineadh satellite experiment. The experiment is a part of the REXUS (Rocket EXperiments for University Students) program and the objective is to deploy a foldable web in space. The assignment of this thesis is to develop a tracking system to find the parts from the Suaineadh experiment that will land on Earth. It is important to find the parts and recover all the data that the experiment performed during the travel in space. The implementation of this thesis investigates two different ways to track and find the experiment. The first way is to locate the experiment module by a Global Positioning System (GPS) and send the coordinates to a satellite modem, controlled by a programmed microprocessor. The other way is by using a radio beacon that sends a speciffic radio frequency. The results of this thesis presents a prototype for the tracking system with a GPS and the satellite modem and code example for the microprocessor. It also presents a working radio freqency beacon system on a Printed Circuit Board. The thesis had some unexpected incidents and had to change some directives. This rendered the work to take longer time then estimated. Despite the difficulties resulted this thesis in a working system to track the experiment.
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Smith, William Whitfield Jr. "A satellite interference location system." Diss., Georgia Institute of Technology, 1990. http://hdl.handle.net/1853/16879.

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Oiesen, Eric A. "A satellite signal recognition system." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-09052009-040513/.

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Gabor, Michael Joseph. "GPS carrier phase ambiguity resolution using satellite-satellite single differences /." Digital version accessible at:, 1999. http://wwwlib.umi.com/cr/utexas/main.

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Grungxu, Lungile Leonard. "Aspect of a hardware-in-the-loop integrated test system." Thesis, Stellenbosch : Stellenbosch University, 2003. http://hdl.handle.net/10019.1/53292.

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Thesis (MScEng)--University of Stellenbosch, 2003.
ENGLISH ABSTRACT: A multiprocessor hardware-in-the-Ioop operating system was developed for the Integrated Test System (ITS) and is aimed at implementing the ITS as a space emulation vehicle. The thesis contains a study of satellite orbits, Kepler elements, geomagnetic fields and communication protocol between the processors. The system structure consists of an orbit generator, a core-operating system and is presented with a study of the satellite sensors. In implementing the orbit propagator, there was a need to pay special attention to the Halving algorithm, the Newton Raphson method and the True Solution. These algorithms were used to calculate the true anomaly angle as a function of eccentric anomaly. The communications protocol was tested and all the errors, with their solutions, have been discussed. A concept of a geomagnetic field emulator has also been included in the hardware-in-theloop operating system. The evaluation of those aspects of the system and the conclusion are presented together with recommendations.
AFRIKAANSE OPSOMMING: 'n multiprosesseerder Hardeware in die lus bedryfstelsel is ontwikkel vir 'n Geintegreerde Toets Stelsel (ITS) en poog om die ITS te implementeer as 'n ruimte emulasie stelsel. Die tesis behels die studie van sateliet wentelbane, Kepler wentelbaan elemente, geomagnetiese velde en kommunikasie protokolle tussen die prosesseerders. Die stelsel struktuur betaal uit 'n wentelbaan propageerder, 'n kern bedryfstelsel en 'n studie van satelliet instrumentasie. As 'n deel van die implementering van die wentelbaan propageerder is die halveer algoritme, Newton-Raphson algoritme en die ware oplossing as numeriese oplossings ondersoek. Die kommunikasie protokol is getoets en foute ondersoek en word bespreek. 'n konsep vir 'n Geomagnetiese veld emulasie word die hardeware in die lus stelsel ingesluit. Die stelsel word ge-ewalueer en die gevolgtrekkings en aanbevelings gemaak.
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Selva, Valero Daniel. "Rule-based system architecting of Earth observation satellite systems." Thesis, Massachusetts Institute of Technology, 2012. http://hdl.handle.net/1721.1/76089.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2012.
Cataloged from PDF version of thesis.
Includes bibliographical references (p. 399-412).
System architecting is concerned with exploring the tradespace of early, high-level, system design decisions with a holistic, value-centric view. In the last few years, several tools and methods have been developed to support the system architecting process, focusing on the representation of an architecture as a set of interrelated decisions. These tools are best suited for applications that focus on breadth - i.e., enumerating a large and representative part of the architectural tradespace -as opposed to depth - modeling fidelity. However, some problems in system architecting require good modeling depth in order to provide useful results. In some cases, a very large body of expert knowledge is required. Current tools are not designed to handle such large bodies of knowledge because they lack scalability and traceability. As the size of the knowledge base increases, it becomes harder: a) to modify existing knowledge or add new knowledge; b) to trace the results of the tool to the model assumptions or knowledge base. This thesis proposes a holistic framework for architecture tradespace exploration of large complex systems that require a large body of expert knowledge. It physically separates the different bodies of knowledge required to solve a system architecting problem (i.e., knowledge about the domain, knowledge about the class of optimization or search problem, knowledge about the particular instance of problem) by using a rule-based expert system. It provides a generic population-based heuristic algorithm for search, which can be augmented with rules that encode knowledge about the domain, or about the optimization problem or class of problems. It identifies five major classes of system architecting problems from the perspective of optimization and search, and provides rules to enumerate architectures and search through the architectural tradespace of each class. A methodology is also defined to assess the value of an architecture using a rule-based approach. This methodology is based on a decomposition of stakeholder needs into requirements and a systematic comparison between system requirements and system capabilities using the rules engine. The framework is applied to the domain of Earth observing satellite systems (EOSS). Three EOSS are studied in depth: the NASA Earth Observing System, the NRC Earth Science Decadal Survey, and the Iridium GEOscan program. The ability of the framework to produce useful results is shown, and specific insights and recommendations are drawn.
by Daniel Selva Valero.
Ph.D.
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Asiri, Hassan M. "Steady motions of a satellite system." Thesis, University of Manchester, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.489508.

