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Dissertations / Theses on the topic 'Satellite system'

Author: Grafiati

Published: 4 June 2021

Last updated: 5 March 2023

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1

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

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2

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 exper

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3

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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4

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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5

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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6

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.<br>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

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7

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.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (p. 399-412).<br>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 o

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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

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9

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.<br>CD-ROM contains 2 Excel spreadsheets.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 139-140).<br>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 feedbac

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10

Hammond, C., D. Beauvarlet, A. Kipple, et al. "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<br>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 som

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11

Brown, Barbie, Parminder Ghuman, Johnny Medina, and Randy Wilke. "A DESKTOP SATELLITE DATA PROCESSING SYSTEM." International Foundation for Telemetering, 1997. http://hdl.handle.net/10150/607552.

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International Telemetering Conference Proceedings / October 27-30, 1997 / Riviera Hotel and Convention Center, Las Vegas, Nevada<br>The international space community, including National Aeronautics and Space Administration (NASA), European Space Agency (ESA), Japanese National Space Agency (NASDA) and others, are committed to using the Consultative Committee for Space Data Systems (CCSDS) recommendations for low earth orbiting satellites. With the advent of the CCSDS standards and the availability of direct broadcast data from a number of current and future spacecraft, a large number of u

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12

Pazzani, Michael, and Anne Brindle. "An Expert System for Satellite Control." International Foundation for Telemetering, 1985. http://hdl.handle.net/10150/615592.

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International Telemetering Conference Proceedings / October 28-31, 1985 / Riviera Hotel, Las Vegas, Nevada<br>As on-board satellite systems develop increased sophistication and autonomous capabilities, failures become fewer, but the diagnosis of the remaining failures becomes more complex. In addition, autonomy requirements for space vehicles are being issued along with requirements for reduced staffing of ground stations. Thus successful groundbased fault handling in the future will require greatly increased automation of fault detection and diagnosis. This paper investigates the use of an ex

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13

Chintalapati, Lakshmi Venkata Bharadwaj. "Integration of Mission Control System, On-board Computer Core and spacecraft Simulator for a Satellite Test Bench." Master's thesis, Universitätsbibliothek Chemnitz, 2016. http://nbn-resolving.de/urn:nbn:de:bsz:ch1-qucosa-212663.

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The satellite avionics platform has been developed in cooperation with Airbus and is called „Future Low-cost Platform“ (FLP). It is based on an Onboard Computer (OBC) with redundant processor boards based on SPARC V8 microchips of type Cobham Aeroflex UT699. At the University of Stuttgart a test bench with a real hardware OBC and a fully simulated satellite is available for testing real flight scenarios with the Onboard Software (OBSW) running on representative hardware. The test bench as later the real flying satellite "Flying Laptop" – is commanded from a real Ground Control Centre (GCC). Th

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14

Clemons, Thomas M. "System analysis of a tactical multi-satellite communication system." Thesis, Monterey, California. Naval Postgraduate School, 1989. http://hdl.handle.net/10945/26289.

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15

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]"<br>"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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16

Davis, Mark J. (Mark Jeffrey). "Synchronization of system-of-systems interfaces in military satellite communications." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/43123.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design and Management Program, 2008.<br>Includes bibliographical references (p. 207-212).<br>Military systems continue to become more complex and nearly all are now part of one or more system of systems (SoS). Military satellite communications programs have expanded over the last decade from three distinct satellite constellations with dedicated ground, ship, and airborne terminals to several existing and planned satellite constellations and dozens of multi-purpose terminal variants. Each of the new systems must operate with both leg

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17

Han, Shin-Chan. "Efficient global gravity field determination from satellite-to-satellite tracking." Columbus, Ohio : Ohio State University, 2003. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1061995200.

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Thesis (Ph. D.)--Ohio State University, 2003.<br>Title from first page of PDF file. Document formatted into pages; contains xvii, 198 p.; also includes graphics (some col.). Includes abstract and vita. Advisor: Christopher Jekeli, Dept. of Geodetic Science and Surveying. Includes bibliographical references (p. 192-198).

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18

Edwards, David J. "Tracking systems for satellite communications." Thesis, University of Bristol, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.379579.

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19

Hultberg, Johanna. "Dehazing of Satellite Images." Thesis, Linköpings universitet, Datorseende, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-148044.

