Academic literature on the topic 'Satellite Command and Data Handling'

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Journal articles on the topic "Satellite Command and Data Handling"

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bin Ibrahim, Syahrim Azhan, Sharizal Fadlie Sabri, and Nor'Asnilawati Salleh. "Preliminary Hardware Design and Development of On-Board Data Handling for Pico-Satellite in National Space Agency." Applied Mechanics and Materials 225 (November 2012): 492–96. http://dx.doi.org/10.4028/www.scientific.net/amm.225.492.

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Malaysia had in the past sent two remote sensing satellites to orbit by collaborating with foreign space companies to build homegrown capacities for space technology development. At the educational institutions, a pico-satellite development program would be an ideal first step to establish such capacity as students could gain the experience and know-how through the complete cycle of designing, building and testing a satellite. As it is now, some of their overseas counterparts have already succeeded in running CubeSat programs due to strong support from kit manufacturers and their national space agencies. However, the cost to purchase such kits could be discouraging and National Space Agency (ANGKASA) recognises the needs to initiate some designs that could be used or referred to for further development or expansion. In this paper, a hardware design of On-Board Data Handling (OBDH) board using PIC Microcontroller is presented. OBDH is a main subsystem which controls all subsystems in the satellite. It provides a series of important services like command, telemetry, data communication, data acquisition, process, storage and management. The PIC Microcontroller made by Microchip Corporation is chosen as it is widely used by the industry and academia in Malaysia. The 16-bit PIC24 microcontroller has been recognized as a suitable part due to its performance, memory, peripherals, cost effective solutions as well as availability. The method used in designing the OBDH in this pico-satellite is first based on a main mission to investigate ionospheric effect on GPS signal transmission. Other considerations taken are that the parts used should be of commercial off the shelf product and having its own development board for ease of testing. The expected result would be the successful arrangement of all required parts in limited pico-satellite’s size and the accomplishment in achieving the satellite’s missions through simulation.
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Tecuapetla-Gómez, Inder, Gerardo López-Saldaña, María Isabel Cruz-López, and Rainer Ressl. "TATSSI: A Free and Open-Source Platform for Analyzing Earth Observation Products with Quality Data Assessment." ISPRS International Journal of Geo-Information 10, no. 4 (April 16, 2021): 267. http://dx.doi.org/10.3390/ijgi10040267.

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Earth observation (EO) data play a crucial role in monitoring ecosystems and environmental processes. Time series of satellite data are essential for long-term studies in this context. Working with large volumes of satellite data, however, can still be a challenge, as the computational environment with respect to storage, processing and data handling can be demanding, which sometimes can be perceived as a barrier when using EO data for scientific purposes. In particular, open-source developments which comprise all components of EO data handling and analysis are still scarce. To overcome this difficulty, we present Tools for Analyzing Time Series of Satellite Imagery (TATSSI), an open-source platform written in Python that provides routines for downloading, generating, gap-filling, smoothing, analyzing and exporting EO time series. Since TATSSI integrates quality assessment and quality control flags when generating time series, data quality analysis is the backbone of any analysis made with the platform. We discuss TATSSI’s 3-layered architecture (data handling, engine and three application programming interfaces (API)); by allowing three APIs (a native graphical user interface, some Jupyter Notebooks and the Python command line) this development is exceptionally user-friendly. Furthermore, to demonstrate the application potential of TATSSI, we evaluated MODIS time series data for three case studies (irrigation area changes, evaluation of moisture dynamics in a wetland ecosystem and vegetation monitoring in a burned area) in different geographical regions of Mexico. Our analyses were based on methods such as the spatio-temporal distribution of maxima over time, statistical trend analysis and change-point decomposition, all of which were implemented in TATSSI. Our results are consistent with other scientific studies and results in these areas and with related in-situ data.
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Mirshams, Mehran, and Ehsan Zabihian. "FADSat: A system engineering tool for the conceptual design of geostationary Earth orbit satellites platform." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 6 (May 3, 2018): 2152–69. http://dx.doi.org/10.1177/0954410018773634.