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This thesis considers two systems: a dumb-bell satellite which is a system of two point masses connected by a massless rigid rod, and a gyrostat consisting of a dumbbell satellite with a gyroscope attached. Stability of relative equilibria of the dumbbell satellite in two dimensions is studied, where two types of relative equilibrium are obtained, which correspond to two orientations: radial and tangential. The only relative equilibrium which is found to be stable is the radial position, and this stability is only satisfied when the length of the dumb-bell satellite is smaller than the radius of the orbit. The reduced energy-momentum method is used through the augmented Hamiltonian.
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Dunn, Nicholas Connor. "Satellite System Safety Analysis Using STPA." Thesis, Massachusetts Institute of Technology, 2013. http://hdl.handle.net/1721.1/85777.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2013.
CD-ROM contains 2 Excel spreadsheets.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 139-140).
Traditional hazard analysis techniques based on failure models of accident causality, such as the probabilistic risk assessment (PRA) method currently used at NASA, are inadequate for analyzing safety at the system level. System-Theoretic Accident Model and Processes (STAMP) shifts the focus of safety from preventing failures to that of a dynamic feedback control system that enforces behavioral constraints. System-Theoretic Process Analysis (STPA), the hazard analysis method based on STAMP, was applied to the launch and mission phases of a NASA/JAXA Global Precipitation Measurement (GPM) Core Observatory-based satellite. Exploiting the fact that nearly all satellites follow similar lifecycles and employ common functional architectures with relatively-decoupled, unique mission payloads, a template for future satellite STPA safety analyses was developed. The template seeks to aid and guide new STPA applications while reducing analysis time by providing the STPA analysis for many common satellite functions. Increasing pressure to reduce satellite mission costs has renewed interest in modular payloads. Traditional hazard analysis methods are dependent on the hardware used, so they must be redone for the entire system if the payload is changed. This repetition of work is time intensive and costly. STPA is the only hazard analysis method that may be performed early in development and without details of the system hardware implementation. Using the GPM-based satellite STPA analysis, the influence of the mission payload on safety at the system-level is considered. Five types of control action mismatch resulting from changing payloads were identified along with the corresponding additional STPA analysis required to ensure safety at the system level.
by Nicholas Connor Dunn.
S.M.
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Hammond, C., D. Beauvarlet, A. Kipple, R. Condit, T. Firestone, V. Ling, G. Morris, and D. Powers. "TELEMETERING SYSTEM FOR THE UA SATELLITE." International Foundation for Telemetering, 2000. http://hdl.handle.net/10150/607700.

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International Telemetering Conference Proceedings / October 23-26, 2000 / Town & Country Hotel and Conference Center, San Diego, California
This student paper was produced as part of the team design competition in the University of Arizona course ECE 485, Radiowaves and Telemetry. It presents a telemetering system proposed for UASat, a small satellite being designed for launch in the year 2004. The overall system architecture is described, including the transducers used by each subsystem, the command and telemetry packet formats, the antennas and modulation schemes, the link budget, and some hardware recommendations. A discussion of the data analysis is also included.
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Books on the topic "Satellite system"

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Bruno, Ronald C. The data distribution satellite system. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1991.

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Satellite communications systems engineering: Atmospheric effects, satellite link design, and system performance. Chichester, West Sussex, England: Wiley, 2008.

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United States. National Aeronautics and Space Administration. Altimetric system. [Washington]: NASA, 1987.

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Braun, Teresa M. Satellite Communications Payload and System. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118345214.

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United States. National Aeronautics and Space Administration., ed. Reusable reentry satellite system specification. Torrance, Calif: Science Applications International Corp., 1990.

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United States. National Environmental Satellite, Data, and Information Service., ed. Search and rescue, satellite system. [Washington, D.C.]: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, National Environmental Satellite, Data, and Information Service, 1988.