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The aim of this work is to find a method for removing haze from satellite imagery. This is done by taking two algorithms developed for images taken from the sur- face of the earth and adapting them for satellite images. The two algorithms are Single Image Haze Removal Using Dark Channel Prior by He et al. and Color Im- age Dehazing Using the Near-Infrared by Schaul et al. Both algorithms, altered to fit satellite images, plus the combination are applied on four sets of satellite images. The results are compared with each other and the unaltered images. The evaluation is both qualitative, i.e.

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20

Descalzi, Doug. "System design of a satellite radio frequency interference analysis system." Master's thesis, Virginia Tech, 1996. http://hdl.handle.net/10919/41244.

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see document<br>The conceptual and preliminary design of the Dynamic Link Tool (DLTool) System are presented. The DLTool System performs moderate fidelity, satellite radio frequency (RF) interference and communications analysis. The primary customer of the DLTool System is Program 607 of Lockheed Martin Corporation (LMC) in Valley Forge, Pennsylvania. The system will dramatically improve the existing satellite RF interference analysis capabilities of Program 607, which are currently inadequate. Most-importantly, the DLTool System will reduce the required analysis time for satellite RF in

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21

Descalzi, Douglas Hall. "System design of a satellite radio frequency interference analysis system /." This resource online, 1996. http://scholar.lib.vt.edu/theses/available/etd-02232010-020027/.

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22

Belguzhanov, Rustem. "Preliminary system design of the modular satellite." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2019.

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The main scope of the present thesis centres around two key points: modular block and binding interface of 4 types (mechanical/electrical/data/thermal). Throughout the development process, the preliminary design of the modular block and mechanical interface was continuously modified, that eventually evolved into the micro-satellite platform of different unit sizes for various mission applications. Similar to CubeSat platforms, it opens perspectives for a cheaper and faster satellite deployment by means of modularization and standardization of future satellite systems. The proposed design is

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23

Prince, Castro Jonathan Castro Jonathan Prince. "A global satellite system for mobile communications /." [S.l.] : [s.n.], 1995. http://library.epfl.ch/theses/?nr=1300.

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24

Chiyangcabut, Sarawoot. "An analysis of a satellite surveillance system." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1999. http://handle.dtic.mil/100.2/ADA362535.

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25

Shark, Lik. "Frame synchronisation methods for digital satellite system." Thesis, University of Central Lancashire, 1988. http://clok.uclan.ac.uk/20271/.

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The research described in this thesis was carried out in four specific areas, namely, Satellite-Switched Time-Division Multiple-Access (SSTDMA) network synchronisation, frame synchronisers, remote sensing satellite data decommutating systems, and prototype frame synchroniser implementation. In the area of SSTDMA network synchronisation, this thesis reports several new synchronisation methods based on an original on-board synchronisation concept. These new methods are shown to have some significant advantages over existing methods. Also reported is a new algorithm to determine the exact satelli

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26

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 B

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27

Beaulieu, Martin Ronald. "Launch detection satellite system engineering error analysis." Thesis, Monterey, California. Naval Postgraduate School, 1996. http://hdl.handle.net/10945/8611.

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Approved for public release; distribution is unlimited.<br>An orbiting detector of infrared (IR) energy may be used to detect the rocket plumes generated by ballistic missiles during the powered segment of their trajectory. By measuring angular directions of the detections over several observations, the trajectory properties, launch location, and impact area may be estimated using a nonlinear least-squares iteration procedure. observations from two or more sensors may be combined to form stereoscopic lines of sight (LOS), increasing the accuracy of the estimation algorithm. The focus of this r

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28

Mehta, Mehul. "Power control for a mobile satellite system." Thesis, University of Southampton, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.245306.

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29

Barry, Richard Malan. "Design of a distributed satellite ground system." Thesis, Stellenbosch : Stellenbosch University, 2001. http://hdl.handle.net/10019.1/52180.

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Thesis (MEng)--University of Stellenbosch, 2001.<br>ENGLISH ABSTRACT: This thesis describes the development of a distributed ground support system to be used in the small satellite program at the University of Stellenbosch. A literature study was done to determine the current trends in ground support design. These trends are presented together with an analysis of the SUNSAT groundstation software. New technologies in the field of distributed systems are discussed and used in the design of a distributed ground support system. The design centres around a servicesbased architecture where s

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30

Orozco, Gina. "BASELINE COMMUNICATIONS SYSTEM FOR A SMALL SATELLITE." International Foundation for Telemetering, 2003. http://hdl.handle.net/10150/605374.

