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Literatura académica sobre el tema "Artificial satellites Constellations"

Autor: Grafiati

Publicado: 4 de junio de 2021

Última modificación: 5 de febrero de 2022

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Artículos de revistas sobre el tema "Artificial satellites Constellations"

Curzi, Giacomo, Dario Modenini y Paolo Tortora. "Large Constellations of Small Satellites: A Survey of Near Future Challenges and Missions". Aerospace 7, n.º 9 (7 de septiembre de 2020): 133. http://dx.doi.org/10.3390/aerospace7090133.

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Constellations of satellites are being proposed in large numbers; most of them are expected to be in orbit within the next decade. They will provide communication to unserved and underserved communities, enable global monitoring of Earth and enhance space observation. Mostly enabled by technology miniaturization, satellite constellations require a coordinated effort to face the technological limits in spacecraft operations and space traffic. At the moment in fact, no cost-effective infrastructure is available to withstand coordinated flight of large fleets of satellites. In order for large constellations to be sustainable, there is the need to efficiently integrate and use them in the current space framework. This review paper provides an overview of the available experience in constellation operations and statistical trends about upcoming constellations at the moment of writing. It highlights also the tools most often proposed in the analyzed works to overcome constellation management issues, such as applications of machine learning/artificial intelligence and resource/infrastructure sharing. As such, it is intended to be a useful resource for both identifying emerging trends in satellite constellations, and enabling technologies still requiring substantial development efforts.

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Kocifaj, M., F. Kundracik, J. C. Barentine y S. Bará. "The proliferation of space objects is a rapidly increasing source of artificial night sky brightness". Monthly Notices of the Royal Astronomical Society: Letters 504, n.º 1 (29 de marzo de 2021): L40—L44. http://dx.doi.org/10.1093/mnrasl/slab030.

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ABSTRACT The population of artificial satellites and space debris orbiting the Earth imposes non-negligible constraints on both space operations and ground-based optical and radio astronomy. The ongoing deployment of several satellite ‘mega-constellations’ in the 2020s represents an additional threat that raises significant concerns. The expected severity of its unwanted consequences is still under study, including radio interference and information loss by satellite streaks appearing in science images. In this Letter, we report a new skyglow effect produced by space objects: increased night sky brightness caused by sunlight reflected and scattered by that large set of orbiting bodies whose direct radiance is a diffuse component when observed with the naked eye or with low angular resolution photometric instruments. According to our preliminary estimates, the zenith luminance of this additional light pollution source may have already reached ∼20 $\mu$cd m−2, which amounts to an approximately 10 per cent increase over the brightness of the night sky determined by natural sources of light. This is the critical limit adopted in 1979 by the International Astronomical Union for the light pollution level not to be exceeded at the sites of astronomical observatories.

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Sampaio, J. C., A. G. S. Neto, S. S. Fernandes, R. Vilhena de Moraes y M. O. Terra. "Artificial satellites orbits in 2:1 resonance: GPS constellation". Acta Astronautica 81, n.º 2 (diciembre de 2012): 623–34. http://dx.doi.org/10.1016/j.actaastro.2012.08.025.

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Zhang, Pengfei. "Research on satellite selection algorithm in ship positioning based on both geometry and geometric dilution of precision contribution". International Journal of Advanced Robotic Systems 16, n.º 1 (1 de enero de 2019): 172988141983024. http://dx.doi.org/10.1177/1729881419830246.

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With the networking of four Global Navigation Satellite Systems, the combination of multi-constellation applications has become an inevitable trend, and there will be more and more visible satellites that can be participated in ship positioning. However, the computational complexity increases sharply, which greatly improves the load capacity of the receiver’s data processor and reduces the output frequency of the positioning result. To achieve the balance between positioning accuracy and computational complexity, a new fast satellite selection algorithm based on both of geometry and geometric dilution of precision contribution is proposed. Firstly, this article analyzes the geometry characteristics of the least visible satellites has minimum geometric dilution of precision that meet the positioning requirements and makes clear the layout of their elevation angles and azimuth angles. In addition, it derives the relationship of geometric dilution of precision and the visible satellites layout and gets geometric dilution of precision contribution of each satellite. Finally, based on the observation data of JFNG tracking station of the Multi-Global Navigation Satellite System (GNSS) Experiment trial network, the positioning error and the elapsed time of GPS/Beidou Satellite Navigation System and GPS/Beidou Satellite Navigation System/Russian Global Orbiting Navigation Satellite System (GLOANSS) are compared. Simulation results show that the algorithm solves the problem that there are a lot of matrix multiplications and matrix inversions in the traditional satellite selection algorithm, and the new algorithm can reduce computational complexity and increase receiver processing speed.