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Science Applications International Corporation. Space Sciences Dept. Advanced Planning and Analysis Division. and Lyndon B. Johnson Space Center. Engineering Directorate., eds. Satellite services system program plan. Schaumburg, IL: Advanced Planning and Analysis Division, Space Sciences Dept., Science Applications International Corporation, 1985.

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United States. National Environmental Satellite, Data, and Information Service, ed. Search and rescue, satellite system. [Washington, D.C.]: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, National Environmental Satellite, Data, and Information Service, 1988.

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H, Park Y., and Jet Propulsion Laboratory (U.S.), eds. Second-generation mobile satellite system: A conceptual design and trade-off study. Pasadena, Calif: National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, 1985.

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Schulz, Colin. A weather satellite receiving system for Pacific Island Nations. Apia, Western Samoa: South Pacific Regional Environment Programme, 1994.

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Book chapters on the topic "Satellite system"

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Weik, Martin H. "satellite system." In Computer Science and Communications Dictionary, 1515. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_16602.

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Hart, Nick. "Mobile Satellite System Design." In Satellite Communications, 103–43. Boston, MA: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4615-3230-9_3.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite orbits." In Global Positioning System, 37–67. Vienna: Springer Vienna, 1992. http://dx.doi.org/10.1007/978-3-7091-5126-6_4.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite signal." In Global Positioning System, 69–78. Vienna: Springer Vienna, 1992. http://dx.doi.org/10.1007/978-3-7091-5126-6_5.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite orbits." In Global Positioning System, 41–72. Vienna: Springer Vienna, 1997. http://dx.doi.org/10.1007/978-3-7091-3297-5_4.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite signal." In Global Positioning System, 73–87. Vienna: Springer Vienna, 1997. http://dx.doi.org/10.1007/978-3-7091-3297-5_5.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite orbits." In Global Positioning System, 43–74. Vienna: Springer Vienna, 1994. http://dx.doi.org/10.1007/978-3-7091-3311-8_4.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite signal." In Global Positioning System, 75–88. Vienna: Springer Vienna, 1994. http://dx.doi.org/10.1007/978-3-7091-3311-8_5.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite orbits." In Global Positioning System, 39–70. Vienna: Springer Vienna, 2001. http://dx.doi.org/10.1007/978-3-7091-6199-9_4.

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Hofmann-Wellenhof, Bernhard, Herbert Lichtenegger, and James Collins. "Satellite signal." In Global Positioning System, 71–85. Vienna: Springer Vienna, 2001. http://dx.doi.org/10.1007/978-3-7091-6199-9_5.

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Conference papers on the topic "Satellite system"

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Ronalds, Beverley F., Scott M. Simpson, and K. F. Thomas Foo. "Towards Satellite Production System Selection for Moderate Water Depths." In ASME 2003 22nd International Conference on Offshore Mechanics and Arctic Engineering. ASMEDC, 2003. http://dx.doi.org/10.1115/omae2003-37489.

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A large database of North Sea subsea satellites and minimum facilities platforms is used to derive and justify key drivers influencing the selection process for satellite production systems in shallow and moderate water depths. The key drivers include reservoir fluid, tieback length, water depth (d), and well count (w) and pattern. In particular, it is found that an approximate dividing line between subsea and surface satellite facilities occurs at d = kw, where k ≈ 8.5m and 15m for oil- and gas-dominated fields, respectively.
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Sasaki, Issei, and Takeshi Hatsuda. "Novel use of optical fiber data transmission technology in space: optical fiber geostationary tether satellite system." In OSA Annual Meeting. Washington, D.C.: Optica Publishing Group, 1991. http://dx.doi.org/10.1364/oam.1991.tunn5.

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A novel use of optical fiber data transmission technology is presented for an optical-fiber-linked geostationary tether satellite (F-GTS) system, in which several satellites are connected with tethers, physically, and with optical fibers. The communication linkage by optical fibers among satellites may be helpful in dividing tasks and in distributing control signals. In addition, the distance of the satellite location could also be sensed from the delay on the optical pulse propagating through the fibers.
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Curran, Robert J. "Satellite Remote Sensing for Earth System Science: NASA's Earth Observing System (Eos)." In Laser and Optical Remote Sensing: Instrumentation and Techniques. Washington, D.C.: Optica Publishing Group, 1987. http://dx.doi.org/10.1364/lors.1987.tua1.

