913 resultados para 100508 Satellite Communications
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For microwave applications, including mobile and satellite communications, ceramic resonators should have a high dielectric constant, low dielectric losses, and high frequency stability. In this sense, TiO2-ZrO 2 ceramics have been investigated as a function of sintering behavior, phase composition, and microstructure. The ceramics were densified reaching a value of about 86% of theoretical density at 1400°C sintering temperature. The ceramics are prepared by mixing raw materials with the following TiO2-ZrO2 weight % ratio: 100 to 0, 90 to 10, and 80 to 20, respectively. The measured dielectric constants are between 79 and 88 values, while the quality factor due to dielectric losses are between 2820 and 5170. These results point out the influence of Ti/Zr ratio on controlling the dielectric properties. © (2010) Trans Tech Publications.
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La tesi descrive alcune applicazioni in ambito satellitare delle tecniche di radio cognitiva. In particolare si analizza la loro possibile implementazione in uno scenario dual-satellite in banda Ka nel quale l'utente primario si avvale dello standard DVB-S2 per la trasmissione. A seguire la verifica delle performance degli algoritmi di spectum sensing per la detection del segnale primario attraverso simulazioni in ambiente matlab con curve ROC e curve di probabilità di detection in funzione del rapporto segnale rumore.
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From its original formulation in 1990 the International Trans-Antarctic Scientific Expedition (ITASE) has had as its primary aim the collection and interpretation of a continent-wide array of environmental parameters assembled through the coordinated efforts of scientists from several nations. ITASE offers the ground-based opportunities of traditional-style traverse travel coupled with the modern technology of CPS, crevasse detecting radar, satellite communications and multidisciplinary research. By operating predominantly in the mode of an oversnow traverse, ITASE offers scientists the opportunity to experience the dynamic range of the Antarctic environment. ITASE also offers an important interactive venue for research similar to that afforded by oceanographic research vessels and large polar field camps, without the cost of the former or the lack of mobility of the latter. More importantly, the combination of disciplines represented by ITASE provides a unique, multidimensional (space and time) view of the ice sheet and its history. ITASE has now collected > 20 000 km of snow radar, recovered more than 240 firn/ice cores (total length 7000m), remotely penetrated to similar to 4000m into the ice sheet, and sampled the atmosphere to heights of > 20 km.
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This work provides the development of an antenna for satellite communications onboard systems based on the recommendations ITU-R S.580-6 [1] and ITU-R S.465-5 [2]. The antenna consists of printed elements grouped in an array, working in a frequency band from 7.25 up to 8.4 GHz (15% of bandwidth). In this working band, transmission and reception are included simultaneously. The antenna reaches a gain about 31 dBi, has a radiation pattern with a beam width smaller than 10oand dual circular polarization. It has the capability to steer in elevation through a Butler matrix to 45
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Nowadays, more a more base stations are equipped with active conformal antennas. These antenna designs combine phase shift systems with multibeam networks providing multi-beam ability and interference rejection, which optimize multiple channel systems. GEODA is a conformal adaptive antenna system designed for satellite communications. Operating at 1.7 GHz with circular polarization, it is possible to track and communicate with several satellites at once thanks to its adaptive beam. The antenna is based on a set of similar triangular arrays that are divided in subarrays of three elements called `cells'. Transmission/Receiver (T/R) modules manage beam steering by shifting the phases. A more accurate steering of the antenna GEODA could be achieved by using a multibeam network. Several multibeam network designs based on Butler network will be presented
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An antenna which has been conceived as a portable system for satellite communications based on the recommendations ITU-R S.580-6 and ITU-R S.465-5 for small antennas, i.e., with a diameter lower than 50 wavelengths, is introduced. It is a planar and a compact structure with a size of 40×40×2 cm. The antenna is formed by an array of 256 printed elements covering a large bandwidth (14.7%) at X-Band with a VSWR of 1.4:1. The specification includes transmission (Tx) and reception (Rx) bands simultaneously. The printed antenna has a radiation pattern with a 3dB beamwidth of 5°, over a 31dBi gain, and a dual and an interchangeable circular polarization.
