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Volumn 56, Issue 8, 2005, Pages 705-720

Design of Earth-Mars transfer trajectories using evolutionary-branching technique

Author keywords

[No Author keywords available]

Indexed keywords

EVOLUTIONARY-BRANCHING TECHNIQUE; GEOSTATIONARY ORBIT; MARS EXPLORATION; SEQUENTIAL QUADRATIC PROGRAMMING (SQP);

EID: 14844360708     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2004.12.002     Document Type: Article
Times cited : (45)

References (19)
  • 2
    • 0030283607 scopus 로고    scopus 로고
    • Near-optimal low-thrust orbit transfers generated by a genetic algorithm
    • G. Rauwolf, and V. Coverstone-Carroll Near-optimal low-thrust orbit transfers generated by a genetic algorithm Journal of Spacecraft and Rockets 33 6 1996 859 862
    • (1996) Journal of Spacecraft and Rockets , vol.33 , Issue.6 , pp. 859-862
    • Rauwolf, G.1    Coverstone-Carroll, V.2
  • 4
    • 1542327384 scopus 로고    scopus 로고
    • A combination of evolution programming and SQP for WSB transfer optimisation
    • Milano, Italy, September 18-21
    • M. Vasile, G. Comoretto, A.E. Finzi, A combination of evolution programming and SQP for WSB transfer optimisation, AIRO2000, Milano, Italy, September 18-21, 2000.
    • (2000) AIRO2000
    • Vasile, M.1    Comoretto, G.2    Finzi, A.E.3
  • 5
    • 0037032706 scopus 로고    scopus 로고
    • Niching genetic algorithms-based characterization of geocentric orbits in the 3D elliptic restricted three-body problem
    • P. Gurfil, and N.J. Kasdin Niching genetic algorithms-based characterization of geocentric orbits in the 3D elliptic restricted three-body problem Computer Methods in Applied Mechanics and Engineering 191 49-50 2002 5673 5696
    • (2002) Computer Methods in Applied Mechanics and Engineering , vol.191 , Issue.49-50 , pp. 5673-5696
    • Gurfil, P.1    Kasdin, N.J.2
  • 12
    • 0032552250 scopus 로고    scopus 로고
    • A global optimization method, alphaBB, for general twice-differentiable constrained NLPs-I. Theoretical advances
    • C.S. Adjiman, S. Dallwing, C.A. Floudas, and A. Neumaier A global optimization method, alphaBB, for general twice-differentiable constrained NLPs-I. Theoretical advances Computers and Chemical Engineering 22 1998 1137 1158
    • (1998) Computers and Chemical Engineering , vol.22 , pp. 1137-1158
    • Adjiman, C.S.1    Dallwing, S.2    Floudas, C.A.3    Neumaier, A.4
  • 16
    • 1542330031 scopus 로고    scopus 로고
    • A global approach to optimal space trajectory design
    • AAS-03-141 Puerto Rico, 9-13 February
    • M. Vasile, A global approach to optimal space trajectory design, AAS-03-141,13th AAS/AIAA Space Flight Mechanics Meeting, Puerto Rico, 9-13 February 2003.
    • (2003) 13th AAS/AIAA Space Flight Mechanics Meeting
    • Vasile, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.