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Environmental concerns of a global nature are influencing the development of a multidisciplinary approach to understanding the Earth as a system. In recent years these concerns have become more prominent due to a series of problems involving large geographic regions such as; understanding the effects of the increases in carbon dioxide, understanding the causes and consequences of changes in the ozone layer, and resolving the anthropogenic influence on the acidity of precipitation. Clearly the global scope of these and other problem areas requires both a multidisciplinary, as well as a multinational approach for their solution. In order to address these problems, observational capabilities must be employed ranging from in situ and laboratory measurements to satellite based global remote sensing. An Earth Observing System (Eos) is planned to meet many of these requirements for remote sensing from low Earth orbiting satellites. A number of instruments are under consideration as the payload for the sun-synchronous satellite platforms. The payload is conceptually grouped into three packages to illustrate the synergistic relationships that exist among the instruments.
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Protheroe, Mark, David R. Sloggett, and Alois J. Sieber. "EARSEC SAR processing system." In Satellite Remote Sensing, edited by Giorgio Franceschetti. SPIE, 1994. http://dx.doi.org/10.1117/12.197552.

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Vostrov, Edgar, Arcady V. Dzenkevich, Leonid A. Mel'nikov, Vladimir A. Volkov, Yury Krylov, and Victor Plyuschev. "IMARK: multifrequency airborne SAR system." In Satellite Remote Sensing, edited by Joan B. Lurie, Paolo Pampaloni, and James C. Shiue. SPIE, 1994. http://dx.doi.org/10.1117/12.197356.

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Tanaka, Masato, Shinichi Yamamoto, Kazuhiro Kimura, Nobufumi Saruwatari, and Takaya Ogawa. "Receiving System for Satellite Broadcast Using Quasi-zenithal Satellite System." In 21st International Communications Satellite Systems Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-2305.

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Yoo, Sang-Keun, Seo-Rim Lee, Hak-Jae Kim, Han-Jun Lim, Hyo-Sam Lee, Dan-Keun Sung, and Soon-Dal Choi. "KITSAT-2 CCD earth imaging system experiment." In Satellite Remote Sensing, edited by William L. Barnes and Brian J. Horais. SPIE, 1995. http://dx.doi.org/10.1117/12.198951.

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Jiang, JingShang, and Shu-hu Cao. "Real-time disaster monitoring system by using SAR." In Satellite Remote Sensing, edited by Joan B. Lurie, Paolo Pampaloni, and James C. Shiue. SPIE, 1994. http://dx.doi.org/10.1117/12.197337.

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Souilhac, Dominique J., and Dominique Billerey. "TeO2 and Te acousto-optic spectrometer imaging system." In Satellite Remote Sensing, edited by Anton Kohnle and Adam D. Devir. SPIE, 1994. http://dx.doi.org/10.1117/12.197378.

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Leitmann, Miguel G., Jose M. Rebordao, Nuno M. Gomes, Marc Fouquet, and Martin N. Sweeting. "PoSAT-1 Star Imaging System: in-flight performance." In Satellite Remote Sensing, edited by William L. Barnes and Brian J. Horais. SPIE, 1995. http://dx.doi.org/10.1117/12.198944.

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Reports on the topic "Satellite system"

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Liaw, D. C., and E. H. Abed. Tethered Satellite System Stability. Fort Belvoir, VA: Defense Technical Information Center, January 1989. http://dx.doi.org/10.21236/ada454743.

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Lauter, Judith. Pet Data Analysis Satellite System. Fort Belvoir, VA: Defense Technical Information Center, January 1988. http://dx.doi.org/10.21236/ada192048.

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Jianping, Yuan. Satellite Positioning System and Flight Dynamics,. Fort Belvoir, VA: Defense Technical Information Center, August 1995. http://dx.doi.org/10.21236/ada300160.

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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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Garriott, G. Low earth orbiting satellite for international information exchange system. Office of Scientific and Technical Information (OSTI), November 1989. http://dx.doi.org/10.2172/7170972.

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Mendoza, Luis. Production process for advanced space satellite system cables/interconnects. Office of Scientific and Technical Information (OSTI), December 2007. http://dx.doi.org/10.2172/1104784.

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Sagovac, C. P., D. A. Danielson, J. R. Clynch, and Beny Neta. Fast Interpolation for Global Positioning System (GPS) Satellite Orbits,. Fort Belvoir, VA: Defense Technical Information Center, August 1995. http://dx.doi.org/10.21236/ada298566.

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Abbot, R. I., R. Clouser, E. W. Evans, and R. Sridharan. A Monitoring and Warning System for Close Geostationary Satellite Encounters. Fort Belvoir, VA: Defense Technical Information Center, April 2001. http://dx.doi.org/10.21236/ada400524.

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Beasley, Matthew A. Development of a Microelectromechanical System for Small Satellite Thermal Control. Fort Belvoir, VA: Defense Technical Information Center, May 2004. http://dx.doi.org/10.21236/ada424969.

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Crombie, Michael A. Sentinel Satellite Positional Precision Derived from the NAVSTAR Global Positioning System. Fort Belvoir, VA: Defense Technical Information Center, August 1989. http://dx.doi.org/10.21236/ada211876.

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