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In this letter, a dual circular polarized steering antenna for satellite communications in X-band is presented. This antenna consists of printed elements grouped in an array, able to work from 7.25 up to 8.4 GHz in both polarizations: left-handed circular polarization (LHCP) and right-handed circular polarization (RHCP). The module antenna is compact, with narrow beamwidth, and reaches a gain of 16 dBi. It has the capability to steer in elevation to and electronically with a Butler matrix. In order to reduce the mutual coupling between adjacent patches, electromagnetic band-gap (EBG) structures are introduced. These EBGs combine double-layer and edge location via in order to reduce the size, without changing the low-permittivity substrate, and therefore maintaining the high radiation efficiency of the antenna.
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An asymmetric stripline is proposed in this paper. The main aim of this line is to distribute the power among subarrays in an array with minimum losses. Several vertical transitions to subarrays are shown besides some network designs at X band for a square array for satellite communications.
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Satellite operators are starting to use the Ka-band (30/20 GHz) for communications systems requiring higher traffic capacity. The use of this band is expected to experience a significant growth in the next few years, as several operators have reported plans to launch new satellites with Ka-band capacity. It is worth mentioning the Ka-Sat satellite in Europe, launched in 2010, and ViaSat-1, of 2011, with coverage of USA1. Some other examples can be found in other parts of the World. Recent satellite communications standards, such as DVB-S22 or DVB-RCS3, which provide means to mitigate propagation impairments, have been developed with the objective of improving the use of the Ka-band, in comparison with previous technical standards. In the next years, the ALPHASAT satellite will bring about new opportunities4 for carrying out propagation and telecommunication experiments in the Ka- and Q/V-bands. Commercial uses are focused on the provision of high speed data communications, for Internet access and other applications. In the near future, it is expected that higher and higher data rates will also be needed to broadcast richer multimedia contents, including HD-TV, interactive content or 3D-TV. All of these services may be provided in the future by satellites of the current generation, whose life span can extend up to 2025 in some cases. Depending on local regulations, the available bandwidth for the satellite fixed and broadcasting services in the Ka-band is in excess of several hundred MHz, bidirectional, comprising more than 1 GHz for each sub-band in some cases. In this paper, the results of a propagation experiment that is being carried out at Universidad Politécnica de Madrid (UPM), Spain, are presented5. The objective of the experiment is twofold: gathering experimental time series of attenuation and analyzing them in order to characterize the propagation channel at these frequencies6. The experiment and statistical results correspond to five complete years of measurements. The experiment is described in more detail in Section II. Yearly characteristics of rain attenuation are presented in Section III, whereas Section IV is dedicated to the monthly, seasonal, and hourly characteristics. Section V covers the dynamic characteristics of this propagation effect, just before the conclusions are described in Section VI.
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In this paper a low cost man-pack antenna for satellite communications at X band is presented. The antenna has dual circular polarization in Tx and Rx.
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This document contains the different parts of a plain antenna which is able to establish a satellite communication. This antenna has been designed in Ku Band. Nowadays this band is specially used by satellite communications and shows numerous advantages, for instance the antennas have small size therefore these antennas are cheaper. The SIW technology is a fundamental part of this project from start to end, because this technology has a lot of applications and leads in this field. Not only have been simulated all the elements of this antenna but also have been built to compare both simulations and measurements.
