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Volumn 3, Issue , 2004, Pages 1477-1489

Dynamics and fuzzy control for formation flying with elliptical reference orbits

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; AUTOMATION; COMPUTER SIMULATION; FUEL CONSUMPTION; FUZZY CONTROL; GRAVITATIONAL EFFECTS; ORBITS; SPACECRAFT PROPULSION;

EID: 19944369791     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5025     Document Type: Conference Paper
Times cited : (5)

References (12)
  • 1
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    • Relative dynamics and control of spacecraft formations in eccentric orbits
    • Jan.-Feb.
    • Inalhan, G., Tillerson, M., and How, J. P., "Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits," Journal of Guidance, Control and Dynamics, Vol. 25, No. 1, Jan.-Feb. 2002, pp. 48-59.
    • (2002) Journal of Guidance, Control and Dynamics , vol.25 , Issue.1 , pp. 48-59
    • Inalhan, G.1    Tillerson, M.2    How, J.P.3
  • 2
    • 0001422127 scopus 로고
    • Terminal guidance system for satellite rendezvous
    • Clohessy, W. H. and Wiltshire, R. S., "Terminal Guidance System for Satellite Rendezvous," Journal of Aerospace Science, Vol. 27, No. 9, 1960, pp. 653-658.
    • (1960) Journal of Aerospace Science , vol.27 , Issue.9 , pp. 653-658
    • Clohessy, W.H.1    Wiltshire, R.S.2
  • 3
    • 0025207410 scopus 로고
    • New form for the optimal rendezvous equations near a keplerian orbit
    • Carter, T. E., "New Form for the Optimal Rendezvous Equations near a Keplerian Orbit," Journal of Guidance, Control and Dynamics, Vol. 13, No. 1, 1990, pp. 183-186.
    • (1990) Journal of Guidance, Control and Dynamics , vol.13 , Issue.1 , pp. 183-186
    • Carter, T.E.1
  • 4
    • 0036154546 scopus 로고    scopus 로고
    • New state transition matrix for relative motion on an arbitrary elliptical orbit
    • Jan.-Feb.
    • Yamanaka, K. and Ankersen, F., "New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit," Journal of Guidance, Control and Dynamics, Vol. 25, No. 1, Jan.-Feb. 2002, pp. 60-66.
    • (2002) Journal of Guidance, Control and Dynamics , vol.25 , Issue.1 , pp. 60-66
    • Yamanaka, K.1    Ankersen, F.2
  • 5
    • 0022025257 scopus 로고
    • Formationkeeping for a pair of satellites in a circular orbit
    • Mar.-Apr.
    • Vassar, R. II. and Sherwood, R. D., "Formationkeeping for a Pair of Satellites in a Circular Orbit," Journal of Guidance, Control and Dynamics, Vol. 8, No. 2, Mar.-Apr. 1985, pp. 235-242.
    • (1985) Journal of Guidance, Control and Dynamics , vol.8 , Issue.2 , pp. 235-242
    • Vassar II, R.1    Sherwood, R.D.2
  • 7
    • 34250663364 scopus 로고    scopus 로고
    • Fuzzy supervised optimal regulator for spacecraft formation flying
    • Chicago, IL, 24-26 July
    • Rahnamai, K., Arabshahi, P., and Gray, A., "Fuzzy supervised optimal regulator for spacecraft formation flying," The 21st NAFIPS International Conference, Chicago, IL, 24-26 July 2003.
    • (2003) The 21st NAFIPS International Conference
    • Rahnamai, K.1    Arabshahi, P.2    Gray, A.3
  • 8
    • 0002805393 scopus 로고    scopus 로고
    • Adaptive control of formation flying spacecraft for interferometry
    • Rio Patras, Greece
    • Hadaegh, F. Y., Lu, W. M., and Wang, P. K. C., "Adaptive control of formation flying spacecraft for interferometry," IFAC Conference on Large Scale Systems, Rio Patras, Greece, 1998, pp. 97-102.
    • (1998) IFAC Conference on Large Scale Systems , pp. 97-102
    • Hadaegh, F.Y.1    Lu, W.M.2    Wang, P.K.C.3
  • 9
    • 0000160268 scopus 로고    scopus 로고
    • Adaptive nonlinear control of multiple spacecraft formation flying
    • May-Jun.
    • de Queiroz, M. S., Kapila, V., and Yan, Q., "Adaptive Nonlinear Control of Multiple Spacecraft Formation Flying," Journal of Guidance, Control and Dynamics, Vol. 23, No. 3, May-Jun. 2000, pp. 385-390.
    • (2000) Journal of Guidance, Control and Dynamics , vol.23 , Issue.3 , pp. 385-390
    • De Queiroz, M.S.1    Kapila, V.2    Yan, Q.3
  • 10
    • 0034547454 scopus 로고    scopus 로고
    • Nonlinear dynamics and output feedback control of multiple spacecraft in elliptical orbits
    • Chicago, IL, 28-30 June
    • Yan, Q., Yang, G., Kapila, V., and de Queiroz, M. S., "Nonlinear dynamics and output feedback control of multiple spacecraft in elliptical orbits," American Control Conference, Chicago, IL, 28-30 June 2000, pp. 839-843.
    • (2000) American Control Conference , pp. 839-843
    • Yan, Q.1    Yang, G.2    Kapila, V.3    De Queiroz, M.S.4
  • 11
    • 0036465645 scopus 로고    scopus 로고
    • Adaptive output feedback tracking control of spacecraft formation
    • Feb.-Mar.
    • Wong, H., Kapila, V., and Sparks, A. G., "Adaptive Output Feedback Tracking Control of Spacecraft Formation," International Journal of Robust and Nonlinear Control, Vol. 12, No. 2-3, Feb.-Mar. 2002, pp. 117-139.
    • (2002) International Journal of Robust and Nonlinear Control , vol.12 , Issue.2-3 , pp. 117-139
    • Wong, H.1    Kapila, V.2    Sparks, A.G.3
  • 12
    • 0041766613 scopus 로고    scopus 로고
    • Linearized dynamic equations for spacecraft subject to J2 perturbations
    • Jul.-Aug.
    • Ross, I. M., "Linearized Dynamic Equations for Spacecraft Subject to J2 Perturbations," Journal of Guidance, Control and Dynamics, Vol. 26, No. 4, Jul.-Aug. 2003, pp. 657-659.
    • (2003) Journal of Guidance, Control and Dynamics , vol.26 , Issue.4 , pp. 657-659
    • Ross, I.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.