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With regard to the increasing use of satellites platform in the geostationary orbit, a system engineering tool, FADSat, has been developed to reduce the prohibitive cost and time of their conceptual design phase. The proposed tool effectively conducts the design of the geostationary Earth orbit satellite platform lying in the mass range of 1–7000 kg. The main feature of the FADSat is to determine the conceptual design of the satellite platform with both high time performance and acceptable accuracy. Using this tool, one can readily extract the characteristics of the structure, attitude determination and control, command and data handling, electrical power, and other subsystems of a satellite. The FADSat exploits a statistical design model in the first instance to yield a rough estimation of the satellite design, i.e. a rapid extraction of the budgets for mass, power, and dimensions of the satellite subsystems as well as the cost of the satellite. Then, using a parametric design model approach, it performs subsystems design more accurately and ascertains their component specifications in terms of a catalog of products with corresponding manufacturers. A database of 462 geostationary Earth orbit communication satellites (with 30 different geostationary Earth orbit satellites platforms (launched from 2000 to 2017 has been used in this paper to implement the statistical design model approach. This tool developed in the LabVIEW software is capable of contributing to the satellite production phases as a connection to the hardware simulators of different subsystems. Herein, after describing the general concepts utilized in the satellite design, we have introduced various parts and relations of the FADSat tool. The tool’s accuracy was amply verified through flight prototypes, indicating an average error of 15% in the obtained results.
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Mohammad Zadeh, Parviz, and Mohadeseh Sadat Shirazi. "Multidisciplinary design optimization architecture to concurrent design of satellite systems." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 231, no. 10 (September 14, 2016): 1898–916. http://dx.doi.org/10.1177/0954410016665412.

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The design of space systems is a complex and multidisciplinary process with multiple conflicting objectives, large number of design variables, and constraints that limits application of the existing multidisciplinary design optimization architectures to this class of design problems. This paper presents an enhanced multidisciplinary design optimization architecture to concurrent holistic design optimization of a satellite system. The proposed multidisciplinary design optimization architecture extends concepts of multidiscipline feasible and bi-level integrated system synthesis into a unified architecture using metamodels. The proposed architecture was evaluated and compared with the existing multidisciplinary design optimization architectures that include all-at-once, bi-level integrated system synthesis, and multidisciplinary design optimization using a remote sensing small satellite in low earth orbit. The satellite design optimization problem deals with the minimization of the total mass of the satellite, involving disciplines of mission analysis, payload, structures, attitude determination and control, communication, command and data handling, power and thermal. The computational performance and accuracy of the proposed architecture were compared with multidisciplinary design optimization benchmark problems. Then the proposed architecture is successfully applied to the satellite system design problem. The results obtained show that metamodel-based bi-level integrated system synthesis-multidisciplinary design optimization architecture presented in this paper provides an effective way of solving large-scale design problems.
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Taufik, Muhammad, Wahyudi Hasbi, and Abdul Karim. "IN-ORBIT IMPLEMENTATION OF ERROR PATCHING METHODS FOR LAPAN-A3/IPB OBDH FIRMWARE SYSTEM." Jurnal Teknologi Dirgantara 17, no. 1 (June 21, 2019): 11. http://dx.doi.org/10.30536/j.jtd.2019.v17.a3012.

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ABSTRACTOBDH (On-board data handling) is a satellite subsystem that receives, processes, decides and executes commands from and to satellites. OBDH is built on two systems namely hardware and software integrated system (firmware system). In terms of hardware, OBDH uses a processor with 32bit RISC architecture, 128/256 Kbyte internal memory and a firmware system that is built using primitive programming. This programming uses the super loop architecture program and interrupt to manage the system to function properly. Problems occur when an error occurs in one of the functions in the interrupt routine resulting in failure of interpretation of commands or data from satellite sensors. This paper describes the implementation of the error patching methods on the LAPAN-A3/IPB Satellite OBDH firmware system in order to keep the system working well. Initial verification through testing on the ground have been successfully performed using engineering model of OBDH and hardware in the loop simulators (HWIL) module. Based on the test results, implementation on satellite has also been successfully done.ABSTRAKOBDH (On-board data handling) merupakan salah satu subsistem satelit yang berfungsi menerima, mengolah, mengambil keputusan dan mengeksekusi perintah dari dan ke satelit. OBDH dibangun berdasarkan dua buah sistem yaitu sistem perangkat keras dan perangkat lunak yang terintegrasi (sistem firmware). Dari sisi perangkat keras, OBDH menggunakan prosesor dengan arsitektur 32bit RISC, 128/256 Kbyte memori internal, dan sistem firmware yang dibangun menggunakan pemrograman primitif. Pemrograman ini menggunakan arsitektur program super loop dan interrupt untuk mengelola sistem agar dapat berfungsi dengan baik. Permasalahan terjadi ketika terjadi kesalahan pada salah satu fungsi pada rutin interrupt sehingga mengakibatkan kegagalan interpretasi perintah atau data dari sensor satelit. Paper ini menjelaskan mengenai implementasi metode penambalan kesalahan pada sistem firmware OBDH satelit LAPAN-A3/IPB yang bertujuan untuk menjaga agar sistem tetap bekerja dengan baik. Verifikasi awal melalui pengujian telah berhasil dilakukan mengunakan engineering model OBDH dan modul hardware in the loop simulators (HWIL). Berdasarkan hasil pengujian, implementasi pada satelit juga telah sukses dilakukan.
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Mielczarek, Magda, Bartosz Czech, Jarosław Stańczyk, Joanna Szyda, and Bernt Guldbrandtsen. "Extraordinary Command Line: Basic Data Editing Tools for Biologists Dealing with Sequence Data." Open Bioinformatics Journal 13, no. 1 (December 31, 2020): 137–45. http://dx.doi.org/10.2174/1875036202013010137.