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International Telemetering Conference Proceedings / October 20-23, 2003 / Riviera Hotel and Convention Center, Las Vegas, Nevada<br>The NMSUSat is part of the AFRL/NASA University Nanosatellite program. The constellation will consist of a main microsatellite that will have a command link from ground and a telemetry link to ground while a picosatellite will act as a sensor reporting data to the microsatellite. Innovative command and data handling will be incorporated at low cost and greater accessibility. In this paper we present the necessary communications and control architecture for the

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31

Hagen, Christoph. "A Bluetooth based intra-satellite communication system." Thesis, Luleå tekniska universitet, Rymdteknik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-65116.

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This thesis presents a wireless communication system for intra-satellite communication based on Bluetooth Low Energy technology, which can have many benefits regarding the design and operation of satellites. The proposed design based on the nRF53832 chip from Nordic Semiconductor is described, followed by the results of several tests regarding the most important design criteria for its application in small satellites. The tested aspects include the power consumption of the wireless module in different operation modes, which is sufficiently low for the application even in small satellites. Sign

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Ruddy, Marcus A. "Pico-Satellite Integrated System Level Test Program." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/688.

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Testing is an integral part of a satellite’s development, requirements verification and risk mitigation efforts. A robust test program serves to verify construction, integration and assembly workmanship, ensures component, subsystem and system level functionality and reduces risk of mission or capability loss on orbit. The objective of this thesis was to develop a detailed test program for pico-satellites with a focus on the Cal Poly CubeSat architecture. The test program established a testing baseline from which other programs or users could tailor to meet their needs. Inclusive of the tes

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Holtzman, Wendy A. "Design of the control systems operations for the Iridium satellite system." Thesis, This resource online, 1995. http://scholar.lib.vt.edu/theses/available/etd-02132009-172625/.

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Khorev, Andrey. "Hardware/Software prototyping of a miniaturized star tracker system for a nanosatellite platform." Thesis, Montpellier, 2016. http://www.theses.fr/2016MONTT248/document.

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Depuis les tous premiers jours de l'ère spatiale, les satellites artificiels ont été considérés comme un outil pour la résolution de problèmes scientifiques et pratiques, notamment dans l'astronomie, l'observation de la Terre et les télécommunications. Traditionnellement, les gros satellites artificiels, avec une masse allant de plusieurs centaines de kilogrammes jusqu'à plusieurs tonnes, ont été utilisés pour ces besoins. Un élément clef pour permettre le succès de ces missions spatiales est un contrôle précis de l'attitude du satellite. Afin d'assurer la haute précision de pointage, un systè

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Mwanakatwe, Mupanga. "Design and link system of a Ka-band VSAT system for use with the Olympus satellite." Thesis, University of Surrey, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.255759.

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36

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

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Thipphayathetthana, Somwang. "Model-based guidelines for user-centric satellite control software development." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/105320.

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Thesis: S.M. in Engineering and Management, Massachusetts Institute of Technology, Engineering Systems Division, 2015.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (page 45).<br>Three persistent common problems in satellite ground control software used by satellite controllers are obsolescence, lack of desired features and flexibilities, and endless software bug fixing. The obsolescence problem occurs when computer and ground equipment hardware become obsolete usually after only one third into the satellite mission lifetime. The satellite ground control softw

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38

Braasch, Michael S. "On the characterization of multipath errors in satellite-based precision approach and landing systems." Ohio : Ohio University, 1992. http://www.ohiolink.edu/etd/view.cgi?ohiou1173748635.

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Nötzel, Klaus R. "Integrated Satellite Control Center." International Foundation for Telemetering, 1995. http://hdl.handle.net/10150/611618.

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International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, Las Vegas, Nevada<br>Deutsche Telekom has been operating different flight models for several years. A Satellite Control Center (SCC) was designed and installed to support the operation of the satellite systems DFS Kopernikus and TV-Sat. The DFS Kopernikus system is composed of three flight models and the satellite system TV-Sat has one flight model. The aim was to design an SCC and ground stations in a way, enabling the operation of satellites and groundstations by only two operators at the main c

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Roberts, Ellen E. "Streamlined automated logistics transmission system program management and commercial satellite systems analyses." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1999. http://handle.dtic.mil/100.2/ADA366174.

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Thesis (M.S. in Systems Techology (Command, Control, and Communications)) Naval Postgraduate School, June 1999.<br>"June 1999". Thesis advisor(s): John Osmundson, Douglas Brinkley. Includes bibliographical references (p. 83-84). Also available online.

