Academic literature on the topic 'Satellite'

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Journal articles on the topic "Satellite"

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Shen, Ziyu, Wenbin Shen, Xinyu Xu, et al. "A Method for Measuring Gravitational Potential of Satellite’s Orbit Using Frequency Signal Transfer Technique between Satellites." Remote Sensing 15, no. 14 (2023): 3514. http://dx.doi.org/10.3390/rs15143514.

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We introduce an approach for the direct measurement of the gravitational potential (GP) along the trajectory of a satellite, with a specific focus on Low-Earth Orbit (LEO) satellites. A LEO satellite communicates with several Geosynchronous Equatorial Orbit (GEO) satellites via frequency signal links. The GP difference can be measured in real-time using the gravitational frequency shift approach by equipping both LEO and GEO satellites with precise atomic clocks. Since the GP at the high orbits of the GEO satellites can be precisely determined by the present gravitational field model EGM2008,
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Wu, Huanqin, Maocai Wang, Zhiming Song, et al. "Random Error Analysis of Launch and Injection Positions for Distributed Multi Micro-nano Satellite System." Journal of Physics: Conference Series 2640, no. 1 (2023): 012014. http://dx.doi.org/10.1088/1742-6596/2640/1/012014.

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Abstract Accurate satellite orbit calculation has always been a focus in the aerospace field. Especially, the error distribution of the orbit involving various internal and external factors in the satellite launch process has an important influence on the effectiveness of the satellite cluster. To qualitatively and quantitatively analyze the cooperative efficiency of multi-satellite clusters involving various random errors, this paper analyzes the random error sources in the launch process of micro-nano satellites and studies the distribution law of these satellite orbit position errors. Based
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R.Sowmya. "A STUDY ON ELECTRONIC BASED ON SATELLITE COMMUNICATION SYSTEM." Shanlax International Journal of Arts, Science and Humanities 6, S2 (2019): 60–68. https://doi.org/10.5281/zenodo.2651937.

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<em>A Communications Satellite is an artificial satellite that relays and amplifies radio tele- communications signals via a transponder, it creates a communication channel between a source transmitter and a receiver at different location on Earth. Communication satellities are ysed for television, telephone, radio, internet, and military applications. Satellite Communication has moved in many steps ahead like frequency reuse, interconnecting many ground terminals spread over the world, concept of multiple spot beam communications, Laser beam based communication through satellites and use of n
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Badis, Tarek, Elhassen Benfriha, and Jalal Eddine Benmansour. "Fuel Consumption Estimation via Bookkeeping Method for Geostationary Satellites: Simple Application." International Journal of Energetica 8, no. 2 (2023): 54. https://doi.org/10.47238/ijeca.v8i2.228.

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This work focuses on the Satellite Propulsion Subsystem (UPS), a critical aspect of satellite technology that can be supported by various propulsion types: electrical, chemical, cold gas, and nuclear propulsion. For communication satellites, chemical propulsion emerges as the most suitable option due to its simplicity and lower energy requirements. The chemical propulsion subsystem comprises oxidizer and fuel tanks, gas pressuring tanks utilizing helium. Wherein, Thrusters are employed for diverse tasks, encompassing tank sinking, orbital maneuvers (correction), attitude control, and deorbitin
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Utami, Vi Bauty Riska, Imam MPB, and Shinta Romadhona. "Analysis the impact of sun outage and satellite orbit at performance of the telkom 3S satellite communication system." JURNAL INFOTEL 13, no. 3 (2021): 134–42. http://dx.doi.org/10.20895/infotel.v13i3.626.

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Satellites of communication are located at altitude of thousands kilometers above the earth's surface, so the signal is transmitted by satellite to earth station is very susceptible to interference. Every March and September equinox or when the sun crosses the Earth's equator for several days, earth station occurs a naturally interference called by sun outage. At this time, satellite and the sun reach the closest distance because satellite's position is same direction with the sun. This interference makes the signal received by earth station weaken and even disappears due to temperature noise
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Tong, Minglei, Song Li, Xiaoxiang Wang, and Peng Wei. "Inter-Satellite Cooperative Offloading Decision and Resource Allocation in Mobile Edge Computing-Enabled Satellite–Terrestrial Networks." Sensors 23, no. 2 (2023): 668. http://dx.doi.org/10.3390/s23020668.

