Relevant bibliographies by topics / Picosatellite

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

Academic literature on the topic 'Picosatellite'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 February 2022

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Journal articles on the topic "Picosatellite"

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Lokman, Abdul Halim, Ping Jack Soh, Saidatul Norlyana Azemi, Herwansyah Lago, Symon K. Podilchak, Suramate Chalermwisutkul, Mohd Faizal Jamlos, Azremi Abdullah Al-Hadi, Prayoot Akkaraekthalin, and Steven Gao. "A Review of Antennas for Picosatellite Applications." International Journal of Antennas and Propagation 2017 (2017): 1–17. http://dx.doi.org/10.1155/2017/4940656.

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Cube Satellite (CubeSat) technology is an attractive emerging alternative to conventional satellites in radio astronomy, earth observation, weather forecasting, space research, and communications. Its size, however, poses a more challenging restriction on the circuitry and components as they are expected to be closely spaced and very power efficient. One of the main components that will require careful design for CubeSats is their antennas, as they are needed to be lightweight, small in size, and compact or deployable for larger antennas. This paper presents a review of antennas suitable for p
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LaBerteaux, Jason, Jason Moesta, and Blaise Bernard. "Advanced Picosatellite Experiment." IEEE Aerospace and Electronic Systems Magazine 24, no. 9 (September 2009): 4–9. http://dx.doi.org/10.1109/maes.2009.5282283.

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Vertat, Ivo, and Ales Vobornik. "Efficient and Reliable Solar Panels for Small CubeSat Picosatellites." International Journal of Photoenergy 2014 (2014): 1–8. http://dx.doi.org/10.1155/2014/537645.

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CubeSat picosatellites have a limited area of walls for solar cells assembling and the available area has to be effectively shared with other parts, such as planar antennas, optical sensors, camera lens, and access port. With standard size of solar cell strings, it is not possible to construct a reliable solar panel for CubeSat with redundant strings interconnection. Typical solar panels for CubeSat consist of two solar cell strings serially wired with no redundancy in case of solar string failure. The loss of electric energy from one solar panel can cause a serious problem for most picosatell
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Céspedes, Jorge Enrique Salamanca, and Roberto Ferro Escobar. "Diseño e Implementacion de un Modulo de Gestion de Energia para un Pico-Satelite Tipo Cubesat." KnE Engineering 3, no. 1 (February 11, 2018): 913. http://dx.doi.org/10.18502/keg.v3i1.1512.

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This article briefly describes the development of Power Module for Experimental picosatellite CubeSat UD Colombia 1 following CubeSat standard requirements. Whether the Power Module project consists of four stages of development: study, design, implementation and testing. In the study phase to review the theoretical framework and preliminary designs made in the Universidad Distrital and other CubeSat developed in the world, also investigates existing components and technologies in the market. The design phase involves analysis of the system and using a computer program designed to generate the
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Wermuth, Martin, Gabriella Gaias, and Simone D’Amico. "Safe Picosatellite Release from a Small Satellite Carrier." Journal of Spacecraft and Rockets 52, no. 5 (September 2015): 1338–47. http://dx.doi.org/10.2514/1.a33036.

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Scholz, A., W. Ley, B. Dachwald, J. J. Miau, and J. C. Juang. "Flight results of the COMPASS-1 picosatellite mission." Acta Astronautica 67, no. 9-10 (November 2010): 1289–98. http://dx.doi.org/10.1016/j.actaastro.2010.06.040.

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Yao, J. Jason, Charles Chien, Robert Mihailovich, Viktor Panov, Jeffrey DeNatale, Judy Studer, Xiaobin Li, Anhua Wang, and Sangtae Park. "Microelectromechanical system radio frequency switches in a picosatellite mission." Smart Materials and Structures 10, no. 6 (November 28, 2001): 1196–203. http://dx.doi.org/10.1088/0964-1726/10/6/308.

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Arnon, Shlomi, and Debbie Kedar. "Sensing and communication trade-offs in picosatellite formation flying missions." Journal of the Optical Society of America A 26, no. 10 (September 3, 2009): 2128. http://dx.doi.org/10.1364/josaa.26.002128.

