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Volumn 26, Issue 6, 2003, Pages 956-971

State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit

Author keywords

[No Author keywords available]

Indexed keywords

DIFFERENTIAL EQUATIONS; GRAVITATION; MATRIX ALGEBRA; PERTURBATION TECHNIQUES; VECTORS;

EID: 0344898941     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.6924     Document Type: Article
Times cited : (363)

References (15)
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  • 5
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    • Univelt, San Diego, CA
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    • Melton, R.G.1
  • 7
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    • Vaddi, S., Vadali, S. R., and Alfriend, K. T., "Formation Flying: Accommodating Non-Linearity and Eccentricity Perturbations," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 2, 2003, pp. 214-223.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.2 , pp. 214-223
    • Vaddi, S.1    Vadali, S.R.2    Alfriend, K.T.3
  • 8
    • 0001229316 scopus 로고    scopus 로고
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  • 9
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    • Alfriend K. T., Schaub, H., and Gim, D.-W., "Gravitational Perturbations, Nonlinearity and Circular Orbit Assumption Effects on Formation Flying Control Strategies," American Astronautical Society, 23rd Annual AAS Guidance and Control Conf., AAS 00-012, Feb. 2000; also Advances in the Astronomical Sciences, Vol. 104, Univelt, San Diego, CA, 2000, pp. 139-158.
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    • Aug.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.