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Mobile edge computing (MEC)-enabled satellite–terrestrial networks (STNs) can provide task computing services for Internet of Things (IoT) devices. However, since some applications’ tasks require huge amounts of computing resources, sometimes the computing resources of a local satellite’s MEC server are insufficient, but the computing resources of neighboring satellites’ MEC servers are redundant. Therefore, we investigated inter-satellite cooperation in MEC-enabled STNs. First, we designed a system model of the MEC-enabled STN architecture, where the local satellite and the neighboring satell
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Papiya, Sumaiya Janefar, Dr Bobby Barua, and Mehnaz Hossain. "Prospects Challenges of Bangabandhu Satellite-2." International Journal of Advanced Networking and Applications 14, no. 02 (2022): 5342–52. http://dx.doi.org/10.35444/ijana.2022.14204.

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The development of the Bangabandhu Satellite-1 has changed the direction of Bangladesh's satellite communication research. Bangladesh's dream project was the Bangabandhu Satellite 1. This satellite's primary goal is to maintain effective internet and communication services in remote places. First of all, we must concentrate to the depth of satellite communication system and its process to reach any conclusion. Our main goal of the research is to recognize a feasibility review on Bangabandhu satellite-2. So, for the feasibility studies we reviewed the most promising technical parts of Bangaband
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Hong, Zhenqiang, Xuxing Huang, Lifeng Yang, Zhiqiang Bian, Yong Yang, and Shuang Li. "Test Method for Single Satellite’s Inter-Satellite Link Pointing and Tracking via Ground Station." Aerospace 11, no. 9 (2024): 713. http://dx.doi.org/10.3390/aerospace11090713.

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An inter-satellite link is a key technology that improves control accuracy, transmission efficiency, and autonomous capability of constellations. A satellite’s pointing and tracking abilities mainly determine the inter-satellite link’s performance, which should be validated through an in-orbit test. However, during the construction of the constellation, the distribution of satellites does not satisfy the constraints of establishing the inter-satellite link. A test method for inter-satellite link pointing and tracking is developed with respect to a single satellite. A practical mission scenario
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Granados-Cruz, L. G., R. G. Chávez-Moreno, J. A. Ferrer-Perez, C. Romo-Fuentes, and J. A. Ramírez-Aguilar. "Historical review of simulators for satellite position and orientation control." Journal of Physics: Conference Series 2804, no. 1 (2024): 012013. http://dx.doi.org/10.1088/1742-6596/2804/1/012013.

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Abstract In the design of satellite systems, it is essential to control the satellite’s position for various reasons, either to have correct communication with a ground station or to make connections with other satellites. In the same way, the positioning of a satellite poses a significant challenge since its behavior is non-linear; due to these issues, several test benches have been developed for the satellite’s position problem. In this review, there will be a journey from the rise of the space age to the latest advances in technology for emulating the satellite’s dynamics.
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Shakila Hosseinzadeh Kondori, Mustafa Helvacı. "Satellite Temperature Modeling in Geostationary Orbit Using COMSOL." Tuijin Jishu/Journal of Propulsion Technology 44, no. 5 (2023): 127–39. http://dx.doi.org/10.52783/tjjpt.v44.i5.2440.

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In our world, communication satellites are becoming more and more significant. They are costly to create, launch, operate, and maintain, thus these costs are crucial. Due to the fact that electronic and satellite components can only operate within a limited temperature range, it is crucial to understand and manage the satellite's temperature in order to maximize efficiency both before and during the mission. This study considers GEO and comparable satellites with the goal of showing satellite temperature. We ignored the entire satellite's internal structure and focused only on the external hea
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Dissertations / Theses on the topic "Satellite"

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

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In the world of educational satellites, student teams manually conduct operations daily, sending commands and collecting downlinked data. Educational satellites typically travel in a Low Earth Orbit allowing line of sight communication for approximately thirty minutes each day. This is manageable for student teams as the required manpower is minimal. The international Global Educational Network for Satellite Operations (GENSO), however, promises satellite contact upwards of sixteen hours per day by connecting earth stations all over the world through the Internet. This dramatic increase in
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Appleby, Graham M. "Satellite laser ranging and the ETALON Geodetic satellites." Thesis, Aston University, 1996. http://publications.aston.ac.uk/13270/.

