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Volumn 120, Issue II, 2005, Pages 1381-1398

Bounded, periodic relative motion using canonical epicyclic orbital elements

Author keywords

[No Author keywords available]

Indexed keywords

EPICYCLE ORBITAL ELEMENTS; NO-DRIFT CONDITIONS; REFERENCE ORBITS;

EID: 26944472373     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (18)
  • 1
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  • 5
    • 1042298574 scopus 로고    scopus 로고
    • Nonlinear modeling and control of spacecraft relative motion in the configuration space
    • January
    • P. Gurfil and N.J. Kasdin. Nonlinear modeling and control of spacecraft relative motion in the configuration space. Journal of Guidance, Control, and Dynamics, 27(1):154-157, January 2004.
    • (2004) Journal of Guidance, Control, and Dynamics , vol.27 , Issue.1 , pp. 154-157
    • Gurfil, P.1    Kasdin, N.J.2
  • 6
    • 26944440670 scopus 로고    scopus 로고
    • Canonical modelling of relative spacecraft motion via epicyclic orbital elements
    • To Be Published
    • N.J. Kasdin, P. Gurfil, and E. Kolemen. Canonical modelling of relative spacecraft motion via epicyclic orbital elements. Celestial Mechanics and Dynamical Astronomy, To Be Published, 2005.
    • (2005) Celestial Mechanics and Dynamical Astronomy
    • Kasdin, N.J.1    Gurfil, P.2    Kolemen, E.3
  • 8
    • 23844441190 scopus 로고    scopus 로고
    • An orbital elements approach to the nonlinear formation flying problem
    • October. Toulouse, France
    • K.T. Alfriend and H. Yan. An orbital elements approach to the nonlinear formation flying problem. In International Formation Flying Symposium, October 2002. Toulouse, France.
    • (2002) International Formation Flying Symposium
    • Alfriend, K.T.1    Yan, H.2
  • 9
    • 1242263446 scopus 로고    scopus 로고
    • A third-order analytical solution for relative motion with a circular reference orbit
    • January-February
    • D.L. Richardson and J.W. Mitchell. A third-order analytical solution for relative motion with a circular reference orbit. The Journal of the Astronautical Sciences, 51(1), January-February 2003.
    • (2003) The Journal of the Astronautical Sciences , vol.51 , Issue.1
    • Richardson, D.L.1    Mitchell, J.W.2
  • 10
    • 0034165585 scopus 로고    scopus 로고
    • Dynamics and control of spacecraft formations: Challenges and some solutions
    • March-April
    • K.T. Alfriend and H. Schaub. Dynamics and control of spacecraft formations: Challenges and some solutions. The Journal of the Astronautical Sciences, 48(2):249-267, March-April 2000.
    • (2000) The Journal of the Astronautical Sciences , vol.48 , Issue.2 , pp. 249-267
    • Alfriend, K.T.1    Schaub, H.2
  • 12
    • 19944380041 scopus 로고    scopus 로고
    • Motion of a satellite under the influence of an oblate earth
    • University of Colorado, Boulder, June
    • G. H. Born. Motion of a satellite under the influence of an oblate earth. Technical Report ASEN 3200, University of Colorado, Boulder, June 2001.
    • (2001) Technical Report , vol.ASEN 3200
    • Born, G.H.1
  • 14
    • 0345581673 scopus 로고    scopus 로고
    • Gauge symmetry of the n-body problem in the hamilton-jacobi approach
    • M. Efroimsky and P. Goldreich. Gauge symmetry of the n-body problem in the hamilton-jacobi approach. Journal of Mathematical Physics, 44:5958-5977, 2003.
    • (2003) Journal of Mathematical Physics , vol.44 , pp. 5958-5977
    • Efroimsky, M.1    Goldreich, P.2
  • 15
    • 1542366376 scopus 로고    scopus 로고
    • Gauge freedom in the n-body problem of celestial mechanics
    • M. Efroimsky and P. Goldreich. Gauge freedom in the n-body problem of celestial mechanics. Astronomy and Astrophysics, 415:1187-1899, 2004.
    • (2004) Astronomy and Astrophysics , vol.415 , pp. 1187-1899
    • Efroimsky, M.1    Goldreich, P.2
  • 16
    • 0023452328 scopus 로고
    • Fuel-optimal rendezvous near a point in general keplerian orbit
    • November
    • T.E. Carter and M. Humi. Fuel-optimal rendezvous near a point in general keplerian orbit. Journal of Guidance, Control and Dynamics, 10(6):567-573, November 1987.
    • (1987) Journal of Guidance, Control and Dynamics , vol.10 , Issue.6 , pp. 567-573
    • Carter, T.E.1    Humi, M.2
  • 17
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    • Relative dynamics and control of spacecraft formations in eccentric orbits
    • January
    • G. Inalhan, M. Tillerson, and J.P. How. Relative dynamics and control of spacecraft formations in eccentric orbits. Journal of Guidance, Control and Dynamics, 25(1):48-60, January 2002.
    • (2002) Journal of Guidance, Control and Dynamics , vol.25 , Issue.1 , pp. 48-60
    • Inalhan, G.1    Tillerson, M.2    How, J.P.3
  • 18
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    • Relative spacecraft motion: A hamiltonian approach to eccentricity perturbations
    • February. Maui, HI
    • E. Kolemen and N.J. Kasdin. Relative spacecraft motion: A hamiltonian approach to eccentricity perturbations. In Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, number AAS-04-294, February 2004. Maui, HI.
    • (2004) Proceedings of the AAS/AIAA Space Flight Mechanics Meeting , Issue.AAS-04-294
    • Kolemen, E.1    Kasdin, N.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.