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The command line is a standard way of using the Linux operating system. It contains many features essential for efficiently handling data editing and analysis processes. Therefore, it is very useful in bioinformatics applications. Commands allow for rapid manipulation of large ASCII files or very numerous files, making basic command line programming skills a critical component in modern life science research. The following article is not a guide to Linux commands. In this manuscript, in contrast to many various Linux manuals, we aim to present basic command line tools helpful in handling biological sequence data. This manuscript provides a collection of simple and popular hacks dedicated to users with very basic experience in the area of the Linux command line. It includes a description of data formats and examples of editing of four types of data formats popular in bioinformatics applications.
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Parkes, Steve, Chris McClements, Iain Martin, Stuart Mills, Ray Manston, and Martin Dunstan. "SpaceWire Satellite Onboard Data-Handling Networks." IFAC Proceedings Volumes 37, no. 6 (June 2004): 759–64. http://dx.doi.org/10.1016/s1474-6670(17)32268-1.

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Parkes, Stephen M. "SpaceWire: a satellite on‐board data‐handling network." Aircraft Engineering and Aerospace Technology 73, no. 4 (August 2001): 374–79. http://dx.doi.org/10.1108/00022660110399407.

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Bozler, Julian, Hans Juergen Herpel, Jan Johansson, Wahida Gasti, and Olivier Mourra. "Advanced data handling architecture for earth observation satellites." it - Information Technology 63, no. 4 (August 20, 2021): 199–208. http://dx.doi.org/10.1515/itit-2020-0036.

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Abstract In this paper we describe how commercial open standards for embedded systems could affect the architecture of future satellite data handling systems. Traditionally, satellite data handling systems are based on the principles of a federated architecture, i. e. one function is implemented as one box. Each box has its own housing and power supply. In the paper we describe the transition path from the traditional federated architecture to a centralized but modular architecture based on adapted industrial standards. In the presented approach functional modules like on-board computer, Global Navigation Satellite System receiver, interface boards, etc. are combined in a rack communicating via a standard backplane using standardized communication links. The analysis performed during the Advanced Data Handling Architecture study showed that this approach contributes significantly to mass and power reduction (approx. 20 %) of a typical satellite data handling system. Another major point highlighted in the Advanced Data Handling Architecture study is the simplification of Assembly, Integration and Test activities. All this will help space industry to handle increasing system complexity while keeping costs at an acceptable level.
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Starling, Rhaana. "Swift: Opportunities, Capabilities and Data Handling." Proceedings of the International Astronomical Union 7, S285 (September 2011): 183–84. http://dx.doi.org/10.1017/s1743921312000579.

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AbstractA focus session was held for those wanting to familiarise themselves with the Swift satellite and to consider its exploitation for specific scientific goals. An overview was presented, with questions throughout. Proposal preparation and and the automated science products from the X-ray Telescope were discussed. This account summarises the information given in the presentation and in the answers to the questions which were raised.
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Dissertations / Theses on the topic "Satellite Command and Data Handling"

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Olsen, Douglas. "Implementation of CCSDS Telemetry and Command Standards for the Fast Auroral Snapshot (FAST) Small Explorer Mission." International Foundation for Telemetering, 1993. http://hdl.handle.net/10150/611870.