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The technique of Satellite Laser Ranging is today a mature, important tool with applications in many area of geodynamics, geodesy and satellite dynamics. A global network of some 40 stations regularly obtains range observations with sub-cm precision to more than twelve orbiting spacecraft. At such levels of precision it is important to minimise potential sources of range bias in the observations, and part of the thesis is a study of subtle effects caused by the extended nature of the arrays of retro-reflectors on the satellites. We develop models that give a precise correction of the range mea
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Sharifi, Mohammad A. "Satellite gradiometry using a satellite pair." [S.l. : s.n.], 2004. http://www.bsz-bw.de/cgi-bin/xvms.cgi?SWB11406716.

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Score, Robert H. "An examination of XM satellite subscriber's perceptions of satellite radio compared to traditional AM/FM radio." Instructions for remote access. Click here to access this electronic resource. Access available to Kutztown University faculty, staff, and students only, 2002. http://www.kutztown.edu/library/services/remote_access.asp.

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Thesis (M.S.)--Kutztown University of Pennsylvania, 2002.<br>Source: Masters Abstracts International, Volume: 45-06, page: 2720. Typescript. Abstract precedes thesis as preliminary leaves 1-2. Includes bibliographical references (leaves 34-35).
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Morimoto, Todd A., Thomas E. Nowitzky, and Steven A. Grippando. "OPERATING A LIGHTWEIGHT, EXPENSIVE LOW EARTH ORBITING SATELLITE." International Foundation for Telemetering, 1994. http://hdl.handle.net/10150/608842.

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International Telemetering Conference Proceedings / October 17-20, 1994 / Town & Country Hotel and Conference Center, San Diego, California<br>An increasing number of satellite users and manufacturers are looking to lightweight, inexpensive satellites as substitutes to traditional large, expensive satellites with multiple payloads. Neither the Department of Defense nor the commercial sector can bear the financial or reputational consequences associated with massive program failures. With the low cost and weight of these new satellites, users can achieve mission success without great risk.
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Zaheer, Muhammad. "Kinematic orbit determination of low Earth orbiting satellites, using satellite-to-satellite tracking data and comparison of results with different propagators." Thesis, KTH, Geodesi och geoinformatik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-142627.

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The GPS data from Challenging Mini-satellite Payload (CHAMP) is used for its orbit determination for the epoch day of January 1st 2002.  The orbit of CHAMP is computed from the GPS data and ionospheric effects are removed by frequency combination. Further, the orbits of CHAMP for the same epoch day are computed using the satellite tool kit (STK) employing simplified general perturbations (SGP4) and a high precision orbit propagator (HPOP). Results from both techniques (GPS computed orbit and STK computed orbit) are compared. Furthermore, orbits computed using GPS data are also compared with j
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Xi, Xiaojin. "Analytical representation for ephemeris with short time-span : application to the longitude of Titan." Thesis, Paris Sciences et Lettres (ComUE), 2018. http://www.theses.fr/2018PSLEO015/document.

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Les éphémérides issues d'intégrations numériques qui peuvent être facilement téléchargées des sites de l'IMCCE ou du JPL, ont une très bonne précision pour les observations récentes. En même temps, un autre type d'éphémérides, celles analytiques comme TASS, décrivent en détail le système dynamique par une représentation en combinaison de fréquences propres. Notre but est d'associer ces deux types d'éphémérides pour l'utiliser dans les études de la rotation des satellites naturelles. Cela signifie qu'il faut reconstruire des éphémérides à long terme et de haute précision montrant les caractéris
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Wolf, Robert. "Satellite orbit and ephemeris determination using inter satellite links." [S.l.] : [s.n.], 2001. http://deposit.ddb.de/cgi-bin/dokserv?idn=961611820.

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Bezuidenhout, Quintus. "Satellite communications strategy selection for optimal LEO satellite communication." Thesis, Stellenbosch : Stellenbosch University, 2012. http://hdl.handle.net/10019.1/71930.

