Spacecraft

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A spacecraft or spaceship is a craft or machine designed for spaceflight. (Wikipedia.org)






Conferences related to Spacecraft

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2020 IEEE International Conference on Plasma Science (ICOPS)

IEEE International Conference on Plasma Science (ICOPS) is an annual conference coordinated by the Plasma Science and Application Committee (PSAC) of the IEEE Nuclear & Plasma Sciences Society.


2019 41st Annual International Conference of the IEEE Engineering in Medicine & Biology Society (EMBC)

The conference program will consist of plenary lectures, symposia, workshops andinvitedsessions of the latest significant findings and developments in all the major fields ofbiomedical engineering.Submitted papers will be peer reviewed. Accepted high quality paperswill be presented in oral and postersessions, will appear in the Conference Proceedings and willbe indexed in PubMed/MEDLINE & IEEE Xplore


2019 IEEE 58th Conference on Decision and Control (CDC)

The CDC is recognized as the premier scientific and engineering conference dedicated to the advancement of the theory and practice of systems and control. The CDC annually brings together an international community of researchers and practitioners in the field of automatic control to discuss new research results, perspectives on future developments, and innovative applications relevant to decision making, systems and control, and related areas.The 58th CDC will feature contributed and invited papers, as well as workshops and may include tutorial sessions.The IEEE CDC is hosted by the IEEE Control Systems Society (CSS) in cooperation with the Society for Industrial and Applied Mathematics (SIAM), the Institute for Operations Research and the Management Sciences (INFORMS), the Japanese Society for Instrument and Control Engineers (SICE), and the European Union Control Association (EUCA).


2019 IEEE Applied Power Electronics Conference and Exposition (APEC)

APEC focuses on the practical and applied aspects of the power electronics business. The conference addresses issues of immediate and long term importance to practicing power electronics engineer.


2019 IEEE International Geoscience and Remote Sensing Symposium (IGARSS)

International Geosicence and Remote Sensing Symposium (IGARSS) is the annual conference sponsored by the IEEE Geoscience and Remote Sensing Society (IEEE GRSS), which is also the flagship event of the society. The topics of IGARSS cover a wide variety of the research on the theory, techniques, and applications of remote sensing in geoscience, which includes: the fundamentals of the interactions electromagnetic waves with environment and target to be observed; the techniques and implementation of remote sensing for imaging and sounding; the analysis, processing and information technology of remote sensing data; the applications of remote sensing in different aspects of earth science; the missions and projects of earth observation satellites and airborne and ground based campaigns. The theme of IGARSS 2019 is “Enviroment and Disasters”, and some emphases will be given on related special topics.


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Periodicals related to Spacecraft

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Aerospace and Electronic Systems Magazine, IEEE

The IEEE Aerospace and Electronic Systems Magazine publishes articles concerned with the various aspects of systems for space, air, ocean, or ground environments.


Antennas and Propagation, IEEE Transactions on

Experimental and theoretical advances in antennas including design and development, and in the propagation of electromagnetic waves including scattering, diffraction and interaction with continuous media; and applications pertinent to antennas and propagation, such as remote sensing, applied optics, and millimeter and submillimeter wave techniques.


Antennas and Wireless Propagation Letters, IEEE

IEEE Antennas and Wireless Propagation Letters (AWP Letters) will be devoted to the rapid electronic publication of short manuscripts in the technical areas of Antennas and Wireless Propagation.


Automatic Control, IEEE Transactions on

The theory, design and application of Control Systems. It shall encompass components, and the integration of these components, as are necessary for the construction of such systems. The word `systems' as used herein shall be interpreted to include physical, biological, organizational and other entities and combinations thereof, which can be represented through a mathematical symbolism. The Field of Interest: shall ...


Communications, IEEE Transactions on

Telephone, telegraphy, facsimile, and point-to-point television, by electromagnetic propagation, including radio; wire; aerial, underground, coaxial, and submarine cables; waveguides, communication satellites, and lasers; in marine, aeronautical, space and fixed station services; repeaters, radio relaying, signal storage, and regeneration; telecommunication error detection and correction; multiplexing and carrier techniques; communication switching systems; data communications; and communication theory. In addition to the above, ...