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International Telemetering Conference Proceedings / October 25-28, 1993 / Riviera Hotel and Convention Center, Las Vegas, Nevada
Recommendations of the Consultative Committee for Space Data Systems (CCSDS) provide a standard approach for implementing spacecraft packet telemetry and command interfaces. The Fast Auroral Snapshot (FAST) Small Explorer mission relies heavily on the CCSDS virtual channel and packetization concepts to achieve near real-time commanding and distribution of telemetry between separate space borne science and spacecraft processors and multiple ground stations. Use of the CCSDS recommendations allows the FAST mission to realize significant re-use of ground systems developed for the first Small Explorer mission, and also simplifies system interfaces and interactions between flight software developers, spacecraft integrators, and ground system operators.
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Van, der Merwe Benjamin. "Micro-satellite data handling : a unified information model." Thesis, Stellenbosch : Stellenbosch University, 2001. http://hdl.handle.net/10019.1/52336.

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Thesis (MScEng)--University of Stellenbosch, 2001.
ENGLISH ABSTRACT: This thesis describes various software technologies implemented, or specifically developed, for the SUNSAT micro-satellite mission. With the discussion centered on the Mission Operations System functions of Data Handling and Mission Control, particular emphasis is placed on data processing aspects such as the deployed database schema, and the data communications mechanisms implemented as part of the communications protocol stack. Both the groundsystem architecture and the Flight Software are discussed, their constituent components are analysed, and recommendations are made for improvement. Finally, a Unified Information Model for the design and operation of future, integrated satellite groundsystems is proposed, with suitable implementation technologies being identified and introduced.
AFRIKAANSE OPSOMMING: Hierdie tesis beskryf die sagteware tegnologieë wat qeirnpternenteer. of spesifiek ontwerp is vir die SUNSAT mikro-satelliet missie, Met die bespreking gefokus op die Missie Operasionele Stelsel funksies van Data Hantering en Missie Beheer, word daar veral klem gelê op data prosesserings aspekte, soos byvoorbeeld die databasis skema wat ontplooi is, asook die data kommunikasie meganismes wat qeimplernenteer is as deel van die kommunikasie protokol stapel. Beide die grondstelsel argitektuur en die Vlugsagteware word bespreek, hulonderskeie komponente word geanaliseer, en aanbevelings ter verbetering word gemaak, Laastens word daar 'n Verenigde Informasie Model voorgestel vir die ontwerp en operasionele werking van 'n toekomstige, qeinteqreerde satelliet grondstelsel. Geskikte tegnologieë vir die implementasie hiervan word ook qeidentifiseer en voorgelê,
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Lokken, Patrick Bucknam. "Command and data handling systems for a multi-instrument sounding rocket payload." Thesis, Montana State University, 2011. http://etd.lib.montana.edu/etd/2011/lokken/LokkenP0511.pdf.

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To improve our physical understanding of the solar transition region, the Multi-Order Solar EUV Spectrograph (MOSES) has been developed at Montana State University to perform imaging spectroscopy of the sun at extreme ultraviolet wavelengths. Launched first in 2006, the instrument performed simultaneous imaging and spectroscopy over a narrow band centered around 30.4 nm. The amount of science that can be accomplished with the instrument is limited by its optical bandwidth, which must be small to reduce ambiguity in its data. This limitation can be overcome by launching an array of instruments operating at different wavelengths, piecing together a comprehensive view of transition region activity on a wide bandwidth. However, the command and data handling (C&DH) system on the current MOSES payload cannot support multiple instruments, and a new system must be built to support the addition of more instrumentation. To this end, designs based on a centralized computer topology and a distributed computer topology have been created for a new C&DH system to support the existing MOSES instrument, an EUV Snapshot Imaging Spectrograph (ESIS) and an improved guide scope. It was found that the frame rate of the entire electro-optical system was limited mostly by the low sensitivity of the optics, and that the choice between the two is driven by the mass of the system and the amount of engineering effort required to build the system. The centralized system was found to be both lighter and easier to build, and therefore a centralized system is recommended for the second revision of the MOSES payload.
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Forman, Michael L., Tushar K. Hazra, Gregory M. Troendly, and William G. Nickum. "APPLYING PC-BASED EMBEDDED PROCESSING FOR REAL-TIME SATELLITE DATA ACQUISITION AND CONTROL." International Foundation for Telemetering, 1993. http://hdl.handle.net/10150/608833.