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Thesis (MScEng)--Stellenbosch University, 2012.<br>ENGLISH ABSTRACT: A low earth orbit satellite system can be useful in numerous communication applications where physical connections are not possible. Communication time available from any point on earth to the satellite is less than one hour per day. This one hour is fragmented into smaller time slots due to the satellite orbiting. This is not much time to transfer data and there is even less time available to transfer data when there are other external factors affecting the system. It is thus crucial to optimise the satellite communicat
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Sharifi, Mohammad A. "Satellite to satellite tracking in the space-wise approach." [S.l. : s.n.], 2006. http://nbn-resolving.de/urn:nbn:de:bsz:93-opus-28337.

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Books on the topic "Satellite"

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Stefan, Kalmár, Museum für Gegenwartskunst Zürich, and Consortium (Art center : Dijon, France), eds. Satellite. Museum für Gegenwartskunst, 1998.

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Committe, International Radio Consultative. Handbook: Satellite communications : fixed-satellite service. International Telecommunication Union, 1988.

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International Radio Consultative Committee., ed. Handbook, satellite communications: Fixed-satellite service. International Telecommunication Union, 1988.

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Roddy, Dennis. Satellite communications. Prentice Hall, 1989.

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Gagliardi, Robert M. Satellite communications. Van Nostrand Reinhold, 1985.

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Maini, Anil K., and Varsha Agrawal. Satellite Technology. John Wiley & Sons, Ltd, 2010. http://dx.doi.org/10.1002/9780470711736.

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Ahmad, Latief, and Syed Sheraz Mahdi. Satellite Farming. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-030-03448-1.

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Gagliardi, Robert M. Satellite Communications. Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-010-9760-4.

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Maini, Anil K., and Varsha Agrawal, eds. Satellite Technology. John Wiley & Sons Ltd, 2014. http://dx.doi.org/10.1002/9781118636459.

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Montenbruck, Oliver, and Eberhard Gill. Satellite Orbits. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-58351-3.

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Book chapters on the topic "Satellite"

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Ashraf, Amir, and Mostafa Mohamed. "Thermal Control and Analysis of a 3U Nanosatellite with Deployed Panels." In Springer Proceedings in Physics. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-3276-3_9.

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Abstract The success of a satellite mission depends on a lot of factors. The satellite thermal control system (TCS) is one of the most important subsystems that ensures that the satellite’s components remain within an acceptable temperature range. Thermal control for satellites includes monitoring the energy that flows into and out of the spacecraft. This monitoring helps to prevent overheating or freezing of critical components. To execute satellite thermal modeling, the mathematical model must be solved while accounting for both the heat rejected out of the internal electrical components of
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Pelton, Joseph N. "Satellite Orbits for Communications Satellites." In Handbook of Satellite Applications. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4419-7671-0_5.

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Pelton, Joseph N. "Satellite Orbits for Communications Satellites." In Handbook of Satellite Applications. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-23386-4_5.

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Pelton, Joseph N. "Satellite Orbits for Communications Satellites." In Handbook of Satellite Applications. Springer New York, 2015. http://dx.doi.org/10.1007/978-1-4614-6423-5_5-3.

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Inglis, Andrew F. "Satellite Program Distribution Geosynchronous Satellites." In Behind the Tube. Routledge, 2023. http://dx.doi.org/10.4324/9781003454601-8.

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Marjoribanks, Roger. "satellite images Satellite Imagery." In Geological Methods in Mineral Exploration and Mining. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-540-74375-0_8.

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Weik, Martin H. "satellite." In Computer Science and Communications Dictionary. Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_16581.

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Smith, Michael G. "Satellite." In The Spacefaring Earth. Routledge, 2024. http://dx.doi.org/10.4324/9781003494409-6.

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Maitra, Amit, and Joseph N. Pelton. "Mobile Satellite Communications and Small Satellites." In Handbook of Small Satellites. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-20707-6_38-1.

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Maitra, Amit, and Joseph N. Pelton. "Mobile Satellite Communications and Small Satellites." In Handbook of Small Satellites. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-36308-6_38.

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Conference papers on the topic "Satellite"

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Gopal, Vignesh, Asher Novick, Xinzhou Su, et al. "Fully Reconfigurable Silicon Photonic Transceiver for Optical Inter-Satellite Links." In Optical Fiber Communication Conference. Optica Publishing Group, 2025. https://doi.org/10.1364/ofc.2025.m3d.3.

