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Volumn 26, Issue 1, 2003, Pages 50-62

Optimal two-impulse rendezvous using multiple-revolution lambert solutions

Author keywords

[No Author keywords available]

Indexed keywords

GLOBAL OPTIMIZATION; MATHEMATICAL MODELS; ORBITAL TRANSFER; ORBITS; SPACECRAFT;

EID: 0037262476     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.5014     Document Type: Article
Times cited : (163)

References (11)
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    • Sparks, A.1
  • 2
    • 0032785314 scopus 로고    scopus 로고
    • Synchronized formation rotation and attitude control of multiple free-flying spacecraft
    • Wang, P. K., Hadaegh, F. Y., and Lau, K., "Synchronized Formation Rotation and Attitude Control of Multiple Free-Flying Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 22, No. 1, 1999, pp. 28-35.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.1 , pp. 28-35
    • Wang, P.K.1    Hadaegh, F.Y.2    Lau, K.3
  • 3
    • 0013101488 scopus 로고    scopus 로고
    • Dynamics and control of spacecraft formations: Challenges and some solutions
    • Univelt, Inc., San Diego, CA
    • Alfriend, K. T., and Schaub, H., "Dynamics and Control of Spacecraft Formations: Challenges and Some Solutions," Advances in the Astronautical Sciences, Vol. 106, Univelt, Inc., San Diego, CA, 2000, pp. 205-223.
    • (2000) Advances in the Astronautical Sciences , vol.106 , pp. 205-223
    • Alfriend, K.T.1    Schaub, H.2
  • 4
    • 0024682359 scopus 로고
    • Refurbishable satellites for low cost communications systems
    • June
    • Helton, M. R., "Refurbishable Satellites for Low Cost Communications Systems," Space Communication and Broadcasting, Vol. 6, June 1989, pp. 379-385.
    • (1989) Space Communication and Broadcasting , vol.6 , pp. 379-385
    • Helton, M.R.1
  • 5
    • 0013097518 scopus 로고    scopus 로고
    • A class of optimal two-impulse rendezvous using multiple-revolution lambert solutions
    • Univelt, Inc., San Diego, CA
    • Prussing, J. E., "A Class of Optimal Two-Impulse Rendezvous Using Multiple-Revolution Lambert Solutions," Advances in the Astronautical Sciences, Vol. 106, Univelt, Inc., San Diego, CA, 2000, pp. 17-39.
    • (2000) Advances in the Astronautical Sciences , vol.106 , pp. 17-39
    • Prussing, J.E.1
  • 6
    • 85007677551 scopus 로고
    • Primer vector on fixed-Time impulsive trajectories
    • Lion, P. M., and Handelsman, M., "Primer Vector on Fixed-Time Impulsive Trajectories," AIAA Journal, Vol. 6, No. 1, 1968, pp. 127-132.
    • (1968) AIAA Journal , vol.6 , Issue.1 , pp. 127-132
    • Lion, P.M.1    Handelsman, M.2
  • 8
    • 0018520381 scopus 로고
    • Geometrical interpretation of the Angles α and β in lambert's problem
    • Prussing, J. E., "Geometrical Interpretation of the Angles α and β in Lambert's Problem," Journal of Guidance Control, and Dynamics, Vol. 2, No. 5, 1979, pp. 442-443.
    • (1979) Journal of Guidance Control, and Dynamics , vol.2 , Issue.5 , pp. 442-443
    • Prussing, J.E.1
  • 9
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    • Prentice-Hall, Englewood Cliffs, NJ
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    • Hale, F.J.1
  • 10
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    • Terminal guidance system for satellite rendezvous
    • Sept.
    • Clohessy, W. H., and Wiltshire, R. S., "Terminal Guidance System for Satellite Rendezvous," Journal of Aerospace Sciences, Vol. 27, Sept. 1960, pp. 653-658.
    • (1960) Journal of Aerospace Sciences , vol.27 , pp. 653-658
    • Clohessy, W.H.1    Wiltshire, R.S.2
  • 11
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    • (1993) Orbital Mechanics , pp. 99-154
    • Prussing, J.E.1    Conway, B.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.