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International Telemetering Conference Proceedings / October 25-28, 1993 / Riviera Hotel and Convention Center, Las Vegas, Nevada
The performance and cost effectiveness of em bedded processing has greatly enhanced the personal computer's (PC) capability, particularly when used for real-time satellite data acquisition, telemetry processing, command and control operations. Utilizing a transputer based parallel architecture, a modular, reusable, and scalable control system is attainable. The synergism between the personal computer and embedded processing results in efficient, low cost desktop workstations up to 1000 MIPS of performance.
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Bester, Manfred, and Brett Stroozas. "TELEMETRY AND COMMAND FRAME ROUTING IN A MULTI-MISSION ENVIRONMENT." International Foundation for Telemetering, 2007. http://hdl.handle.net/10150/604572.

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ITC/USA 2007 Conference Proceedings / The Forty-Third Annual International Telemetering Conference and Technical Exhibition / October 22-25, 2007 / Riviera Hotel & Convention Center, Las Vegas, Nevada
In a modern ground control network for space communications, secure peer-to-peer TCP/IP network socket connections are typically used to transfer real-time telemetry and command frames between satellite operations centers and remote ground stations. Reliable and timely reconfiguration of data paths for upcoming pass supports becomes rather complex when many spacecraft and ground stations are involved. This paper describes a routing software application that was developed to facilitate switching of telemetry and command data paths between multiple ground stations and spacecraft command and control systems, and to forward telemetry streams to multiple client applications in parallel. Fully automated configuration and monitoring of the data flows is accomplished via a remote control interface that is tied into a pass scheduling system. The software is part of the SatTrack Suite and currently supports multi-mission flight operations, including those of the recently launched THEMIS constellation mission at Space Sciences Laboratory, University of California at Berkeley.
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DeBoy, Christopher C., Paul D. Schwartz, and Richard K. Huebschman. "Midcourse Space Experiment Spacecraft and Ground Segment Telemetry Design and Implementation." International Foundation for Telemetering, 1996. http://hdl.handle.net/10150/608390.

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International Telemetering Conference Proceedings / October 28-31, 1996 / Town and Country Hotel and Convention Center, San Diego, California
This paper reviews the performance requirements that provided the baseline for development of the onboard data system, RF transmission system, and ground segment receiving system of the Midcourse Space Experiment (MSX) spacecraft. The onboard Command and Data Handling (C&DH) System was designed to support the high data outputs of the three imaging sensor systems onboard the spacecraft and the requirement for large volumes of data storage. Because of the high data rates, it was necessary to construct a dedicated X-band ground receiver system at The Johns Hopkins University Applied Physics Laboratory (APL) and implement a tape recorder system for recording and downlinking sensor and spacecraft data. The system uses two onboard tape recorders to provide redundancy and backup capabilities. The storage capability of each tape recorder is 54 gigabits. The MSX C&DH System can record data at 25 Mbps or 5 Mbps. To meet the redundancy requirements of the high-priority experiments, the data can also be recorded in parallel on both tape recorders. To provide longer onboard recording, the data can also be recorded serially on the two recorders. The reproduce (playback) mode is at 25 Mbps. A unique requirement of the C&DH System is to multiplex and commutate the different output rates of the sensors and housekeeping signals into a common data stream for recording. The system also supports 1-Mbps real-time sensor data and 16-kbps real-time housekeeping data transmission to the dedicated ground site and through the U.S. Air Force Satellite Control Network ground stations. The primary ground receiving site for the telemetry is the MSX Tracking System (MTS) at APL. A dedicated 10-m X-band antenna is used to track the satellite during overhead passes and acquire the 25-Mbps telemetry downlinks, along with the 1-Mbps and 16-kbps real-time transmissions. This paper discusses some of the key technology trade-offs that were made in the design of the system to meet requirements for reliability, performance, and development schedule. It also presents some of the lessons learned during development and the impact these lessons will have on development of future systems.
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Johl, Shaina Ashley Mattu. "A reusable command and data handling system for university CubeSat missions." Thesis, 2013. http://hdl.handle.net/2152/23627.