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Most published Xplore authors for Spacecraft

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Xplore Articles related to Spacecraft

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Design for Automatic Generation of Spacecraft Telemetry Software Code Based on Incremental Model

[{u'author_order': 1, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086461668', u'full_name': u'Wenping Wang', u'id': 37086461668}, {u'author_order': 2, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086462662', u'full_name': u'Jianbing Zhu', u'id': 37086462662}, {u'author_order': 3, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086462107', u'full_name': u'Yahang Zhang', u'id': 37086462107}, {u'author_order': 4, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086460871', u'full_name': u'Zhixin Tian', u'id': 37086460871}, {u'author_order': 5, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086463318', u'full_name': u'Xianghui Wang', u'id': 37086463318}] 2018 2nd IEEE Advanced Information Management,Communicates,Electronic and Automation Control Conference (IMCEC), 2018

This paper describes an automatic generation method of spacecraft telemetry software code based on incremental model. First of all, a spacecraft incremental telemetry design model is established, including data system architecture model, detailed design model and system integration model. Secondly, the related parameter design of each telemetry design model is completed in turn. Then, each telemetry design model is automatically ...


Fault Detection and Recovery Strategy for Partial 1553B Bus Controller RAM Failure of Spacecraft in Orbit

[{u'author_order': 1, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086461668', u'full_name': u'Wenping Wang', u'id': 37086461668}, {u'author_order': 2, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086462107', u'full_name': u'Yahang Zhang', u'id': 37086462107}, {u'author_order': 3, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086463318', u'full_name': u'Xianghui Wang', u'id': 37086463318}, {u'author_order': 4, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086461927', u'full_name': u'Yong Lei', u'id': 37086461927}, {u'author_order': 5, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086462252', u'full_name': u'Zhenhui Dong', u'id': 37086462252}, {u'author_order': 6, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086461259', u'full_name': u'Li Pan', u'id': 37086461259}, {u'author_order': 7, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086463461', u'full_name': u'Hongjun Zhang', u'id': 37086463461}, {u'author_order': 8, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, Beijing, 100094, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086463404', u'full_name': u'Feng Fang', u'id': 37086463404}] 2018 2nd IEEE Advanced Information Management,Communicates,Electronic and Automation Control Conference (IMCEC), 2018

In the spacecraft, 1553B bus controller is the central for the management of bus information exchange, whose reliability directly relates to system security. In recent years, due to the hash space environment in orbit, many cases of spacecraft bus RAM failures caused by the single event effect have occurred both at home and abroad. This paper presents a method for ...


Design analysis & verification of separation test platform for spacecraft

[{u'author_order': 1, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085735583', u'full_name': u'Zheng Shengyu', u'id': 37085735583}, {u'author_order': 2, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085738110', u'full_name': u'Yi Wangmin', u'id': 37085738110}, {u'author_order': 3, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085734002', u'full_name': u'Feng Wei', u'id': 37085734002}, {u'author_order': 4, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085727311', u'full_name': u'Guo Dabao', u'id': 37085727311}, {u'author_order': 5, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085735083', u'full_name': u'Chen Qiwei', u'id': 37085735083}, {u'author_order': 6, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085732798', u'full_name': u'Tang Laiying', u'id': 37085732798}, {u'author_order': 7, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085721228', u'full_name': u'Fang Zhikai', u'id': 37085721228}, {u'author_order': 8, u'affiliation': u'Beijing Institute of Spacecraft System Engineering, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37085736797', u'full_name': u'Li Qing', u'id': 37085736797}] 2015 IEEE International Conference on Mechatronics and Automation (ICMA), 2015

The spacecraft which is composed by several modules should be tested on the ground whether the modules can be separated successfully or not, and separation locomotion data should be obtained as well. This paper has described the requirements and difficulties of separation test, and has designed the zero gravity platform. The critical design parameters are obtained by the analysis result ...


