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Volumn , Issue , 2002, Pages

The technical issues with implementing spacecraft open avionics platforms

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894291628     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (32)
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  • 8
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    • The Implementation of a COTS Based Fault Tolerant Avionic Bus Architecture
    • Chau, S. et. al. (2000), "The Implementation of a COTS Based Fault Tolerant Avionic Bus Architecture", IEEE Aerospace Conference
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  • 9
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    • MIDEX Advance Modular and Distributed Spacecraft Avionics Architecture
    • Ruffa, Castell, Flatley, and Lin (1998), "MIDEX Advance Modular and Distributed Spacecraft Avionics Architecture", IEEE Aerospace Conference Proceedings
    • (1998) IEEE Aerospace Conference Proceedings
    • Ruffa, C.1    Flatley2    Lin3
  • 10
    • 84879379845 scopus 로고    scopus 로고
    • A Standard of Excellence, Internal NASA Report
    • Strope, D., (1996), X-Ray Timing Explorer (XTE), A Standard of Excellence, Internal NASA Report
    • (1996) X-Ray Timing Explorer (XTE)
    • Strope, D.1
  • 11
    • 0003222572 scopus 로고    scopus 로고
    • A Fault Tolerant Integrated Electronics Module for Small Satellites
    • Fraeman, M. (1997), "A Fault Tolerant Integrated Electronics Module for Small Satellites", 11thAIAA/USU Conference on Small Satellites
    • (1997) 11thAIAA/USU Conference on Small Satellites
    • Fraeman, M.1
  • 12
    • 84894331899 scopus 로고    scopus 로고
    • SMEX-Lite-An Innovative System Architecture for Reducing Spacecraft Size and Cost
    • Watzin, J. (1998), "SMEX-Lite-An Innovative System Architecture for Reducing Spacecraft Size and Cost", 49th International Astronautical Congress
    • (1998) 49th International Astronautical Congress
    • Watzin, J.1
  • 19
    • 0001834005 scopus 로고    scopus 로고
    • Planning Product Platforms
    • (September)
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    • Roberson1    Ulrich, K.T.2
  • 23
    • 84894320158 scopus 로고
    • New Techniques Allow 22-Day Satellite Assembly
    • (April 3), #14
    • (April 3, 1995), "New Techniques Allow 22-Day Satellite Assembly", Aviation Week and Space Technology, Vol 142, #14
    • (1995) Aviation Week and Space Technology , vol.142
  • 27
    • 84980047942 scopus 로고
    • Creating Scaleble, Reusable, Interoperable, Spaceborne Computer Modules with a High Performance Backplane Bus
    • AIAA-95-1005-C
    • Marshal, J., Belvin, S., Laurvick, C. (1995), "Creating Scaleble, Reusable, Interoperable, Spaceborne Computer Modules with a High Performance Backplane Bus", AIAA Computing in Aerospace 10, AIAA-95-1005-C
    • (1995) AIAA Computing in Aerospace 10
    • Marshal, J.1    Belvin, S.2    Laurvick, C.3
  • 29
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    • PRIMA: A New, Competitive Small Satellite Platform
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  • 31
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    • The LEOSTAR Solution for High Performance Earth Observation Missions
    • Durteste, C., Schirmann, T., Dribault, L. (2000), "The LEOSTAR Solution for High Performance Earth Observation Missions", Acta Astronautica, Vol. 46, Nos. 2-6
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    • Durteste, C.1    Schirmann, T.2    Dribault, L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.