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A Command and Data Handling (C&DH) system is being developed as part of a series of CubeSat missions being built at The University of Texas at Austin’s Texas Spacecraft Laboratory (TSL). With concurrent development of four missions, and with more missions planned for the future, the C&DH team is developing a system architecture that can support many mission requirements. The presented research aims to establish itself as a reference for the development of the C&DH system architecture so that it can be reused for future university missions. The C&DH system is designed using a centralized architecture with one main flight computer controlling the actions and the state of the satellite. A Commercial Off-The-Shelf (COTS) system-on-module embedded computer running a Linux environment hosted on a custom interface board is used as the platform for the mission software. This design choice and the implementation details of the flight software are described in detail in this report. The design of the flight software and the associated hardware are integral components of the spacecraft for the current missions in the TSL which, when flown, will be some of the most operationally complex CubeSat missions attempted to date.
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Book chapters on the topic "Satellite Command and Data Handling"

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Fillery, Nigel P., and David Stanton. "Telemetry, Command, Data Handling and Processing." In Spacecraft Systems Engineering, 439–66. Chichester, UK: John Wiley & Sons, Ltd, 2011. http://dx.doi.org/10.1002/9781119971009.ch13.

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Nannipieri, Pietro, Gianmarco Dinelli, Luca Dello Sterpaio, Antonino Marino, and Luca Fanucci. "Introduction to Satellite on-Board Data-Handling." In Next-Generation High-Speed Satellite Interconnect, 1–21. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-77044-0_1.

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Mishra, Deepti, and Garima Khandelwal. "Command-Line Tools in Linux for Handling Large Data Files." In Bioinformatics: Sequences, Structures, Phylogeny, 375–92. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-1562-6_17.

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McFadden, J. P., R. E. Ergun, C. W. Carlson, W. Herrick, J. Loran, J. Vernetti, W. Teitler, K. Bromund, and T. Quinn. "Science Operations and Data Handling for the Fast Satellite." In The FAST Mission, 169–96. Dordrecht: Springer Netherlands, 2001. http://dx.doi.org/10.1007/978-94-010-0332-2_7.

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Abujayyab, Sohaib K. M., and Ismail Rakip Karas. "Handling Massive Data Size Issue in Buildings Footprints Extraction from High-Resolution Satellite Images." In Advances in Building Information Modeling, 195–210. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-42852-5_16.

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Maitra, Saswata, S. Chandrakanth, R. M. K. Guptha, P. Neeraja, K. L. Raja Sekhar, and T. Venkata Mani. "Integrated High Speed and High Capacity Base-Band Data Handling—Solid-State Recorder for Small Satellite Applications." In Lecture Notes in Mechanical Engineering, 237–48. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-1724-2_25.

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Perez, Reinaldo. "Command Data Handling Subsystem." In Wireless Communications Design Handbook, 141–201. Elsevier, 1998. http://dx.doi.org/10.1016/s1874-6101(99)80018-0.

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Knox, Jason, Stan Aungst, Todd Bacastow, Mark Campbell, David Beyerle, and Jeff Kuhns. "Fusion of Ground and Satellite Data via Army Battle Command System." In Handbook of Multisensor Data Fusion, 759–72. CRC Press, 2008. http://dx.doi.org/10.1201/9781420053098.ch30.

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Pillai, Dhanasekaran K. "New Computational Models for Image Remote Sensing and Big Data." In Big Data Analytics for Satellite Image Processing and Remote Sensing, 1–21. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-3643-7.ch001.

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This chapter focuses on the development of new computational models for remote sensing applications with big data handling method using image data. Furthermore, this chapter presents an overview of the process of developing systems for remote sensing and monitoring. The issues and challenges are presented to discuss various problems related to the handling of image big data in wireless sensor networks that have various real-world applications. Moreover, the possible solutions and future recommendations to address the challenges have been presented and also this chapter includes discussion of emerging trends and a conclusion.
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Srivastava, Utkarsh, and Ramanathan L. "Iterative MapReduce." In Big Data Analytics for Satellite Image Processing and Remote Sensing, 117–32. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-3643-7.ch007.