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En la era actual de la tecnología en la que nos encontramos se han experimentado una infinidad de avances. En concreto el interés por las comunicaciones por satélite y los, cada vez más exigentes, terminales móviles han provocado que se inicie líneas de investigación en el campo de las telecomunicaciones. En concreto el estudio de las Antenas de Bocina utilizadas como alimentadores en sistemas de satélite han generado gran interés por la comunidad académica y empresarial. En este Proyecto Fin de Carrera se realiza el estudio del Método de Análisis Modal, método por el cual podemos realizar el estudio del comportamiento de los campos en recintos cerrados y con discontinuidades. El tipo de discontinuidades que se estudia son geometrías cilíndricas en las que se practica un incremento abrupto en el radio de salida. El estudio para el caso inverso, es decir geometrías cilíndricas con radios de salida menores, también lo abordamos, es por esto que es posible la formación de corrugaciones. El proyecto es una continuación de otro anterior que se centra en la optimización de bocinas cónicas lisas. Aunque el método se puede aplicar a cualquier tipo de geometría en este proyecto lo aplicaremos sólo a geometrías cilíndricas dado que diseñaremos un alimentador de bocina cilíndrica con paredes corrugadas. Para el estudio y la implementación de las distintas formulaciones matemáticas haremos uso de la herramienta de cálculo MatLab, es así que podremos generar resultados como el diagrama de radiación de la antena diseñada. Dichos resultados serían contrastados con otro programa de análisis comercial. Se observaría que finalmente el método del análisis modal es una herramienta de cálculo robusta y consistente, que nos permite ahorrar tiempos de cálculo y nos presenta resultados similares a otras herramientas comerciales de análisis electromagnético. ABSTRACT. Technologies sector has made great progress . Specifically, in the area of the satellite communications and mobile communications . These have begun investigation lines in telecommunication areas. Particularly, the study about horn antennas use how feeders in satellite communications have generated high interest at University community and the space companies. The Final Project study is focused in the Method of Modal Analysis, this method allows to study the performance of Electromagnetic fields in closed places with discontinuities. This Project continues other project, where studied the optimization for smoothwall conical horns. In this work we will use this study for implemented a antenna cylindrical corrugated. For the study and implementation of special mathematical equations is necessary to use a calculus mathematical tool like MatLab, this software allows to draw the radiation pattern for antennas design. It should be emphasized that all results will be compare with others commercial softwares for Electromagnetic studies. Finally, we take a look at the method of modal analysis is a robust and consistent mathematical tool that save simulation time and show us similar results to other commercial softwares.
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Actualmente las redes VSAT (Very Small Aperture Terminal) están adquiriendo una mayor importancia en las comunicaciones por satélite debido a las nuevas aplicaciones que se están desarrollando tanto a nivel empresarial como a nivel de usuario final. El presente proyecto pretende hacer un estudio de este tipo de red para presentarla como una solución al problema de querer conectar estaciones dispersas, que por el perfil del terreno hace difícil la conexión de las mismas a través de las redes terrestres convencionales. Los nuevos estándares están haciendo que este tipo de redes proliferen muy deprisa ya que se consigue una mayor flexibilidad que con los estándares precedentes para este tipo de red. En concreto, en este proyecto se ha estudiado el estándar abierto DVB-S desarrollado por el grupo de trabajo DVB por ser uno de los más aceptado internacionalmente. Para comprender este sistema de comunicaciones, el proyecto está estructurado en dos partes. En la primera parte se hace una revisión de cómo han evolucionado las comunicaciones satelitales VSAT, indicando las ventajas y desventajas de su implementación y sobre todo la orientación que éstas muestran a la utilización de los estándares DVB. Posteriormente se realiza un estudio de los estándares DVB-S y DVBRCS en donde se profundiza en conceptos claves tales como el Multiplexado de Transporte MPEG-2, los mecanismos de envío de mensajes de señalización, etc. En la segunda parte del proyecto se presta atención a la seguridad de la red, analizando los mecanismos propios que presenta el estándar DVB así como los diferentes protocolos de seguridad existentes en las capas superiores para una protección adicional. Para concluir el proyecto se han creado dos aplicaciones, la primera como método didáctico para comprender mejor el comportamiento de las redes VSAT con el estándar DVB-S, y una segunda aplicación con carácter