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Fadlie Sabri, Sharizal, Nor'Asnilawati Salleh, and Elena Woo Lai Leng. "Designing and Developing a Ground Operation Software for Picosatellite Operation and Data Processing." Applied Mechanics and Materials 225 (November 2012): 475–80. http://dx.doi.org/10.4028/www.scientific.net/amm.225.475.

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Ground operation software (GOS) plays an important role in satellite operations. The software need to be able to retrieve, decode, display and archive the telemetry data as well as send command to control the satellite. These are mandatory functions which will allow satellite operators to communicate and command the satellite in ensuring its mission is executed as designed. Researchers in Agensi Angkasa Negara (ANGKASA) are currently developing a picosatellite as a research project using various Commercial Off-The-Shelf (COTS) components. Even the software algorithm and coding are being develo
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Reichel, F., P. Bangert, S. Busch, K. Ravandoor, and K. Schilling. "The Attitude Determination and Control System of the Picosatellite UWE-3*." IFAC Proceedings Volumes 46, no. 19 (2013): 271–76. http://dx.doi.org/10.3182/20130902-5-de-2040.00088.

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Dissertations / Theses on the topic "Picosatellite"

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Pignatelli, David. "Improving and Expanding the Capabilities of the Poly-Picosatellite Orbital Deployer." DigitalCommons@CalPoly, 2014. https://digitalcommons.calpoly.edu/theses/1312.

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The Poly-Picosatellite Orbital Deployer (P-POD) has undergone a series of revisions over the years. The latest revision, described in this Master’s Thesis, incorporates new capabilities like EMI shielding, an inert gas purge system, and an electrical interface to the CubeSats after they are integrated into the P-POD. Additionally, some mass reduction modifications are made to the P-POD, while its overall strength is increased. The P-POD inert gas purge system successfully flew, on a previous revision P-POD. The P-POD components are analyzed to a set of dynamic loads for qualification, and succ
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Chiew, Jingyi. "Modelling of picosatellite constellation-based network and effects on quality of service." Thesis, Monterey, California: Naval Postgraduate School, 2015. http://hdl.handle.net/10945/45168.

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Approved for public release; distribution is unlimited<br>The military applications for miniature, low-cost satellites that could be quickly launched to provide ad-hoc tactical networks have risen in recent years. Currently, the smallest practical variant of these miniaturized satellites is known as the picosatellite. In order to evaluate the performance of the picosatellite constellation-based network, a model that can accurately simulate the orbital physics of the constellation as well as the satellite-to-ground communication links and data traffic is necessary. The focus of this thesis was
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Bowen, John Arthur. "On-Board Orbit Determination and 3-Axis Attitude Determination for Picosatellite Applications." DigitalCommons@CalPoly, 2009. https://digitalcommons.calpoly.edu/theses/131.

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This thesis outlines an orbit determination and 3-axis attitude determination system for use on orbit as applicable to 1U CubeSats and other picosatellites. The constraints imposed by the CubeSat form factor led to the need for a simple configuration and relaxed accuracy requirements. To design a system within the tight mass, volume, and power constraints inherent to CubeSats, a balance between hardware complexity, software complexity and accuracy is sought. The proposed solution consists of a simple orbit propagator, magnetometers with a magnetic field look-up table, Sun sensors with an analy
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Orozco, Gina. "BASELINE COMMUNICATIONS SYSTEM FOR A SMALL SATELLITE." International Foundation for Telemetering, 2003. http://hdl.handle.net/10150/605374.

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International Telemetering Conference Proceedings / October 20-23, 2003 / Riviera Hotel and Convention Center, Las Vegas, Nevada<br>The NMSUSat is part of the AFRL/NASA University Nanosatellite program. The constellation will consist of a main microsatellite that will have a command link from ground and a telemetry link to ground while a picosatellite will act as a sensor reporting data to the microsatellite. Innovative command and data handling will be incorporated at low cost and greater accessibility. In this paper we present the necessary communications and control architecture for the
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Foley, Justin Dean. "Calibration and Characterization of Cubesat Magnetic Sensors Using a Helmholtz Cage." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/903.