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Bonnet, Grégory y Catherine Tessier. "Evaluation d'un système multirobot. Cas d'une constellation de satellites". Revue d'intelligence artificielle 23, n.º 5-6 (10 de noviembre de 2009): 565–92. http://dx.doi.org/10.3166/ria.23.565-592.

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Schetter, Thomas, Mark Campbell y Derek Surka. "Multiple agent-based autonomy for satellite constellations". Artificial Intelligence 145, n.º 1-2 (abril de 2003): 147–80. http://dx.doi.org/10.1016/s0004-3702(02)00382-x.

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Walczak, Ken, Geza Gyuk, Andrew Kruger, Enoch Byers y Sigi Huerta. "NITESat: A High Resolution, Full-Color, Light Pollution Imaging Satellite Mission". International Journal of Sustainable Lighting 19, n.º 1 (28 de junio de 2017): 48–55. http://dx.doi.org/10.26607/ijsl.v19i1.68.

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The NITESat (Night Imaging and Tracking Experiment Satellite) mission is a 2U CubeSat satellite designed for nighttime Earth imaging to quantify and characterize light pollution across the Midwestern United States. It is accompanied and supported by an array of ground-based light pollution observing stations called GONet (Ground Observing Network). NITESat is a pilot mission testing the potential for a simple and inexpensive (<$500,000) satellite to deliver high-resolution, three-color regional data of artificial light at night. In addition, GONet will form the core of an educational outreach program by establishing an array of all-sky monitors covering the imaging region of the satellite with 20+ full sky light pollution citizen-operated stations. This will provide synchronized data coinciding with the NITESat overpasses as well as providing near continuous night sky quality monitoring. If the initial mission is a success, the potential exists to expand the program into a low cost constellation of satellites capable of delivering global coverage. NITESat is being designed, built and will be operated by the Far Horizons program at the Adler Planetarium in Chicago, Illinois. Far Horizons is a student and volunteer centered program offering hands-on engineering and scientific research opportunities for education.

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Zhu, Li Li y Yi Feng Duan. "Research on the Resource Allocation Model for the Satellite Constellation Communication System". Advanced Materials Research 121-122 (junio de 2010): 669–77. http://dx.doi.org/10.4028/www.scientific.net/amr.121-122.669.

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Satellite constellation, emerging as a new paradigm for next-generation communicating, enables large-scale application of the geographically and spatially distributed heterogeneous resources for solving problems in science, engineering, and military affairs. The resource allocation in such a large-scale distributed environment is a complex task. Due to the factors that trigger the deployment of resources in satellite constellation communication system, the artificial immune theory is applied to resource allocation field to propose the task-oriented common mathematic model about resource allocation of communication system, which is aimed at the purpose of improving the effectiveness of resource allocation and is based on the 2 important indicators that are communication task’s effectiveness factors and the degree of satisfaction in the communication system. As the immune system has characteristics of self-adaptive, self-learning and self-organization, an immune allocation algorithm that fuzzy processing time is presented by applying the immune theory to resource allocation. Simulation results show that these methods are feasible and efficient in solving the problems of resource allocation for satellite constellation communication system, and the research on this object is a meaningful exploring.

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Yalcin, I., S. Kocaman, S. Saunier y C. Albinet. "RADIOMETRIC QUALITY ASSESSMENT FOR MAXAR HD IMAGERY". International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences XLIII-B3-2021 (29 de junio de 2021): 797–804. http://dx.doi.org/10.5194/isprs-archives-xliii-b3-2021-797-2021.

