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Volumn , Issue , 2001, Pages

Constrained trajectory generation for micro-satellite formation flying

Author keywords

[No Author keywords available]

Indexed keywords


EID: 77955282093     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (57)

References (13)
  • 1
    • 0001422127 scopus 로고
    • Terminal guidance system for satellite rendezvous
    • W. Clohessy and R. Wiltshire. Terminal guidance system for satellite rendezvous. Journal of Aerospace Sciences, 27(9):653-658, 1960.
    • (1960) Journal of Aerospace Sciences , vol.27 , Issue.9 , pp. 653-658
    • Clohessy, W.1    Wiltshire, R.2
  • 2
    • 0029327262 scopus 로고
    • Flatness and defect of non-linear systems: Introductory theory and examples
    • M. Fliess, J. Levine, P. Martin, and P. Rouchon. Flatness and defect of non-linear systems: introductory theory and examples. International Journal of Control, 61(6):1327-1360, 1995.
    • (1995) International Journal of Control , vol.61 , Issue.6 , pp. 1327-1360
    • Fliess, M.1    Levine, J.2    Martin, P.3    Rouchon, P.4
  • 3
    • 0032690021 scopus 로고    scopus 로고
    • A Lie-Backlund approach to equivalence and flatness of nonlinear systems
    • M. Fliess, J. Levine, P. Martin, and P. Rouchon. A Lie-Backlund approach to equivalence and flatness of nonlinear systems. IEEE Trans. Auto. Cont., 44(5):928-937, 1999.
    • (1999) IEEE Trans. Auto. Cont , vol.44 , Issue.5 , pp. 928-937
    • Fliess, M.1    Levine, J.2    Martin, P.3    Rouchon, P.4
  • 5
    • 70350359744 scopus 로고    scopus 로고
    • Precise formation flying control of multiple spacecraft using carrier-phase differential GPS
    • number AAS 00-109
    • G. Inalhan, J. Busse, and J. How. Precise formation flying control of multiple spacecraft using carrier-phase differential GPS. In Proc. Guidance, Control and Navigation Conference, number AAS 00-109, 2000.
    • (2000) Proc. Guidance, Control and Navigation Conference
    • Inalhan, G.1    Busse, J.2    How, J.3
  • 7
    • 0029369425 scopus 로고
    • Fuel-optimal stationkeeping via differential inclusions
    • R. Kumar and H. Seywald. Fuel-optimal stationkeeping via differential inclusions. Journal of Guidance, Control, and Dynamics, 18(5):1156-1162, 1995.
    • (1995) Journal of Guidance Control, and Dynamics , vol.18 , Issue.5 , pp. 1156-1162
    • Kumar, R.1    Seywald, H.2
  • 8
    • 0034439330 scopus 로고    scopus 로고
    • A new computational approach to real-time trajectory generation for constrained mechanical systems
    • M. B. Milam, K. Mushambi, and R. M. Murray. A new computational approach to real-time trajectory generation for constrained mechanical systems. In IEEE Conference on Decision and Control, 2000.
    • (2000) IEEE Conference On Decision and Control
    • Milam, M.B.1    Mushambi, K.2    Murray, R.M.3
  • 11
    • 0033155839 scopus 로고    scopus 로고
    • Mitigation of differential perturbations in formation flying satellite clusters
    • Y. Sedwick, D. Miller, and E. Kong. Mitigation of differential perturbations in formation flying satellite clusters. Journal of Astronautical Sciences, 47(3 and 4):309-331, 1999.
    • (1999) Journal of Astronautical Sciences , vol.47 , Issue.3-4 , pp. 309-331
    • Sedwick, Y.1    Miller, D.2    Kong, E.3
  • 12
    • 84894439228 scopus 로고    scopus 로고
    • TechSat 21
    • TechSat 21. http: //www.vs.af rl.af.mil/vsd/techsat21/


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.