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Volumn 38, Issue 1, 1996, Pages 1-14

Optimal low-thrust rendezvous using equinoctial orbit elements

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; BOUNDARY VALUE PROBLEMS; DIFFERENTIAL EQUATIONS; EQUATIONS OF MOTION; INTEGRATION; LAGRANGE MULTIPLIERS; OPTIMIZATION; ORBITAL TRANSFER; ORBITS; STATISTICAL METHODS; VARIATIONAL TECHNIQUES;

EID: 0029716076     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/0094-5765(95)00121-2     Document Type: Article
Times cited : (47)

References (13)
  • 1
    • 0041538617 scopus 로고
    • A linear theory of optimum low-thrust rendezvous trajectories
    • F. W. Gobetz, A linear theory of optimum low-thrust rendezvous trajectories. JAS XII, 69-76 (1965).
    • (1965) JAS , vol.12 , pp. 69-76
    • Gobetz, F.W.1
  • 2
    • 85007706717 scopus 로고
    • Optimum low-thrust rendezvous and station keeping
    • T. N. Edelbaum, Optimum low-thrust rendezvous and station keeping. AIAA J. 2, No. 7 (1964).
    • (1964) AIAA J. , vol.2 , Issue.7
    • Edelbaum, T.N.1
  • 3
    • 0017487020 scopus 로고
    • Optimum low-thrust limited-power transfers between arbitrary elliptical orbits
    • J.-P. Marec and N. X. Vinh, Optimum low-thrust limited-power transfers between arbitrary elliptical orbits. Acta Astronautica 4, 511-540 (1977).
    • (1977) Acta Astronautica , vol.4 , pp. 511-540
    • Marec, J.-P.1    Vinh, N.X.2
  • 4
    • 0000927391 scopus 로고
    • On the equinoctial orbit elements
    • R. A. Broucke and P. J. Cefola, On the equinoctial orbit elements. Celestial Mech. 5, 303-310 (1972).
    • (1972) Celestial Mech. , vol.5 , pp. 303-310
    • Broucke, R.A.1    Cefola, P.J.2
  • 5
    • 0345418624 scopus 로고
    • Equinoctial orbit elements: Application to artificial satelite orbits
    • AIAA 72-937, Palo Alto, CA, 11-12 September
    • P. Cefola, Equinoctial orbit elements: application to artificial satelite orbits. AIAA 72-937, AIAA/AAS Astrodynamics Conference, Palo Alto, CA, 11-12 September (1972).
    • (1972) AIAA/AAS Astrodynamics Conference
    • Cefola, P.1
  • 7
    • 0043041473 scopus 로고
    • The long-term prediction of artificial satellite orbits
    • AIAA 74-170, Washington, DC, 30 January-1 February
    • P. Cefola, A. Long and G. Holloway, The long-term prediction of artificial satellite orbits. AIAA 74-170, AIAA 12th Aerospace Sciences Meeting, Washington, DC, 30 January-1 February (1974).
    • (1974) AIAA 12th Aerospace Sciences Meeting
    • Cefola, P.1    Long, A.2    Holloway, G.3
  • 8
    • 0345418625 scopus 로고
    • Equinoctial orbit elements: Application to optimal transfer problems
    • AIAA 90-2976, Portland, OR, 20-22 August
    • J. Kechichian, Equinoctial orbit elements: application to optimal transfer problems. AIAA 90-2976, AIAA/ AAS Astrodynamics Conference, Portland, OR, 20-22 August (1990).
    • (1990) AIAA/ AAS Astrodynamics Conference
    • Kechichian, J.1
  • 9
    • 0344556473 scopus 로고
    • Trajectory optimization with a modified set of equinoctial orbit elements
    • AAS/AIAA 91-524, Durango, CO, 19-22 August
    • J. Kechichian, Trajectory optimization with a modified set of equinoctial orbit elements. AAS/AIAA 91-524, Astrodynamics Specialist Conference, Durango, CO, 19-22 August (1991).
    • (1991) Astrodynamics Specialist Conference
    • Kechichian, J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.