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Smith, H. Todd. "A systems engineering approach to designing a remote sensing satellite simulation system." Master's thesis, This resource online, 1995. http://scholar.lib.vt.edu/theses/available/etd-02162010-020240/.

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Luciani, Daniel Patrick. "System Design and Implementation of the Virginia Tech Optical Satellite Tracking Telescope." Thesis, Virginia Tech, 2016. http://hdl.handle.net/10919/71387.

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The Virginia Tech Optical Satellite Tracking Telescope (VTOST) aims to test the feasibility of a commercial off-the-shelf (COTS) designed tracking system for Space Situational Awareness (SSA) data contribution. A novel approach is considered, combining two COTS systems, a high-powered telescope, built for astronomy purposes, and a larger field of view (FOV) camera. Using only publicly available two-line element sets (TLEs), orbital propagation accuracy degrades quickly with time from epoch and is often not accurate enough to task a high-powered, small FOV telescope. Under this experimental app

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Hellman, Hans. "Design of wire boom system for a satellite." Thesis, KTH, Rymd- och plasmafysik, 1996. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-91569.

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Broomhall, Mark A. "Development of the portable satellite laser ranging system /." Full text available, 2003. http://adt.curtin.edu.au/theses/available/adt-WCU20041207.142708.

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Gerhart, Charlotte M. "A model for communications satellite system architecture assessment." Thesis, Monterey, California. Naval Postgraduate School, 2011. http://hdl.handle.net/10945/5594.

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Approved for public release; distribution is unlimited.<br>Communications satellite system architecture trades traditionally consider only the cost per unit of capacity provided. This selection method ignores the other requirements with which the system architectures were designed and which are critical to providing a capability to the warfighter. A survey of communications satellite systems identified five common attributes that are incorporated in the design process: communications capacity; access; interoperability; commandability; and information assurance and protection. A mathematical mo

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Hecker, Michael A. "An expert system for processing uncorrelated satellite tracks." Thesis, Monterey, California. Naval Postgraduate School, 1992. http://hdl.handle.net/10945/23894.

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47

Cooke, Adrian (Adrian Gerard). "Rural e-mail system for the Sumbandila satellite." Thesis, Stellenbosch : Stellenbosch University, 2007. http://hdl.handle.net/10019.1/17745.

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Thesis (MScIng)--University of Stellenbosch, 2007.<br>ENGLISH ABSTRACT: Keywords: digital signal processing, OSI layer, network protocols, embedded systems, satellite technology This thesis describes the design and implementation of a rural e-mail system for the Sumbandila satellite. The rural e-mail system was developed during a project sponsored by the Department of Communications of the South African government. The complete Open Systems Interconnect (OSI) layer structure of the protocol architecture used on the satellite hardware and software is described. The equivalent implementati

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48

Nasta, Rodolphe. "TELECOMMUNICATION SATELLITE TELEMETRY TRACKING AND COMMAND SUB-SYSTEM." International Foundation for Telemetering, 1998. http://hdl.handle.net/10150/607355.

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International Telemetering Conference Proceedings / October 26-29, 1998 / Town & Country Resort Hotel and Convention Center, San Diego, California<br>This paper gives an overview on Telemetry, Tracking and Command (TTC) sub-system that are used onboard some telecommunication satellites. Then, a description of the equipments of such a sub-system is given, together with the main performances.

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49

Holstein, Dennis K. "Integrated Satellite Control Open System Architecture Design Standards." International Foundation for Telemetering, 1993. http://hdl.handle.net/10150/611876.

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International Telemetering Conference Proceedings / October 25-28, 1993 / Riviera Hotel and Convention Center, Las Vegas, Nevada<br>Design standards defined in this paper provide the framework to implement an open system architecture to achieve the interoperability requirements for integrated satellite control directed by USCINCSPACE. Ground segment space operations that implement these standards will provide the capability to eliminate the artificial barriers between mission unique ground systems that operate in a stove-pipe manner today. Through common support equipment and advanced workstat

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He, Xiaoping. "The signalling system in satellite personal communication networks." Thesis, University of Surrey, 1996. http://epubs.surrey.ac.uk/844181/.

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Recent advances in both satellite and terrestrial mobile communications technologies are now leading to the realisation of the dream of the global personal communications within a few years. Satellite systems, as a complement to terrestrial cellular systems, are introduced into the future Personal Communication Networks (S-PCN) to provide global coverage and to allow global roaming. The inter-working and the integration between the satellite and the terrestrial cellular systems (e.g. GSM system) are the key issues in developing the network architecture and designing the control functions and s

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