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Volumn 4, Issue , 2004, Pages 3333-3338

Utilization of the bias momentum approach for capturing a tumbling satellite

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; KINEMATICS; MANIPULATORS; MATRIX ALGEBRA; METHOD OF MOMENTS; PARAMETER ESTIMATION; ROBOTS; SPACE DEBRIS; TRAJECTORIES;

EID: 14044252313     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (45)

References (15)
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  • 2
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  • 5
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    • Dynamics, control and impedance matching for robotic capture of a non-cooperative satellite
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    • Yoshida, K.1    Nakanishi, H.2
  • 6
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    • Impact analysis and post-impact motion control issues of a free-floating space robot subject to a force impulse
    • June
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  • 7
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    • Satellite stabilization using space leeches
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    • Walker, M.W.1    Kim, D.M.2
  • 8
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    • Rotational motion-damper for the capture of an uncontrolled floating satellite
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  • 9
    • 14044257566 scopus 로고    scopus 로고
    • Impulsive control for angular momentum management of tumbling spacecraft
    • Miyazaki, Japan, May 30 - June 6
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  • 10
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    • Guidance and control of "Tethered retriever" for future on-orbit service missions
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    • Nakamura, Y.1    Sasaki, F.2    Nakasuka, S.3
  • 11
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  • 12
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  • 13
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  • 14
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.