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Volumn 1, Issue , 2005, Pages 158-169

J2-Modified GVE-based MPC for formation flying spacecraft

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; LINEARIZATION; MATHEMATICAL MODELS; ORBITS; PARAMETER ESTIMATION; VARIATIONAL TECHNIQUES;

EID: 29744438232     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-5833     Document Type: Conference Paper
Times cited : (22)

References (21)
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    • Control, and Dynamics (0731-5090), Jan.-Feb.
    • G. Inalhan, M. Tillerson, and J. How, "Relative Dynamics & Control of Spacecraft Formations in Eccentric Orbits," AIAA Journal of Guidance, Control, and Dynamics (0731-5090), vol. 25, no. 1, Jan.-Feb. 2002, p. 48-59.
    • (2002) AIAA Journal of Guidance , vol.25 , Issue.1 , pp. 48-59
    • Inalhan, G.1    Tillerson, M.2    How, J.3
  • 4
    • 0036465418 scopus 로고    scopus 로고
    • Coordination and control of distributed spacecraft systems using convex optimization techniques
    • Feb.-Mar.
    • M. Tillerson, G. Inalhan, and J. How, "Coordination and Control of Distributed Spacecraft Systems Using Convex Optimization Techniques," Int. Journal of Robust and Nonlinear Control, vol 12, Issue 2-3, Feb.-Mar. 2002, p.207-242.
    • (2002) Int. Journal of Robust and Nonlinear Control , vol.12 , Issue.2-3 , pp. 207-242
    • Tillerson, M.1    Inalhan, G.2    How, J.3
  • 5
    • 0027735651 scopus 로고
    • Low thrust OTV guidance using lyapunov optimal feedback control techniques
    • Victoria, B.C., Canada, Aug. 16-19 Paper No. AAS 93-680
    • Ilgen, M.R., "Low Thrust OTV Guidance using Lyapunov Optimal Feedback Control Techniques," AAS/AIAA Astrodynamics Specialist Conference, Victoria, B.C., Canada, Aug. 16-19 1993, Paper No. AAS 93-680.
    • (1993) AAS/AIAA Astrodynamics Specialist Conference
    • Ilgen, M.R.1
  • 6
  • 8
    • 0344514833 scopus 로고    scopus 로고
    • Control-theoretic analysis of low-thrust orbital transfer using orbital elements
    • November-December
    • P. Gurfil, "Control-Theoretic Analysis of Low-Thrust Orbital Transfer Using Orbital Elements," AIAA Journal of Guidance, Control, and Dynamics, vol. 26, no. 6, November-December 2003, p. 979-983.
    • (2003) AIAA Journal of Guidance, Control, and Dynamics , vol.26 , Issue.6 , pp. 979-983
    • Gurfil, P.1
  • 9
    • 29744461792 scopus 로고    scopus 로고
    • 2 Invariant relative orbits for spacecraft formations
    • (Goddard Space Flight Center, Greenbelt, Maryland), January 18-20, Paper No. 11
    • 2 Invariant Relative Orbits for Spacecraft Formations," Flight Mechanics Symposium, (Goddard Space Flight Center, Greenbelt, Maryland), January 18-20, 2002, Paper No. 11.
    • (2002) Flight Mechanics Symposium
    • Schaub, H.1    Alfriend, K.T.2
  • 12
    • 3242746623 scopus 로고    scopus 로고
    • Cambridge University Press, Cambridge
    • Greenwood, D.T., Advanced Dynamics, Cambridge University Press, Cambridge, 2003.
    • (2003) Advanced Dynamics
    • Greenwood, D.T.1
  • 13
    • 85085779454 scopus 로고    scopus 로고
    • A preliminary study for a tetrahedron formation - Quality factors and visualization (spacecraft formation flying)
    • Aug
    • J. Guzman and C. Schiff, "A Preliminary Study for a Tetrahedron Formation - Quality Factors and Visualization (Spacecraft Formation Flying)," AIAA/AAS Astro. Specialists Conf., Aug 2002.
    • (2002) AIAA/AAS Astro. Specialists Conf.
    • Guzman, J.1    Schiff, C.2
  • 17
    • 85087595840 scopus 로고    scopus 로고
    • Virtual structure based spacecraft formation control with formation feedback
    • Aug.
    • W. Ren, and R. Beard, "Virtual Structure Based Spacecraft Formation Control with Formation Feedback," presented at, the AIAA GN&C Conference, Aug. 2002.
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    • Ren, W.1    Beard, R.2
  • 18
    • 0344898941 scopus 로고    scopus 로고
    • State transition matrix of relative motion for the perturbed noncircular reference orbit
    • Nov.-Dec.
    • D.W. Gim and K.T. Alfriend, "State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit," AIAA Journal of Guidance, Control, and Dynamics, vol. 26, no. 6, Nov.-Dec. 2003, p. 956-971.
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    • Gim, D.W.1    Alfriend, K.T.2
  • 19
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    • S.M. Thesis, Massachusetts Institute of Technology, Dept. Aeronautics and Astronautics, June
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    • Breger, L.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.