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Abstract. The requirement for very high-resolution satellite imagery by different applications has been increasing continuously. Several commercial and government-supported missions provide sub-meter spatial resolutions from optical sensors aboard Earth Observation (EO) satellites. The MAXAR satellite constellation acquires images with up to 30 cm Ground Sampling Distances (GSDs); and the High-Definition (HD) image production technology developed by MAXAR doubles the resolution by using artificial intelligence methods. Although the spatial resolution is one of the most important image quality metrics, several other factors indicated by diverse radiometric and geometric characteristics may circumscribe the usability of data in different projects. As part of mandatory activities of European Space Agency (ESA), Earthnet Programme provides a framework for integrating Third-Party Missions into the overall EO strategy and promotes the international use of the data. The Earthnet Data Assessment Pilot (EDAP) project aims at assessing the quality and the suitability of TPMs, and provides a communication platform between mission providers to ensure the coherence of the systems. In this study, the radiometric quality of the MAXAR HD products was evaluated within the EDAP project framework by using several General Image-Quality Equation (GIQE) metrics, visual inspections, and comparative assessments with orthophotos obtained from an Unmanned Aerial Vehicle (UAV) platform and with the original (non-HD) orthophotos with 30 cm resolutions. The results show that the spatial resolution improvements are observable in urban areas, where sharp edges are present. However, blurring and color noise patterns also occured in the HD images.

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Vasilyev, Roman, Artem Setov, Vladimir Frolov, Konstantin Ratovsky, Aleksandr Beletsky, Aleksey Oinats, Yury Yasyukevich y Andrey Medvedev. "Modern heating facility for research into the mid-latitude ionosphere". Solnechno-Zemnaya Fizika 6, n.º 2 (27 de junio de 2020): 61–78. http://dx.doi.org/10.12737/szf-62202005.

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The development of new devices for research in physics of the upper atmosphere and near-Earth space, which can be used to carry out controlled experiments on the modification of the ionosphere by powerful short-wave radiation, is an urgent task of modern solar-terrestrial physics, space weather, operation of satellite constellations in near-Earth space, radio communications, and radar. The paper describes a modern heating facility, created within the framework of the National Heliogeophysical Complex of the Russian Academy of Sciences. We review the tasks facing the heater, discuss its main technical characteristics, and describe the capability of the observational infrastructure surrounding the heating facility. The paper justifies the long-term benefits of the development of a heating facility at middle latitudes of Eastern Siberia, which can radiate in a frequency range 2.5–6.0 MHz with an effective power of the order of several hundred megawatts. It is important that the heater will be surrounded by such multifunctional instruments as the modern incoherent scatter radar, mesostratospheric lidar, observational systems that can provide a wide range of possibilities for diagnosing artificial plasma disturbances and artificial airglow structures.

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Tesis sobre el tema "Artificial satellites Constellations"

Salazar, Kardozo Alexandros. "A High-Level Framework for the Autonomous Refueling of Satellite Constellations". Thesis, Georgia Institute of Technology, 2007. http://hdl.handle.net/1853/14534.

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Satellite constellations are an increasingly attractive option for many commercial and military applications. They provide a robust and distributed method of accomplishing the goals of expensive monolithic satellites. Among the many challenges that satellite constellations engender (challenges in control, coordination, disposal, and other areas), refueling is of particular interest because of the many methods one can use to refuel a constellation and the lifetime implications on the satellites. The present work presents a methodology for carrying out peer-to-peer refueling maneuvers within a constellation. Peer-to-peer (P2P) refueling can be of great value both in cases where a satellite unexpectedly consumes more fuel than it was alloted, and as part of a mixed refueling strategy that will include an outside tanker bringing fuel to the constellation. Without considering mixed-refueling, we formulate the peer-to-peer refueling problem as an assignment problem that seeks to guarantee that all satellites will have the fuel they need to be functional until the next refueling, while concurrently minimizing the cost in fuel that the refueling maneuvers entail. The assignment problem is then solved via auctions, which, by virtue of their distributed nature, can easily and effectively be implemented on a constellation without jeopardizing any robustness properties. Taking as a given that the P2P assignment problem has been solved, and that it has produced some matching among fuel deficient and fuel sufficient satellites, we then seek to sequence those prescribed maneuvers in the most effective manner. The idea is that while a constellation can be expected to have some redundancy, enough satellites leaving their assigned orbital slots will eventually make it impossible for the constellation to function. To tackle this problem, we define a wide class of operability conditions, and present three algorithms that intelligently schedule the maneuvers. We then briefly show how combining the matching and scheduling problems yields a complete methodology for organizing P2P satellite refueling operations.

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Budianto, Irene Arianti. "A collaborative optimization approach to improve the design and deployment of satellite constellations". Diss., Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/12384.

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Dutta, Atri. "Optimal cooperative and non-cooperative peer-to-peer maneuvers for refueling satellites in circular constellations". Diss., Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/28082.

