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Volumn 221, Issue 5, 2007, Pages 767-774

Almost periodic relative orbits under J2 perturbations

Author keywords

Almost periodic orbits; J2 perturbation; Spacecraft formation flying

Indexed keywords

FEEDBACK CONTROL; ITERATIVE METHODS; NUMERICAL METHODS; PERTURBATION TECHNIQUES; SPACECRAFT;

EID: 36749039268     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/09544100JAERO200     Document Type: Article
Times cited : (11)

References (15)
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    • (2003) J. Guid. Control Dyn , vol.26 , Issue.2 , pp. 214-223
    • Vaddi, S.S.1    Vadali, S.R.2    Alfriend, K.T.3
  • 3
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    • 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. J. Guid. Control Dyn., 2002, 25(1), 48-59.
    • (2002) J. Guid. Control Dyn , vol.25 , Issue.1 , pp. 48-59
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  • 4
    • 1242263446 scopus 로고    scopus 로고
    • A third-order analytical solution for relative motion with a circular reference orbit
    • Richardson, D. L. and Mitchell, J. W. A third-order analytical solution for relative motion with a circular reference orbit. J. Astronaut. Sci., 2003, 51(1), 1-12.
    • (2003) J. Astronaut. Sci , vol.51 , Issue.1 , pp. 1-12
    • Richardson, D.L.1    Mitchell, J.W.2
  • 5
    • 32544432981 scopus 로고    scopus 로고
    • Guibout, V. M. and Scheeres, D. J. Spacecraft formation dynamics and design. J. Guid. Control Dyn., 2006, 29(1), 121-133.
    • Guibout, V. M. and Scheeres, D. J. Spacecraft formation dynamics and design. J. Guid. Control Dyn., 2006, 29(1), 121-133.
  • 6
    • 38149067500 scopus 로고    scopus 로고
    • Bounded relative motion using canonical epicyclic orbital elements
    • Copper Mountain, CO, USA, 23-27 January, paper AAS 05-186
    • Kasdin, N. J. and Kolemen, E. Bounded relative motion using canonical epicyclic orbital elements. In AAS/AIAA Spaceflight Mechanics Meeting, Copper Mountain, CO, USA, 23-27 January 2005, paper AAS 05-186.
    • (2005) AAS/AIAA Spaceflight Mechanics Meeting
    • Kasdin, N.J.1    Kolemen, E.2
  • 7
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    • 2 invariant relative orbits for spacecraft formations
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    • (2001) Celest. Mech. Dyn. Astr , vol.79 , pp. 77-95
    • Schaub, H.1    Alfriend, K.T.2
  • 10
    • 34247103664 scopus 로고    scopus 로고
    • Analysis and control of convenient orbital configuration for formation flying missions
    • Tampa, FL, USA, 22-26 January, paper AAS 06-120
    • Sabatini, M., Bevilacqua, R., Pantaleoni, M., and Izzo, D. Analysis and control of convenient orbital configuration for formation flying missions. In AAS/AIAA Spaceflight Mechanics Meeting, Tampa, FL, USA, 22-26 January 2005, paper AAS 06-120.
    • (2005) AAS/AIAA Spaceflight Mechanics Meeting
    • Sabatini, M.1    Bevilacqua, R.2    Pantaleoni, M.3    Izzo, D.4
  • 11
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    • An adaptive Newton-Picard algorithm with subspace iteration for computing periodic solutions
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  • 12
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  • 13
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  • 14
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    • Melton, R. G. Time-explicit representation of relative motion between elliptical orbits. J. Guid. Control Dyn., 2003, 23(4), 604-610.
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    • Melton, R.G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.