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Volumn 104, Issue , 2000, Pages 197-212

Project Orion: Carrier phase differential GPS navigation for formation flying

Author keywords

[No Author keywords available]

Indexed keywords


EID: 0040953192     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article
Times cited : (10)

References (32)
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    • (1999) GPS Sensing for Formation Flying Vehicles
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    • Ph.D. Thesis, Stanford University, Dept. of Aeronautical and Astronautical Engineering, Dec
    • J.C. Adams, "Robust GPS Attitude Determination for Spacecraft," Ph.D. Thesis, Stanford University, Dept. of Aeronautical and Astronautical Engineering, Dec 1999.
    • (1999) Robust GPS Attitude Determination for Spacecraft
    • Adams, J.C.1
  • 20
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    • Operational use of civil space-based synthetic aperture radar
    • Aug
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  • 21
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    • A universal 3-D method for controlling the relative motion of multiple spacecraft in any orbit
    • Aug
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  • 22
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    • Aug.
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    • Meshabi, M.1    Hadaegh, F.Y.2
  • 23
    • 0030182761 scopus 로고    scopus 로고
    • Coordination and control of multiple microspacecraft moving in formation
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  • 24
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  • 32
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.