comercial para la transferencia de ficheros de manera segura con características específicas, enfocada particularmente en redes VSAT, aunque siendo posible su uso en otras redes. ABSTRACT. Nowadays VSAT networks (Very Small Aperture Terminal) are becoming more important in satellite communications, due to several new applications that are being developed both at company level and end user level. This project aims to make a study of this type of network to present it as a solution to the problem of wanting to connect scattered stations, because the terrain profile makes difficult to connect them via conventional terrestrial networks. New standards are making that such networks proliferate very quickly for the reason that a more flexibility than the previous standards for this type of network is achieved. Specifically, this project has studied the open standard DVB-S developed by the DVB workgroup as one of the most internationally accepted. To understand this communication system, this project is structured in two different parts: On one hand, in the first part a review about how VSAT satellite communications have evolved, indicating the advantages and disadvantages of its implementation and above all, the guidance that they show to the use of the DVB standards. Subsequently, a study of the DVB-S and DVB-RCS standards is developed, where delves into key concepts such as MPEG-2 Multiplexed Transport, mechanisms of transmission of signaling messages, etc. On the other hand, in the second part of the project, we focus on network security, analyzing the mechanisms presented by the DVB standard and various existing security protocols in the upper layers for an extra protection. To complete the project two different applications have been developed: the first one as a teaching method to better understand the behavior of VSAT networks in DVB-S standard, and the second one with a commercial basis for transferring files securely with specific features applications focused particularly in VSAT networks, although with a possible use on other networks.
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Esta tesis se desarrolla dentro del marco de las comunicaciones satelitales en el innovador campo de los pequeños satélites también llamados nanosatélites o cubesats, llamados así por su forma cubica. Estos nanosatélites se caracterizan por su bajo costo debido a que usan componentes comerciales llamados COTS (commercial off-the-shelf) y su pequeño tamaño como los Cubesats 1U (10cm*10 cm*10 cm) con masa aproximada a 1 kg. Este trabajo de tesis tiene como base una iniciativa propuesta por el autor de la tesis para poner en órbita el primer satélite peruano en mi país llamado chasqui I, actualmente puesto en órbita desde la Estación Espacial Internacional. La experiencia de este trabajo de investigación me llevo a proponer una constelación de pequeños satélites llamada Waposat para dar servicio de monitoreo de sensores de calidad de agua a nivel global, escenario que es usado en esta tesis. Es ente entorno y dadas las características limitadas de los pequeños satélites, tanto en potencia como en velocidad de datos, es que propongo investigar una nueva arquitectura de comunicaciones que permita resolver en forma óptima la problemática planteada por los nanosatélites en órbita LEO debido a su carácter disruptivo en sus comunicaciones poniendo énfasis en las capas de enlace y aplicación. Esta tesis presenta y evalúa una nueva arquitectura de comunicaciones para proveer servicio a una red de sensores terrestres usando una solución basada en DTN (Delay/Disruption Tolerant Networking) para comunicaciones espaciales. Adicionalmente, propongo un nuevo protocolo de acceso múltiple que usa una extensión del protocolo ALOHA no ranurado, el cual toma en cuenta la prioridad del trafico del Gateway (ALOHAGP) con un mecanismo de contienda adaptativo. Utiliza la realimentación del satélite para implementar el control de la congestión y adapta dinámicamente el rendimiento efectivo del canal de una manera óptima. Asumimos un modelo de población de sensores finito y una condición de tráfico saturado en el que cada sensor tiene siempre tramas que transmitir. El desempeño de la red se evaluó en términos de rendimiento efectivo, retardo y la equidad del sistema. Además, se ha definido una capa de convergencia DTN (ALOHAGP-CL) como un subconjunto del estándar TCP-CL (Transmission Control Protocol-Convergency Layer). Esta tesis muestra que ALOHAGP/CL soporta adecuadamente el escenario DTN propuesto, sobre todo cuando se utiliza la fragmentación reactiva. Finalmente, esta tesis investiga una transferencia óptima de mensajes DTN (Bundles) utilizando estrategias de fragmentación proactivas para dar servicio a una red de sensores terrestres utilizando un enlace de comunicaciones satelitales que utiliza el mecanismo de acceso múltiple con prioridad en el tráfico de enlace descendente (ALOHAGP). El rendimiento efectivo ha sido optimizado mediante la adaptación de los parámetros del protocolo como una función del número actual de los sensores activos recibidos