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Small satellites, and CubeSats in particular, have quickly become a hot topic in the aerospace industry. Attitude determination is currently one of the most intense areas of development for these miniaturized systems and future Cal Poly satellite missions will depend heavily on magnetometers. In order to utilize magnetometers as a viable source of attitude knowledge, precise calibration is required to ensure the greatest accuracy achievable. This paper outlines a procedure for calibrating and testing magnetometers on the next generation of Cal Poly CubeSates, utilizing a Helmholtz cage to s
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Koritza, Trevor Joseph. "STORE AND FORWARD ROUTING FOR SPARSE PICO-SATELLITE SENSOR NETWORKS WITH DATA-MULES." DigitalCommons@CalPoly, 2009. https://digitalcommons.calpoly.edu/theses/104.

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Satellites are playing an increasingly important role in collecting scientific information, providing communication services, and revolutionizing navigation. Until recently satellites were large and very expensive, creating a high barrier to entry that only large corporations and government agencies could overcome. In the past few years the CubeSat project at California Polytechnic University in San Luis Obispo (Cal Poly) has worked to refine the design and launching of small, lightweight, and less expensive satellites called pico-satellites, opening space up to a wider audience. Now that Cal
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Giesselmann, Jens Uwe Michael, and jens giesselmann@gmx net. "Development of an Active Magnetic Attitude Determination and Control System for Picosatellites on highly inclined circular Low Earth Orbits." RMIT University. Aerospace, Mechanical and Manufacturing Engineering, 2006. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20070514.162516.

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Small satellites are becoming increasingly important to the aerospace industry mainly due to their significantly reduced development and launch cost as well as shorter development time frames. In order to meet the requirements imposed by critically limited resources of very small satellites, e.g. picosatellites, innovative approaches have to be taken in the design of effective subsystem technologies. This thesis presents the design of an active attitude determination and control system for flight testing on-board the picosatellite 'Compass-1' of the University of Applied Sciences Aachen, Germa
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Loubser, Hanco Evert. "The development of Sun and Nadir sensors for a solar sail CubeSat." Thesis, Stellenbosch : University of Stellenbosch, 2011. http://hdl.handle.net/10019.1/6748.

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Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2011.<br>ENGLISH ABSTRACT: This thesis describes the development of attitude sensors required for the Attitude Determination and Control System (ADCS) for a Cubesat. The aim is to find the most suitable sensors for use on a small picosatellite by implementing miniaturised sensors with available commercial-off-the-shelf (COTS) technology. Specifically, the algorithms, hardware prototypes, software and filters required to create accurate sensors to determine the 3-axis orientation of a CubeSat are discussed.
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Whalen, William D. "ADAPTIVE COMPONENT USAGE FOR THE THERMAL MANAGEMENT OF PICOSATELLITES." DigitalCommons@CalPoly, 2011. https://digitalcommons.calpoly.edu/theses/563.

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The CubeSat standard originated in 1999. It was a joint development led by Dr. Jordi Puig-Suari of California State Polytechnic University San Luis Obispo and Professor Robert Twiggs of Stanford University. The engineering challenges that have come from this picosatellite class have created incredible educational opportunities for engineering students throughout the world. Since the challenges of engineering a CubeSat abound the designers are always looking at novel and even revolutionary solutions to each one. One of those opportunities is in thermal subsystem design, implementation and ch
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Wolf, Ronny [Verfasser], Klaus [Gutachter] Brieß, Hakan [Gutachter] Kayal, and Andreas [Gutachter] Bardenhagen. "Thermalkontrollsystem mit Latentwärmespeicher für Picosatelliten / Ronny Wolf ; Gutachter: Klaus Brieß, Hakan Kayal, Andreas Bardenhagen." Berlin : Technische Universität Berlin, 2021. http://d-nb.info/1235523012/34.

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Books on the topic "Picosatellite"

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Diy Satellite Platforms Building A Spaceready General Base Picosatellite For Any Mission. O'Reilly Media, 2012.

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Rankin, Daniel John Paul. Integration, testing, and operations of the CanX-1 picosatellite and the design of the CanX-2 attitude determination and control system. 2004.

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Temperature regulation of electronic equipment in the picosatellites. Space Colonization Journal, Vol. 4, 2013. Space Robotics Corporation Limited, 2013.