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Thesis (M. S.)--Aerospace Engineering, Georgia Institute of Technology, 2009.
Committee Chair: Panagiotis Tsiotras; Committee Member: Eric Feron; Committee Member: Joseph Saleh; Committee Member: Ryan Russell; Committee Member: William Cook

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Du, Toit Daniel N. J. "Low Earth orbit satellite constellation control using atmospheric drag". Thesis, Link to the online version, 1997. http://hdl.handle.net/10019/2999.

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Mtshemla, Kanyisa Sipho. "Mission design of a CubeSat constellation for in-situ monitoring applications". Thesis, Cape Peninsula University of Technology, 2017. http://hdl.handle.net/20.500.11838/2633.

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Thesis (MEng (Electrical Engineering))--Cape Peninsula University of Technology, 2017.
Real-time remote monitoring of Africa’s resources, such as water quality, by using terrestrial sensors is impeded by the limited connectivity over the vast rural areas of the continent. Without such monitoring, the effective management of natural resources, and the response to associated disasters such as flooding, is almost impossible. A constellation of nanosatellites could provide near real-time connectivity with ground-based sensors that are distributed across the continent. This study evaluates the high level development of a mission design for a near real-time remote monitoring CubeSat constellation and ground segment for in-situ monitoring in regions of interest on the African continent. This would facilitate management of scarce resources using a low-cost constellation. To achieve this, the design concept and operation of a Walker constellation are examined as a means of providing connectivity to a low bit rate sensor network distributed across geographic areas of interest in South Africa, Algeria, Kenya and Nigeria. The mission requirements include the optimisation of the constellation to maintain short revisit times over South Africa and an investigation of the required communications link to perform the operations effectively. STK software is used in the design and evaluation of the constellations and the communications system. The temporal performance parameters investigated are access and revisit times of the constellations to the geographic areas mentioned. The types of constellation configurations examined, involved starting with a system level analysis of one satellite. This seed satellite has known orbital parameters. Then a gradual expansion of two to twelve satellites in one, two and three orbital planes follows. VHF, UHF and S-band communication links are considered for low data rate in-situ monitoring applications. RF link budgets and data budgets for typical applications are determined. For South Africa, in particular, a total of 12 satellites evenly distributed in a two-plane constellation at an inclination of 39° provide the optimal solution and offer an average daily revisit time of about 5 minutes. This constellation provides average daily access time of more than 16 hours per day. A case study is undertaken that decribes a constellation for the provision of maritime vessel tracking in the Southern African oceans using the Automated Information System (AIS). This service supports the Maritime Domain Awareness (MDA) initiative implemented by the South African Government, under its Operation Phakisa.
National Research Foundation (NRF) French South African Institute of Technology (F’SATI)

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Dainty, Benjamin G. "Use of two-way time transfer measurements to improve geostationary satellite navigation :". Ft. Belvoir Defense Technical Information Center, 2007. http://handle.dtic.mil/100.2/ADA472457.

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Luong, Ngoc-Dung. "Analyse d'erreurs de constellations de satellites en termes de positionnement global et d'orbitographie". Thesis, Nice, 2015. http://www.theses.fr/2015NICE4112/document.

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Grâce au développement des techniques spatiales (GNSS, DORIS, laser et le VLBI), la géodésie apporte quantité d’informations sur la forme de la Terre (sa géométrie et sa gravité), sa rotation et son orientation dans l’espace, aux échelles globales comme aux échelles régionales. L’étude des déformations de chaînes de montagne par GPS, des courants marins cartographiés par altimétrie satellitaire, des variations temporelles du champ de gravité, ainsi que l’établissement du repère de référence terrestre international, sont les exemples de l’apport de ces techniques à l’observation de la Terre et au changement global. Notre travail a pour but de faire un bilan des erreurs résiduelles de la géodésie spatiale, en séparant les causes des effets. Le but est de montrer comment les erreurs d’orbite se propagent d’abord dans la trajectoire, puis dans des produits globaux comme le repère de référence (via les mesures de poursuite de satellites) et la surface topographique (via les mesures altimétriques). Nous avons développé une approche analytique qui traite du transfert des erreurs d’origines géométrique et dynamique. En partant des équations du mouvement orbital, nous proposons une solution analytique d’ordre un du mouvement orbital circulaire, qui est appliquée pour propager les erreurs de modèle dynamique. Ensuite, les résultats sont transférés (ou projetés) sur plusieurs types de fonction de mesure : l’altimétrie, les mesures de distance et les mesures de vitesse radiale. L’originalité de ce travail tient pour beaucoup dans les méthodes purement analytiques qui ont été développées spécifiquement pour effectuer les analyses
Thanks to the development of space techniques (GNSS, DORIS, laser and VLBI) geodesy provides amount of information to determine and to study the shape of the Earth (its geometry and its gravity), its rotation and orientation in space at global scales as well as at regional scales. The study of crustal deformations by using GPS, the ocean topography by satellite altimetry, the temporal variations of the gravity field (mass transports) as well as the construction and monitoring of the International Terrestrial Reference Frame (ITRF), are some examples of the contribution of these techniques to the Earth observation including the current global change. Our work aims to separate causes and consequences. We developed a dedicated approach in which different source of errors, of geometrical and dynamical natures, are treated by analytical expressions. Starting from the dynamical satellite equation of motion, we propose to integrate and propagate the model errors and then to project the results into different measurement functions: altimetry, tracking distances and radial velocities. It results in a complex but comprehensive way that enables the propagation of prediction errors into some general geodetic products as the terrestrial reference frame or the ocean surface topography. The originality of this work lies in the development of a purely analytical method for circular orbits, which has been used to propagate errors from dynamical models. In addition, the resulting orbit errors were projected at the measurement level in order to deduce the impacts on some global geodetic products