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Diabetes Mellitus has turned into a noteworthy general wellbeing issue in India. Most recent measurements on diabetes uncover that 63 million individuals in India are experiencing diabetes, and this figure is probably going to go up to 80 million by 2025. Given the rise of big data as a socio-technical phenomenon, there are various complications in analyzing big data and its related data handling issues. This chapter examines Hadoop, an open source structure that permits the disseminated handling for huge datasets on group of PCs and thus finally produces better results with the deployment of Iterative MapReduce. The goal of this chapter is to dissect and extricate the enhanced performance of data analysis in distributed environment. Iterative MapReduce (i-MapReduce) plays a major role in optimizing the analytics performance. Implementation is done on Cloudera Hadoop introduced on top of Hortonworks Data Platform (HDP) Sandbox.
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Conference papers on the topic "Satellite Command and Data Handling"

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Schor, D., J. Scowcroft, C. Nichols, and W. Kinsner. "A Command and Data Handling unit for pico-satellite missions." In 2009 Canadian Conference on Electrical and Computer Engineering (CCECE). IEEE, 2009. http://dx.doi.org/10.1109/ccece.2009.5090254.

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Yra, Pablito, Matteo Genna, Sean McMahon, Kevin Kerns, Robert Tiede, Mike Laird, and Tom Cronauer. "Next-Generation Spacecraft Command & Data Handling System Based on the RAD750 Processor." In 28th AIAA International Communications Satellite Systems Conference (ICSSC-2010). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-8888.

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Ogut, Mehmet, Yuriy Goncharenko, Steven C. Reising, Braxton Kilmer, Xavier Bosch-Lluis, Pekka Kangaslahti, and Erich Schlecht. "Single Event Effect Analysis for Command and Data Handling Electronics of a Millimeter-Wave Radiometer 6U-Class Satellite Instrument." In 2017 17th European Conference on Radiation and Its Effects on Components and Systems (RADECS). IEEE, 2017. http://dx.doi.org/10.1109/radecs.2017.8696153.

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Ogut, Mehmet, Xavier Bosch-Lluis, Steven C. Reising, Yuriy V. Goncharenko, Pekka Kangaslahti, Erich Schlecht, Richard Cofield, et al. "Command and data handling (C&DH) subsystem for the tropospheric water and cloud ice (twice) 6u-class satellite instrument." In 2017 IEEE International Geoscience and Remote Sensing Symposium (IGARSS). IEEE, 2017. http://dx.doi.org/10.1109/igarss.2017.8127565.

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Ogut, Mehmet, Steven C. Reising, Yuriy V. Goncharenko, Braxton Kilmer, Xavier Bosch-Lluis, Pekka Kangaslahti, Erich Schlecht, et al. "Design, Testing and Reliability Analysis of Command and Data Handling (C&DH) Subsystem for the Tropospheric Water and Cloud Ice (Twice) Instrument for a 6U-Class Small Satellite." In IGARSS 2018 - 2018 IEEE International Geoscience and Remote Sensing Symposium. IEEE, 2018. http://dx.doi.org/10.1109/igarss.2018.8517952.

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Eger, George. "Orion's Command and Data Handling Architecture." In AIAA SPACE 2008 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-7743.

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Akhtar, Syed Ashar, and Craig I. Underwood. "Dynamic Command and Data Handling Ground Station Software." In 2007 3rd International Conference on Recent Advances in Space Technologies. IEEE, 2007. http://dx.doi.org/10.1109/rast.2007.4284048.

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Raphael, David, Robert F. Stone, Damaris L. Guevara, and James E. Fraction. "Command & Data Handling for the magnetospheric multiscale mission." In 2014 IEEE Aerospace Conference. IEEE, 2014. http://dx.doi.org/10.1109/aero.2014.6836373.

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Black, Randall H. "Integrated Modular Concepts for Improved ECLSS Command and Data Handling." In International Conference On Environmental Systems. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2006. http://dx.doi.org/10.4271/2006-01-2122.

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Urbanec, T., P. Vagner, O. Baran, and M. Kasal. "Experimental satellite communication and data handling system." In 2013 23rd International Conference Radioelektronika (RADIOELEKTRONIKA 2013). IEEE, 2013. http://dx.doi.org/10.1109/radioelek.2013.6530913.

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Reports on the topic "Satellite Command and Data Handling"

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Health hazard evaluation report: HETA-2007-0095-3063, nonionizing radiation exposure to technicians at a satellite communications facility, U.S. Department of Commerce, Wallops Command and Data Acquisition Station, Wallops, Virginia. U.S. Department of Health and Human Services, Public Health Service, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, June 2008. http://dx.doi.org/10.26616/nioshheta200700953063.

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