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Volumn 27, Issue 1, 2004, Pages 154-157

Nonlinear Modeling of Spacecraft Relative Motion in the Configuration Space

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; FUNCTIONS; LAGRANGE MULTIPLIERS; MOTION ESTIMATION; ORBITS; PARAMETER ESTIMATION; PROBLEM SOLVING; SPACECRAFT; TIME SERIES ANALYSIS; VECTORS;

EID: 1042298574     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.9343     Document Type: Article
Times cited : (86)

References (10)
  • 1
    • 0001422127 scopus 로고
    • Terminal Guidance System for Satellite Rendezvous
    • Clohessy, W. H., and Wiltshire, R. S., "Terminal Guidance System for Satellite Rendezvous," Journal of Astronautical Sciences, Vol. 27, No. 9, 1960, pp. 653-678.
    • (1960) Journal of Astronautical Sciences , vol.27 , Issue.9 , pp. 653-678
    • Clohessy, W.H.1    Wiltshire, R.S.2
  • 2
    • 0036157296 scopus 로고    scopus 로고
    • Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits
    • Inalhan, G., Tillerson, M., and How, J. P., "Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 1, 2002, pp. 48-60.
    • (2002) Journal of Guidance, Control, and Dynamics , vol.25 , Issue.1 , pp. 48-60
    • Inalhan, G.1    Tillerson, M.2    How, J.P.3
  • 4
    • 0034165585 scopus 로고    scopus 로고
    • Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions
    • Alfriend, K. T., and Schaub, H., "Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions," Journal of Astronautical Sciences, Vol. 48, No. 2, 2000, pp. 249-267.
    • (2000) Journal of Astronautical Sciences , vol.48 , Issue.2 , pp. 249-267
    • Alfriend, K.T.1    Schaub, H.2
  • 5
    • 0002311236 scopus 로고
    • Researches in the Lunar Theory
    • Hill, G. W., "Researches in the Lunar Theory," American Journal of Mathematics, Vol. 1, 1878, pp. 5-26.
    • (1878) American Journal of Mathematics , vol.1 , pp. 5-26
    • Hill, G.W.1
  • 6
    • 0035067855 scopus 로고    scopus 로고
    • Spacecraft Formation Flying Control Using Mean Orbital Elements
    • Schaub, H., Vadali, S. R., and Alfriend, K. T., "Spacecraft Formation Flying Control Using Mean Orbital Elements," Journal of Astronautical Sciences, Vol. 48, No. 1, 2000, pp. 69-87.
    • (2000) Journal of Astronautical Sciences , vol.48 , Issue.1 , pp. 69-87
    • Schaub, H.1    Vadali, S.R.2    Alfriend, K.T.3
  • 7
    • 0036494036 scopus 로고    scopus 로고
    • Hybrid Cartesian and Orbit Elements Feedback Law for Formation Flying Spacecraft
    • Schaub, H., and Alfriend, K., "Hybrid Cartesian and Orbit Elements Feedback Law for Formation Flying Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 2, 2002, pp. 387-393.
    • (2002) Journal of Guidance, Control, and Dynamics , vol.25 , Issue.2 , pp. 387-393
    • Schaub, H.1    Alfriend, K.2
  • 9
    • 85088181260 scopus 로고    scopus 로고
    • Nonlinear Considerations in Satellite Formation Flying
    • Aug.
    • Alfriend, K. T., Yan, H., and Vadali, S. R., "Nonlinear Considerations in Satellite Formation Flying," AIAA Paper 2002-4741, Aug. 2002.
    • (2002) AIAA Paper 2002-4741
    • Alfriend, K.T.1    Yan, H.2    Vadali, S.R.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.