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Bonnet, Grégory. "Coopération au sein d'une constellation de satellites". Toulouse, ISAE, 2008. http://www.theses.fr/2008ESAE0006.

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L'objectif de ces travaux est d'utiliser des liaisons intersatellites (InterSatellite Links) au sein d'une constellation de satellites d'observation autonomes en termes de planification, permettant ainsi aux satellites de communiquer entre eux et d'avoir une indépendance maximale par rapport au sol. Nous considérons donc un problème d'affectation de tâches (1) dynamique car des tâches d'observation asynchrones sont générées au cours de l'exécution, (2) distribué car chaque satellite ne connaît qu'un sous-ensemble des tâches à réaliser et (3) contraint en communication car les satellites ne peuvent communiquer que lorsque leurs orbites se croisent. Nous proposons une approche décentralisée en modélisant la constellation de satellites par un système multiagent. Chaque agent planifie individuellement, communique avec ses voisins et coopère avec eux par la suite. Pour cela, nous proposons une notion de connaissance commune et de confiance en cette connaissance fondées sur le modèle d'accointances de la constellation ainsi qu'une méthode décentralisée de formation de coalitions par référence. Cette approche coopérative a été validée expérimentalement en proposant des métriques permettant de caractériser la dimension multiagent du système. Les résultats expérimentaux montrent que notre approche permet non seulement aux constellations de satellites de réaliser plus rapidement plus de tâches d'observation mais aussi de réduire la taille des constellations mises en œuvre pour un même niveau de performance.

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Lavina, Frédérique. "Risques et responsabilités dans la mise en place et l'exploitation d'une constellation de satellites : le cas Galiléo". Montpellier 1, 2003. http://www.theses.fr/2003MON10060.

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La radionavigation par satellite permet de déterminer sa position géographique et d'acquérir une référence temporelle à partir de signaux satellitaires, où que l'on soit sur le globe. L'Europe a décidé de mettre en place une constellation sous contrôle civil, Galileo, indépendante des systèmes existants américain et russe d'origine militaire. Le programme Galileo innove à bien des égards car il proposera différents types de services : un service de base pour les applications de masse, un service commercial payant et garanti, un service destiné aux applications critiques et un service crypté pour les applications stratégiques. Mais avant de fournir ces services le système devra être conçu, construit et positionné dans l'espace. La problématique de la responsabilité est centrale dans les activités spatiales où le risque sous toutes ses formes est omniprésent. La mise en place de la constellation implique des relations contractuelles entre chacun des acteurs, processus classique de gestion des risques dans le cadre des activités spatiales. L'exploitation de la constellation implique quant à elle une multitude de questions de responsabilité liées à la couverture mondiale des services, à leurs caractéristiques techniques et à la diversité des applications pouvant utiliser ces informations. Ainsi, en dehors du cas, peu probable, d'un retour accidentel sur terre d'un des satellites de la constellation pouvant causer directement des dégâts matériels, la défaillance des satellites pourra par exemple entraîner la dégradation voire l'interruption des signaux de navigation et provoquer indirectement des dommages de grande envergure pour les utilisateurs comme pour les tiers (crashs d'avions). Cet ensemble de risques d'exploitation nécessitera une gestion adaptée des responsabilités en fonction du type d'utilisateur, du type de service utilisé et des régimes d'indemnisation existants afin de satisfaire les victimes éventuelles (utilisateurs ou tiers) tout en préservant la santé économique du système.