Spacecraft Charging Analysis of Large GEO Satellites Using MUSCAT

[{u'author_order': 1, u'affiliation': u'Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology , Kitakyushu, Japan', u'authorUrl': u'https://ieeexplore.ieee.org/author/37289899500', u'full_name': u'Mengu Cho', u'id': 37289899500}, {u'author_order': 2, u'affiliation': u'Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology , Kitakyushu, Japan', u'authorUrl': u'https://ieeexplore.ieee.org/author/38242261500', u'full_name': u'Takahiro Sumida', u'id': 38242261500}, {u'author_order': 3, u'affiliation': u'Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology , Kitakyushu, Japan', u'authorUrl': u'https://ieeexplore.ieee.org/author/37602204300', u'full_name': u'Hirokazu Masui', u'id': 37602204300}, {u'author_order': 4, u'affiliation': u'Laboratory of Spacecraft Environment Interaction Engineering, Kyushu Institute of Technology , Kitakyushu, Japan', u'authorUrl': u'https://ieeexplore.ieee.org/author/37298843700', u'full_name': u'Kazuhiro Toyoda', u'id': 37298843700}, {u'author_order': 5, u'affiliation': u'MUSCAT Space Engineering Co. Ltd., Kitakyushu, Japan', u'authorUrl': u'https://ieeexplore.ieee.org/author/37423834600', u'full_name': u'Jeong-Ho Kim', u'id': 37423834600}, {u'author_order': 6, u'affiliation': u'MUSCAT Space Engineering Co. Ltd., Kitakyushu, Japan', u'authorUrl': u'https://ieeexplore.ieee.org/author/37883908700', u'full_name': u'Shinji Hatta', u'id': 37883908700}, {u'author_order': 7, u'affiliation': u'Space Systems/Loral, Palo Alto, USA', u'authorUrl': u'https://ieeexplore.ieee.org/author/37596903500', u'full_name': u'Frankie K. Wong', u'id': 37596903500}, {u'author_order': 8, u'affiliation': u'Space Systems/Loral, Palo Alto, CA, USA', u'authorUrl': u'https://ieeexplore.ieee.org/author/37589660300', u'full_name': u'Bao Hoang', u'id': 37589660300}] IEEE Transactions on Plasma Science, 2012

A series of spacecraft charging analyses was carried out for large GEO satellites using Multi-Utility Spacecraft Charging Analysis Tool. The purpose was to derive the number of electrostatic discharges expected for 15 years in orbit, which would be used as the basis of the number of primary electrostatic discharges (ESDs) to be used in future solar cell coupon ESD tests. ...


Interference Detection of Spacecraft Before Deck Docking Based on 3D Scanner

[{u'author_order': 1, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086522278', u'full_name': u'Wei Zhang', u'id': 37086522278}, {u'author_order': 2, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086521449', u'full_name': u'Zaihua Yang', u'id': 37086521449}, {u'author_order': 3, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing Engineering Research Center of the Intelligent Assembly Technology and Equipment for Aerospace Product, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086521004', u'full_name': u'Kai Xu', u'id': 37086521004}, {u'author_order': 4, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086521866', u'full_name': u'Rongxu Xiao', u'id': 37086521866}, {u'author_order': 5, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086522718', u'full_name': u'Lei Sun', u'id': 37086522718}, {u'author_order': 6, u'affiliation': u'Beijing Institute of Spacecraft Environment Engineering, Beijing, China', u'authorUrl': u'https://ieeexplore.ieee.org/author/37086521259', u'full_name': u'Pan Hao', u'id': 37086521259}] 2017 5th International Conference on Mechanical, Automotive and Materials Engineering (CMAME), 2017

Spacecraft contains many flexible components and sampling parts, there are often many differences between real product and three-dimensional design models, so spacecraft component sometimes can't be installed due to component interference or small safety distance in assembly and integration process of spacecraft. Non-contact interference detection based on 3D scanner Handyscan 700 and Geomagic Control is designed, The Handyscan 700 which ...


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Standards related to Spacecraft

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IEEE Recommended Practice for Inertial Sensor Test Equipment, Instrumentation, Data Acquisition, and Analysis

Recommended practices for gyroscope and accelerometer testing are discussed, ranging from the equipment and instrumentation employed to the way that tests are carried out and data are acquired and analyzed.


IEEE Recommended Practice for Precision Centrifuge Testing of Linear Accelerometers

Generate errata and/or revisions to the existing Std. 836-1991.


IEEE Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros


IEEE Specification Format Guide and Test Procedure for Two-Degree-of-Freedom Dynamically Tuned Gyros


IEEE Standard for Inertial Sensor Terminology

To review all of the definitions included in the standard and to revise them as required. New terminology will be added to bring the document up to date with current technology.


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Jobs related to Spacecraft

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