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Volumn 96, Issue 3-4, 2006, Pages 289-309

A sixth-order accurate scheme for solving two-point boundary value problems in astrodynamics

Author keywords

Bicircular four body problem; Halo orbits; Non linear boundary value problem; Restricted three body problem

Indexed keywords


EID: 33751563469     PISSN: 09232958     EISSN: 15729478     Source Type: Journal    
DOI: 10.1007/s10569-006-9047-4     Document Type: Article
Times cited : (28)

References (17)
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    • Masdemont, J.J.: High order expansions of invariant manifolds of libration point orbits with applications to mission design. Dyn. Sys.: An Int. J. 20, 59-113 (2005)
    • (2005) Dyn. Sys.: An Int. J. , vol.20 , pp. 59-113
    • Masdemont, J.J.1
  • 9
    • 28144437450 scopus 로고
    • Numerical solution of two-point boundary value problems
    • Quartapelle, L., Rebay, S.: Numerical solution of two-point boundary value problems, J. Comput. Phys. 86, 314-354 (1990)
    • (1990) J. Comput. Phys. , vol.86 , pp. 314-354
    • Quartapelle, L.1    Rebay, S.2
  • 11
    • 0019080136 scopus 로고
    • Halo orbit formulation for the ISEE-3 mission
    • Richardson, D.L.: Halo orbit formulation for the ISEE-3 mission. J. Guid. Contr. 3, 543-548 (1980)
    • (1980) J. Guid. Contr. , vol.3 , pp. 543-548
    • Richardson, D.L.1
  • 12
    • 15744382908 scopus 로고    scopus 로고
    • Low-thrust variable-specific-impulse transfers and guidance to unstable periodic orbits
    • Senent, J., Oeampo, C., Capella, A.: Low-thrust variable-specific-impulse transfers and guidance to unstable periodic orbits. J. Guid. Conlr. Dyn, 28, 280-290 (2005)
    • (2005) J. Guid. Conlr. Dyn , vol.28 , pp. 280-290
    • Senent, J.1    Oeampo, C.2    Capella, A.3
  • 13
    • 0000879938 scopus 로고
    • The bicircular model near the triangular libration points of the RTBP
    • Roy, A.E., Steves, B.A. (eds.). Plenum Press. New York
    • Simó, C., Gómez, G., Jorba, Á., Masdemont, J.: The bicircular model near the triangular libration points of the RTBP. In: Roy, A.E., Steves, B.A. (eds.) From Newton to Chaos, pp. 343-370. Plenum Press. New York (1995)
    • (1995) From Newton to Chaos , pp. 343-370
    • Simó, C.1    Gómez, G.2    Jorba, Á.3    Masdemont, J.4
  • 16
    • 0010197598 scopus 로고    scopus 로고
    • The geometry of halo orbits in the circular restricted three-body problem
    • University of Minnesota. GCG95
    • Thurman, R., Worfolk, P.: The Geometry of Halo Orbits in the Circular Restricted Three-Body Problem. Geometry Center Research Report, University of Minnesota. GCG95 (1996)
    • (1996) Geometry Center Research Report
    • Thurman, R.1    Worfolk, P.2
  • 17
    • 12744258082 scopus 로고    scopus 로고
    • Sun-perturbated earth-to-moon transfers with low energy and moderate flight time
    • Yagasaki, K.: Sun-perturbated earth-to-moon transfers with low energy and moderate flight time. Celest. Mech. Dyn. Astr. 90, 197-212 (2004)
    • (2004) Celest. Mech. Dyn. Astr. , vol.90 , pp. 197-212
    • Yagasaki, K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.