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Over the past two decades, LEO satellites have rapidly proliferated, fragmenting communication protocols. We propose a reconfigurable silicon-photonic link enabling versatile modulation formats to promote seamless interoperability and efficiency in inter-satellite communications. Full-text article not available; see video presentation
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Spoelstra, T. A. Th. "Oh Satellite, Oh Satellite!" In EMC_2000_Wroclaw. IEEE, 2000. https://doi.org/10.23919/emc.2000.10842081.

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Specht, Cezary, and Paweł Dąbrowski. "Runaway PRN11 GPS satellite." In Environmental Engineering. VGTU Technika, 2017. http://dx.doi.org/10.3846/enviro.2017.244.

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The paper discusses the position of the orbit of PRN11 GPS satellite. Visual analysis of the current GPS constellation showed considerable deviation of PRN11 GPS satellite orbital parameters relative to other orbital plane D satellites. Short comparison of available GPS almanac format was included. Two almanacs per year since the launch of the PRN11 satellites in 1999 were obtained. Parameters of right ascension of ascending node and rate of right ascension of ascending node were taken into investigation. The results confirmed the fact of constant and progressive separation of the orbit from h
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Yun, Sang-Hyuk, Hyo-Sung Ahn, Sun-Ju Park, Ok-Chul Jung, and Dae-Won Chung. "Ground Antenna Scheduling Algorithm for Multi-Satellite Tracking." In ASME 2011 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/detc2011-48042.

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In this paper, we address the optimal ground antenna scheduling problem for multiple satellites when multiple satellites have visibility conflicts at a ground station. Visibility conflict occurs when multiple satellites have either overlapping visibilities at a ground station or difference with time of loss of signal (LOS) of a satellite and time of acquisition of signal (AOS) of another satellite is less than reconfiguration time of ground station. Each satellite has a priority value that is a weight function with various factors. Multi-antenna scheduling (MAS) algorithm 1 and Multi-antenna s
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Senes, Maxime, Kristen Lagadec, Baptiste Brault, and Bertrand Raffier. "A Passive Device for Postmortem Detumbling/Antitumbling of LEO Satellites, to Facilitate Active Removal." In ESA 12th International Conference on Guidance Navigation and Control and 9th International Conference on Astrodynamics Tools and Techniques. ESA, 2023. http://dx.doi.org/10.5270/esa-gnc-icatt-2023-093.

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To limit the risk of cascading collisions, we will need active debris removal missions to retrieve satellites that die before they can be deorbited. It is well understood that sudden fatal failures can cause a dead satellite to tumble uncontrollably, but it also happens that even properly decommissioned satellites are not immune to spontaneous self-tumbling due to momentum buildup from solar radiation pressure torque, making removal much more challenging. The availability of a detumbling/antitumbling device ensuring passive stabilization of dead satellites could greatly reduce the risk and cos
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McMullen, Matthew G., Tamara Alexander, and Adam Huang. "Small Satellite Formations via Higher Velocity Deployment." In ASME 2010 International Mechanical Engineering Congress and Exposition. ASMEDC, 2010. http://dx.doi.org/10.1115/imece2010-40010.

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Small satellites can be constructed at a fraction of the cost of a full-size satellite. One full-size satellite can be replaced with a multitude of small satellites, which offers a benefit in covering more area at the same time, achievable through formations. However, the shortcoming to the smaller size is usually a lack of thrusting capabilities. Furthermore, current designs for small satellite deployment mechanisms are only capable of low deployment velocities (on the order of meters per second). Prior research in using a pneumatic launcher shows that it is possible to achieve higher deploym
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Paul, Johns, Abdul Salam PM, Rajeev P, Santhosh J. Nalluveettil, and Jothiramalingam A. "Development of INLS 3U Uni-Pod Nano Satellite (CubeSat) Dispenser System for 3U Class Satellites." In AeroCON 2024. SAE International, 2024. http://dx.doi.org/10.4271/2024-26-0458.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;With the present state of the art technology, size and mass of the satellites have come down. This necessitated the need for a low shock separation system that does not have mass attached to the separated satellite. Development of Nano satellites with mass of the order of 1 to 24 kg has become popular among scientific/ academic institutions for carrying out scientific experiments. INLS 3U Uni-Pod System (Nano satellite dispenser system) is a satellite dispensing system designed by ISRO for accommodating four 3U class Nan
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Meng, Jingxiong, Yan Chen, and Junfeng Zhao. "Simulator Development for Vehicle Localization Using Low Earth Orbit Satellites." In WCX SAE World Congress Experience. SAE International, 2024. http://dx.doi.org/10.4271/2024-01-2846.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;This paper investigates the utilization of Low Earth Orbit (LEO) satellites for vehicle localization and conducts a comparative analysis with traditional Global Navigation Satellite Systems (GNSS)-based methods. With the rise of LEO satellite constellations, such as Starlink, LEO-based vehicle localization may offer solutions to GNSS-related challenges. With a large number of satellites and short communication distance, the LEO-based method has great potential to improve accuracy, reduce warm-up time, and provide a robus
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Adam, Steve, and Mike Farrell. "High Resolution Satellite Imagery: From Spies to Pipeline Management." In 2000 3rd International Pipeline Conference. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/ipc2000-152.

