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Volumn , Issue , 2013, Pages 1584-1589

Formation flying of small satellites using suboptimal MPSP guidance

Author keywords

Model Predictive Static Programming; MPSP; Satellite Formation Flying

Indexed keywords

EQUATIONS OF STATE; NONLINEAR EQUATIONS; ORBITS; RICCATI EQUATIONS;

EID: 84883502996     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2013.6580061     Document Type: Conference Paper
Times cited : (5)

References (13)
  • 1
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    • (2012) Applications and Communications Key Issues
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  • 2
    • 84959130465 scopus 로고    scopus 로고
    • Initial condition and fuel optimal control for formation flying satellites
    • (Portland, USA), August
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    • (1999) AIAA Guidance, Navigation and Control Conference
    • Vadali, H.S.S.R.1    Alfrend, K.T.2
  • 3
    • 77957377823 scopus 로고    scopus 로고
    • Trajectory keeping in satellite formation flying via robust periodic control
    • K. L. M. H. S. Ahn and Y. Q. Chen, "Trajectory keeping in satellite formation flying via robust periodic control, " International Journal Of Robust And Non-Linear Control, vol. 20, pp. 1655-1666, 2010.
    • (2010) International Journal of Robust and Non-Linear Control , vol.20 , pp. 1655-1666
    • Ahn, K.L.M.H.S.1    Chen, Y.Q.2
  • 4
    • 80052263709 scopus 로고    scopus 로고
    • Satellite formation reconfiguration & station keeping using sdre technique
    • S.-Y. P. H.-E. Park and K.-H. Choi, "Satellite formation reconfiguration & station keeping using sdre technique, " Aerospace Science And Technology, vol. 15, pp. 440-452, 2011.
    • (2011) Aerospace Science and Technology , vol.15 , pp. 440-452
    • Park, S.-Y.P.H.-E.1    Choi, K.-H.2
  • 5
    • 0036062357 scopus 로고    scopus 로고
    • A study of linear versus nonlinear control techniques for the reconfiguration of satellite formations
    • D. J. D. J. Irvin, "A study of linear versus nonlinear control techniques for the reconfiguration of satellite formations, " Advances in the Astronautical Sciences, pp. 589-608, 2002.
    • (2002) Advances in the Astronautical Sciences , pp. 589-608
    • Irvin, D.J.D.J.1
  • 6
    • 64349108343 scopus 로고    scopus 로고
    • Model predictive static programming: A computaionally efficient technique for suboptimal control design
    • R. Padhi and M. Kothari, "Model predictive static programming: A computaionally efficient technique for suboptimal control design, " International Journal of Innovative Computing, Information and Control, vol. 5, no. 2, pp. 399-411, 2009.
    • (2009) International Journal of Innovative Computing, Information and Control , vol.5 , Issue.2 , pp. 399-411
    • Padhi, R.1    Kothari, M.2
  • 7
    • 84855315718 scopus 로고    scopus 로고
    • Impact angle constrained suboptimal mpsp guidance of air-to-ground missiles
    • H. Oza and R. Padhi, "Impact angle constrained suboptimal mpsp guidance of air-to-ground missiles, " AIAA Journal of Guidance, Control, and Dynamics, vol. 35, no. 1, pp. 153-164, 2012.
    • (2012) AIAA Journal of Guidance, Control, and Dynamics , vol.35 , Issue.1 , pp. 153-164
    • Oza, H.1    Padhi, R.2
  • 11
    • 0001422127 scopus 로고
    • Terminal guidance for satellite rendezvous
    • W. H. Clohessy and R. S. Wiltshire, "Terminal guidance for satellite rendezvous, " Journal of the Aerospace Sciences, vol. 27, no. 5, pp. 653-658, 674, 1960.
    • (1960) Journal of the Aerospace Sciences , vol.27 , Issue.5 , pp. 653-658
    • Clohessy, W.H.1    Wiltshire, R.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.