desde el satélite. También, actualmente no existe un método para advertir o negociar el tamaño máximo de un “bundle” que puede ser aceptado por un agente DTN “bundle” en las comunicaciones por satélite tanto para el almacenamiento y la entrega, por lo que los “bundles” que son demasiado grandes son eliminados o demasiado pequeños son ineficientes. He caracterizado este tipo de escenario obteniendo una distribución de probabilidad de la llegada de tramas al nanosatélite así como una distribución de probabilidad del tiempo de visibilidad del nanosatélite, los cuales proveen una fragmentación proactiva óptima de los DTN “bundles”. He encontrado que el rendimiento efectivo (goodput) de la fragmentación proactiva alcanza un valor ligeramente inferior al de la fragmentación reactiva. Esta contribución permite utilizar la fragmentación activa de forma óptima con todas sus ventajas tales como permitir implantar el modelo de seguridad de DTN y la simplicidad al implementarlo en equipos con muchas limitaciones de CPU y memoria. La implementación de estas contribuciones se han contemplado inicialmente como parte de la carga útil del nanosatélite QBito, que forma parte de la constelación de 50 nanosatélites que se está llevando a cabo dentro del proyecto QB50. ABSTRACT This thesis is developed within the framework of satellite communications in the innovative field of small satellites also known as nanosatellites (<10 kg) or CubeSats, so called from their cubic form. These nanosatellites are characterized by their low cost because they use commercial components called COTS (commercial off-the-shelf), and their small size and mass, such as 1U Cubesats (10cm * 10cm * 10cm) with approximately 1 kg mass. This thesis is based on a proposal made by the author of the thesis to put into orbit the first Peruvian satellite in his country called Chasqui I, which was successfully launched into orbit from the International Space Station in 2014. The experience of this research work led me to propose a constellation of small satellites named Waposat to provide water quality monitoring sensors worldwide, scenario that is used in this thesis. In this scenario and given the limited features of nanosatellites, both power and data rate, I propose to investigate a new communications architecture that allows solving in an optimal manner the problems of nanosatellites in orbit LEO due to the disruptive nature of their communications by putting emphasis on the link and application layers. This thesis presents and evaluates a new communications architecture to provide services to terrestrial sensor networks using a space Delay/Disruption Tolerant Networking (DTN) based solution. In addition, I propose a new multiple access mechanism protocol based on extended unslotted ALOHA that takes into account the priority of gateway traffic, which we call ALOHA multiple access with gateway priority (ALOHAGP) with an adaptive contention mechanism. It uses satellite feedback to implement the congestion control, and to dynamically adapt the channel effective throughput in an optimal way. We assume a finite sensor population model and a saturated traffic condition where every sensor always has frames to transmit. The performance was evaluated in terms of effective throughput, delay and system fairness. In addition, a DTN convergence layer (ALOHAGP-CL) has been defined as a subset of the standard TCP-CL (Transmission Control Protocol-Convergence Layer). This thesis reveals that ALOHAGP/CL adequately supports the proposed DTN scenario, mainly when reactive fragmentation is used. Finally, this thesis investigates an optimal DTN message (bundles) transfer using proactive fragmentation strategies to give service to a ground sensor network using a nanosatellite communications link which uses a multi-access mechanism with priority in downlink traffic (ALOHAGP). The effective throughput has been optimized by adapting the protocol parameters as a function of the current number of active sensors received from satellite. Also, there is currently no method for advertising or negotiating the maximum size of a bundle which can be accepted by a bundle agent in satellite communications for storage and delivery, so that bundles which are too large can be dropped or which are too small are inefficient. We have characterized this kind of scenario obtaining a probability distribution for frame arrivals to nanosatellite and visibility time distribution that provide an optimal proactive fragmentation of DTN bundles. We have found that the proactive effective throughput (goodput) reaches a value slightly lower than reactive fragmentation approach. This contribution allows to use the proactive fragmentation optimally with all its advantages such as the incorporation of the security model of DTN and simplicity in protocol implementation for computers with many CPU and memory limitations. The implementation of these contributions was initially contemplated as part of the payload of the nanosatellite QBito, which is part of the constellation of 50 nanosatellites envisaged under the QB50 project.
