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Volumn 26, Issue 2, 2003, Pages 214-223

Formation flying: Accommodating nonlinearity and eccentricity perturbations

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; ASYMPTOTIC STABILITY; EQUATIONS OF MOTION; GRAVITATION; MATHEMATICAL MODELS; NONLINEAR EQUATIONS; ORBITS; PERTURBATION TECHNIQUES; SATELLITES;

EID: 0037352111     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.5054     Document Type: Article
Times cited : (184)

References (12)
  • 1
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    • Time explicit representation of relative motion between elliptical orbits
    • Melton, R. G., "Time Explicit Representation of Relative Motion Between Elliptical Orbits," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 4, 2000, pp. 604-610.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.4 , pp. 604-610
    • Melton, R.G.1
  • 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. 48-59.
    • (2002) Journal of Guidance, Control, and Dynamics , vol.25 , Issue.1 , pp. 48-59
    • Inalhan, G.1    Tillerson, M.2    How, J.P.3
  • 3
    • 0001354861 scopus 로고
    • Rendezvous problem for nearly circular orbits
    • Anthony, M. L., and Sasaki, F. T., "Rendezvous Problem for Nearly Circular Orbits," AIAA Journal, Vol. 3, No. 9, 1965, pp. 1666-1673.
    • (1965) AIAA Journal , vol.3 , Issue.9 , pp. 1666-1673
    • Anthony, M.L.1    Sasaki, F.T.2
  • 4
    • 85003237213 scopus 로고
    • Relative trajectories of objects ejected from a near satellite
    • Knollman, G. C., and Pyron, B. O., "Relative Trajectories of Objects Ejected from a Near Satellite," AIAA Journal, Vol. 1, No. 2, 1963, pp. 424-429.
    • (1963) AIAA Journal , vol.1 , Issue.2 , pp. 424-429
    • Knollman, G.C.1    Pyron, B.O.2
  • 5
    • 85003321464 scopus 로고
    • Elliptic elements in terms of small increments of position and velocity components
    • de Vries, J. P., "Elliptic Elements in Terms of Small Increments of Position and Velocity Components," AIAA Journal, Vol. 1, No. 11, 1963, pp. 2626-2629.
    • (1963) AIAA Journal , vol.1 , Issue.11 , pp. 2626-2629
    • De Vries, J.P.1
  • 6
    • 85003383727 scopus 로고
    • Second approximation to the solution of rendezvous equations
    • London, H. S., "Second Approximation to the Solution of Rendezvous Equations," AIAA Journal, Vol. 1, No. 7, 1963, pp. 1691-1693.
    • (1963) AIAA Journal , vol.1 , Issue.7 , pp. 1691-1693
    • London, H.S.1
  • 7
    • 0003970092 scopus 로고    scopus 로고
    • Second-order relative motion equations
    • American Astronautical Society, AAS Paper 01-474, July-Aug.
    • Karlgaard, C. D., and Lutze, F. H., "Second-Order Relative Motion Equations," American Astronautical Society, AAS Paper 01-474, July-Aug. 2001.
    • (2001)
    • Karlgaard, C.D.1    Lutze, F.H.2
  • 8
    • 0001229316 scopus 로고    scopus 로고
    • Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies
    • American Astronautical Society, AAS Paper 00-012, Feb.
    • 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, AAS Paper 00-012, Feb. 2000.
    • (2000)
    • Alfriend, K.T.1    Schaub, H.2    Gim, D.-W.3
  • 9
    • 4243972841 scopus 로고    scopus 로고
    • Maintaining periodic trajectories with the first-order nonlinear hill's equations
    • American Astronautical Society, AAS Paper 01-473, July-Aug.
    • Mitchell, J. W., and Richardson, D. L., "Maintaining Periodic Trajectories with the First-Order Nonlinear Hill's Equations," American Astronautical Society, AAS Paper 01-473, July-Aug. 2001.
    • (2001)
    • Mitchell, J.W.1    Richardson, D.L.2
  • 10
    • 0036914740 scopus 로고    scopus 로고
    • A solution to the elliptic rendezvous problem with time as the independent variable
    • American Astronautical Society, AAS Paper 02-144, Jan.
    • Broucke, R. A., "A Solution to the Elliptic Rendezvous Problem with Time as the Independent Variable," American Astronautical Society, AAS Paper 02-144, Jan. 2002.
    • (2002)
    • Broucke, R.A.1
  • 11
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    • New state transition matrix for relative motion on an arbitrary elliptical orbit
    • Yamanaka, K., and Ankersen, F., "New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 1, 2002, pp. 60-67.
    • (2002) Journal of Guidance, Control, and Dynamics , vol.25 , Issue.1 , pp. 60-67
    • Yamanaka, K.1    Ankersen, F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.