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Burlacu, Maria-Mihaela. "Analyse des performances et routage dans les constellations de nano-satellites : modèles et applications pour les régions éloignées". Phd thesis, Université de Haute Alsace - Mulhouse, 2010. http://tel.archives-ouvertes.fr/tel-00608660.

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La réduction des budgets du domaine spatial et les missions scientifiques traditionnelles ayant des coûts et une complexité croissants a amené la communauté scientifique à se concentrer sur les petits satellites qui fournissent non seulement des résultats scientifiques de valeur, mais permettent aussi de nouvelles applications dans le domaine de la télédétection, de la surveillance environnementale et des télécommunications. De plus, le concept de vol en formation de petits satellites est une technologie-clé pour beaucoup de missions spatiales futures, en améliorant la capacité de survie et réduisant le coût des missions. Ce travail de recherche a un double but : la proposition de modèles innovants de constellations de nano-satellites et de nouvelles approches de routage pour les réseaux de nano-satellites. Cette thèse propose et analyse trois modèles de constellations de nano-satellites dénommés NanoDREAM, NanoiCE et NanoSPHERE, qui fournissent des services de télécommunications aux régions éloignées. Le modèle NanoDREAM est conçu pour le Désert Salar de Uyuni en Bolivie, une région qui détient 70% de la réserve mondiale de lithium. Le modèle NanoiCE est destiné aux Régions Polaires, pour satisfaire les besoins de télécommunications de la communauté scientifique. Le modèle NanoSPHERE est conçu pour fournir une couverture globale de la Terre pour un marché de télécommunications concurrentiel. De plus, nous avons proposé une architecture pour le segment terrestre basée sur la technologie sans fil. Cette architecture a été déployée sur la zone d'exploitation du Désert Salar de Uyuni. Ces modèles ont été développés analytiquement et mis ensuite en œuvre dans le simulateur SaVi afin d'identifier la meilleure constellation satisfaisant les requis de la mission en terme de couverture et en réduisant au minimum le nombre de nano-satellites de la constellation. [...]

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Libros sobre el tema "Artificial satellites Constellations"

Blair, S. Birth of the European satellite navigation constellation: Galileo In-Orbit Validation. [Noordwijk, The Netherlands]: [ESA Scientific & Technical Publications Branch], 2011.

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Wei xing xing zuo li lun yu she ji: Theory and design of satellite constellations. Beijing: Ke xue chu ban she, 2008.

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der, Ha Jozef van, ed. Mission design & implementation of satellite constellations. Dordrecht: Kluwer Academic Publishers, 1998.

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Center, Goddard Space Flight y Smithsonian Astrophysical Observatory, eds. Constellation X-Ray Observatory: Unlocking the mysteries of black holes, dark matter, dark energy, and life cycles of matter in the universe. [Greenbelt, Md.]: National Aeronautics and Space Administration, Goddard Space Flight Center, 2004.

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Center, Goddard Space Flight y Smithsonian Astrophysical Observatory, eds. Constellation X-Ray Observatory: Unlocking the mysteries of black holes, dark matter, dark energy, and life cycles of matter in the universe. [Greenbelt, Md.]: National Aeronautics and Space Administration, Goddard Space Flight Center, 2004.

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Capítulos de libros sobre el tema "Artificial satellites Constellations"

Palmerini, Giovanni B. "Coordinated Orbital Control for Satellite Constellations and Formations". En Dynamics of Natural and Artificial Celestial Bodies, 415–24. Dordrecht: Springer Netherlands, 2001. http://dx.doi.org/10.1007/978-94-017-1327-6_70.

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Li, Jing, Hong-jun Hu, Pei-jun Yu y Jun Zhu. "Analysis of Requirement and Constrained Model of Inter-Satellite-Link TT&C Scheduling Problem on Navigation Constellation". En Artificial Intelligence and Computational Intelligence, 160–69. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-33478-8_21.

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Actas de conferencias sobre el tema "Artificial satellites Constellations"

Cetin, Omer y Guray Yilmaz. "Notice of Violation of IEEE Publication Principles: Artificial potential field based autonomous guidance & navigation for a planar constellation of satellites". En 2015 7th International Conference on Recent Advances in Space Technologies (RAST). IEEE, 2015. http://dx.doi.org/10.1109/rast.2015.7208321.

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