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Este Proyecto Fin de Carrera tiene como principal objetivo analizar la evolución de los Sistemas de Comunicación por Satélite, así como dar a conocer al lector la tecnología EGNOS y su aplicabilidad como ayuda a la navegación Aeronáutica. Este trabajo comenzará con una primera parte, la cual está dedicada a conocer qué es un satélite y como ha sido su evolución a lo largo de la historia, desde la aparición del primer satélite hasta nuestros días, así como mostrar las partes que lo componen y su proceso de lanzamiento. Todo este capítulo, sirve de base para poder entender mejor las siguientes partes del proyecto. En la segunda parte de esta memoria, se entra más en detalle y se desarrollan los temas principales de este documento. Podríamos decir que este segundo capítulo se divide a su vez en dos subpartes claramente diferenciadas: En la primera, se analiza la estructura de un sistema de comunicaciones por satélite, los diferentes tipos de satélites según su órbita o según su finalidad, viendo unos claros ejemplos de cada uno de ellos, así como las bandas de frecuencias en las que trabajan. Para concluir esta sección se habla de los diferentes tipos de servicios que ofrecen las comunicaciones por satélite para centrarnos más adelante en los servicios aeronáuticos. En la segunda parte, se habla de la aplicación de la tecnología EGNOS como ayuda a la navegación aeronáutica. Para ello, primero se explican los diferentes sistemas de navegación que usan las aeronaves, entre los que se encuentran los sistemas VOR, DME, ADF y TACAN, y después se introduce al usuario a la tecnología EGNOS, viendo su arquitectura y explicando su funcionamiento. Como ejemplo de aplicabilidad de esta tecnología se explica el novedoso sistema SLS que llevan las aeronaves. Toda esta segunda parte constituye el cuerpo del proyecto y el punto más importante de esta memoria. Para finalizar, en la última parte del Proyecto Fin de Carrera, se habla del presente y futuro del sistema EGNOS evaluando sus principales ventajas y las conclusiones que se han sacado al hacer esta memoria. ABSTRACT. This thesis has as main objective to analyze the evolution of satellite communication systems, as well as to inform the reader about EGNOS technology and its applicability as an aid to aeronautical navigation. This document will begin with a first part, which is dedicated to know what a satellite is and how has its evolution been throughout history, from the appearance of the first satellite until nowadays, as well as showing the parts that it is composed of and different launch processes. This chapter serves as a base to a better understanding of these parts of the project. In the second part of this report, more detail is introduced and it is developed the main themes of this document. We could say that this second chapter is divided in two clearly differentiated subparts: The first, analyzes the structure of a communications system by satellite, different types of satellites according to its orbit or according to their purpose, seeing some clear examples of each of them, as well as the frequency bands in which they work. To conclude, this section refers to different types of services offered by satellite communications to focus later in the aeronautical services. In the second part, application of EGNOS technology is referred as an aid to the aeronautical navigation. To do this, first they are explained the different navigation systems that the aircraft uses, which include VOR, DME, ADF and TACAN systems, and then EGNOS technology is introduced to the user, seeing its architecture and explaining its operation. As an example of applicability of this technology, the new system SLS carried by the aircraft is explained. Throughout this second part it is constituted the body of the project and the most important point of this report. Finally, in the last part of the thesis, the present and future of the EGNOS system are analyzed evaluating the main advantages and conclusions that have been obtained to make this memory.