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In the past, high resolution satellite imagery was the domain of national security organizations. However, this has recently changed with the launch of Space Imaging’s IKONOS satellite. Launched on September 24, 1999 it is the world’s first commercial high resolution satellite, collecting data at 1-meter black/white and 4-meter multi-spectral. 2000 has the scheduled launch of at least two more commercial high resolution satellites. If these satellites are successfully launched, a buyer will be able to acquire imagery every day of the year (barring cloud cover). As an added convenience, an imag
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Kumar Maurya, Ashutosh, Uma Yadav, Mukesh Kumar, and Javalkar Dinesh Kumar. "Developing and deploying a satellite communication ground station: Design and Implementation." In International Conference on Cutting-Edge Developments in Engineering Technology and Science. ICCDETS, 2024. http://dx.doi.org/10.62919/gsaa7128.

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Amidst the proliferation of satellites encircling the Earth, the establishment of an extensive ground station network assumes paramount importance for effective reception of satellite-transmitted data. This paper delves into the intricacies surrounding the deployment of a ground station tailored for Low Earth Orbit (LEO) satellites, situated in Suceava city. It outlines a straightforward and economical ground station solution while showcasing a practical demonstration of satellite data reception. Given the urban setting of the ground station and the utilization of omnidirectional antennas, the
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Reports on the topic "Satellite"

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Schug, Klaus. Satellite Local Area Network Inter-Satellite Link. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada387200.

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COLORADO UNIV AT BOULDER. Satellite Oceanography. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada277286.

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Hansen, Elaine, Dave Beckwith, Brian Egaas, Steve Levin-Stankevich, and Jennifer Michels. Three Corner Satellite. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada410043.

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Horan, Stephen. 3 Corner Satellite. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada410185.

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Danielson, D. A., C. P. Sagovac, B. Neta, and L. W. Early. Semianalytic Satellite Theory. Defense Technical Information Center, 1995. http://dx.doi.org/10.21236/ada531136.

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BACCELLI, François, Sébastien CANDEL, Guy PERRIN, and Jean-Loup PUGET. Large Satellite Constellations: Challenges and Impact. Académie des sciences, 2024. http://dx.doi.org/10.62686/3.

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The New Space Age (NewSpace) marks the advent of a new era in the use of space, characterized by the opening of space to new players, the use of new space technologies, new functionalities for satellites in orbit, and the development of satellite constellations, mainly in the fields of communications and Earth observation. These developments are underpinned by first-rate scientific and technological advances, as well as considerable public and private investment, in particular in the USA, China and, to a lesser extent, Europe. Fleets of small low- and medium-orbit satellites are replacing or c
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España Fontán, Paula, and Maria Angeles Gomez Flechoso. Effects of the orbit orientation on the evolution of dwarf satellite galaxies. Fundación Avanza, 2023. http://dx.doi.org/10.60096/fundacionavanza/2492022.

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Cosmological models propose a hierarchical scenario for galaxy evolution, where dwarf galaxies are accreted in the halo of larger ones. We study the effect of the satellite’s orbital orientation on the planar alignment of satellite galaxies.
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Schultz, J. F., S. J. Czuchlewski, and C. R. Quick. Satellite-based laser windsounder. Office of Scientific and Technical Information (OSTI), 1997. http://dx.doi.org/10.2172/549682.

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

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Counselman, C. C. Millimeter-Accuracy Satellite Navigation. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/ada237736.

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