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Volumn 26, Issue 6, 2003, Pages 846-854

Attitude Control of a Reentry Vehicle with Internal Dynamics

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; INVERSE KINEMATICS; NEURAL NETWORKS; PARAMETER ESTIMATION; PERTURBATION TECHNIQUES; REENTRY; ROBUSTNESS (CONTROL SYSTEMS); SYSTEMS ANALYSIS;

EID: 0344898945     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.6928     Document Type: Article
Times cited : (48)

References (15)
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    • Enns, D.1    Bugajski, D.2    Hendrick, R.3    Stein, G.4
  • 3
    • 0030284815 scopus 로고    scopus 로고
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    • Reiner, J.1    Balas, G.J.2    Garrard, W.L.3
  • 5
    • 0026897471 scopus 로고
    • Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft
    • Snell, S. A., Enns, D. F., and Garrard, W. L., "Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 976-984.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.4 , pp. 976-984
    • Snell, S.A.1    Enns, D.F.2    Garrard, W.L.3
  • 6
    • 0032301440 scopus 로고    scopus 로고
    • Nonlinear Adaptive Flight Control Using Neural Networks
    • Calise, A. J., and Rysdyk, R. T., "Nonlinear Adaptive Flight Control Using Neural Networks," IEEE Control System Magazine, Vol 18. No. 6, 1998, pp. 14-25.
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    • Calise, A.J.1    Rysdyk, R.T.2
  • 7
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    • Output-Redefinition Based on Robust Zero Dynamics
    • Aug.
    • Kim, S.-G., and Tahk, M.-J., "Output-Redefinition Based on Robust Zero Dynamics," AIAA Paper 98-4493, Aug. 1998.
    • (1998) AIAA Paper , vol.4493
    • Kim, S.-G.1    Tahk, M.-J.2
  • 8
    • 84893296512 scopus 로고
    • Tracking Nonlinear Non-Minimum Phase Systems Using Sliding Control
    • Gopalswamy, S., and Hedrick, J. K., "Tracking Nonlinear Non-Minimum Phase Systems Using Sliding Control," International Journal of Control, Vol. 57, No. 5, 1993, pp. 1141-1158.
    • (1993) International Journal of Control , vol.57 , Issue.5 , pp. 1141-1158
    • Gopalswamy, S.1    Hedrick, J.K.2
  • 9
    • 0026997890 scopus 로고
    • Control of a High Performance Aircraft with Unacceptable Zero Dynamics
    • Inst. of Electrical and Electronics Engineers Publications, Piscataway, NJ
    • Gopalswamy, S., and Hedrick, J. K., "Control of a High Performance Aircraft with Unacceptable Zero Dynamics," Proceedings of the American Control Conference, Inst. of Electrical and Electronics Engineers Publications, Piscataway, NJ, 1992, pp. 1834-1838.
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  • 10
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  • 12
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    • Polycarpou, M.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.