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Book chapters on the topic "Picosatellite"

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Michelena, M. D. "Commercial Off-The-Shelf GMR Based Sensor on Board Optos Picosatellite." In Giant Magnetoresistance (GMR) Sensors, 181–210. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-37172-1_8.

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"Picosatellite Power System Design." In Emergence of Pico- and Nanosatellites for Atmospheric Research and Technology Testing, 227–38. Reston ,VA: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/5.9781600867699.0227.0238.

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"Micro/Nano/Picosatellite-Activities: Challenges towards Space Education and Utilisation." In Small Satellites, 5–27. Brill | Nijhoff, 2016. http://dx.doi.org/10.1163/9789004312234_003.

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"PowerSphere Development—An Example in Using Gossamer Technology on Picosatellites." In Emergence of Pico- and Nanosatellites for Atmospheric Research and Technology Testing, 109–24. Reston ,VA: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/5.9781600867699.0109.0124.

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Conference papers on the topic "Picosatellite"

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LaBerteaux, Jason, Jason Moesta, and Blaise Bernard. "Cajun advanced picosatellite experiment." In 2007 IEEE/AIAA 26th Digital Avionics Systems Conference. IEEE, 2007. http://dx.doi.org/10.1109/dasc.2007.4391943.

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"Picosatellite Technologies and Operation Concepts." In 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.iac-04-iaa.4.11.6.09.

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Rausch, William D., Lloyd E. Hartshorn, Alan Rendon, and Alan Kitrell. "CUBESAT: a dual-mission picosatellite." In International Symposium on Optical Science and Technology, edited by Brian J. Horais and Robert J. Twiggs. SPIE, 2000. http://dx.doi.org/10.1117/12.406653.

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Fiala, P., and A. Vobornik. "Embedded microcontroller system for PilsenCUBE picosatellite." In 2013 IEEE 16th International Symposium on Design and Diagnostics of Electronic Circuits & Systems (DDECS). IEEE, 2013. http://dx.doi.org/10.1109/ddecs.2013.6549804.

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Vladimirova, T., Xiaofeng Wu, A. H. Jallad, and C. P. Bridges. "Distributed Computing in Reconfigurable Picosatellite Networks." In 2007 2nd NASA/ESA Conference on Adaptive Hardware and Systems. IEEE, 2007. http://dx.doi.org/10.1109/ahs.2007.44.

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Dudacek, Karel, and Petr Mayr. "Experimental Payload for the PilsenCube Picosatellite." In 2018 International Conference on Applied Electronics (AE). IEEE, 2018. http://dx.doi.org/10.23919/ae.2018.8501442.

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Vladimirova, T., Xiaofeng Wu, K. Sidibeh, D. Barnhart, and A. Jallad. "Enabling Technologies for Distributed Picosatellite Missions in LEO." In First NASA/ESA Conference on Adaptive Hardware and Systems. IEEE, 2006. http://dx.doi.org/10.1109/ahs.2006.33.

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Young-Keun Chang, Je-Hong Park, Young-Hyun Kim, Byoung-Young Moon, and Myung-Il Min. "Design and development of HAUSAT-1 picosatellite system (CubeSat)." In Proceedings of International Conference on Recent Advances in Space Technologies. IEEE, 2003. http://dx.doi.org/10.1109/rast.2003.1303389.

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Williams, Trevor, and Zhong-Sheng Wang. "Potential non-propulsive stationkeeping techniques for picosatellite formation flight." In Astrodynamics Specialist Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4134.

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Arslan, Tughrul, Erfu Yang, Nakul Haridas, Alicia Morales, Ahmed O. El-Rayis, Ahmet T. Erdogan, and Adrian Stoica. "An adaptive approach to space-based picosatellite sensor networks." In SPIE Defense, Security, and Sensing, edited by Teresa H. O'Donnell, Misty Blowers, and Kevin L. Priddy. SPIE, 2009. http://dx.doi.org/10.1117/12.820792.

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Reports on the topic "Picosatellite"

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Tethered Picosatellites: A First Step towards Electrodynamic Orbital Control and Power Generation. Purdue University, August 2018. http://dx.doi.org/10.5703/1288284316842.

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