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Volumn 21, Issue 3, 1998, Pages 508-515

Stability analysis of a missile control system with a dynamic inversion controller

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; MATHEMATICAL MODELS; MISSILES; STATE SPACE METHODS; SYSTEM STABILITY;

EID: 0032073491     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4266     Document Type: Article
Times cited : (89)

References (13)
  • 1
    • 0026856998 scopus 로고
    • Nonlinear Control Law with Application to High Angle-of-Attack Flight
    • Bugajski, D. J., and Enns, D. F., "Nonlinear Control Law with Application to High Angle-of-Attack Flight," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 3, 1992, pp. 761-767.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.3 , pp. 761-767
    • Bugajski, D.J.1    Enns, D.F.2
  • 2
    • 84999286973 scopus 로고
    • Missile Flight Control with Dynamic Inversion and Structured Singular Value Synthesis
    • (Scottsdale, AZ), AIAA, Washington, DC
    • McFarland, M. B., and D'Souza, C. N., "Missile Flight Control with Dynamic Inversion and Structured Singular Value Synthesis," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Scottsdale, AZ), AIAA, Washington, DC, 1994, pp. 544-550.
    • (1994) Proceedings of the AIAA Guidance, Navigation, and Control Conference , pp. 544-550
    • McFarland, M.B.1    D'Souza, C.N.2
  • 3
    • 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
    • 0003980507 scopus 로고
    • Springer-Verlag, New York
    • Hahn, W., Stability of Motion. Springer-Verlag, New York. 1967, pp. 102-115, 271-278.
    • (1967) Stability of Motion , pp. 102-115
    • Hahn, W.1
  • 7
    • 0004178386 scopus 로고
    • Macmillan, New York
    • Khalil, H. K., Nonlinear Systems. Macmillan, New York, 1992, pp. 97-122, 136-151
    • (1992) Nonlinear Systems , pp. 97-122
    • Khalil, H.K.1
  • 8
    • 4243154350 scopus 로고    scopus 로고
    • Derivation of the Full Nonlinear Equations of Motion for a Rigid Airframe
    • to be published
    • DeSouza, C., and Schumacher, D., "Derivation of the Full Nonlinear Equations of Motion for a Rigid Airframe," Journal of Guidance, Control, and Dynamics (to be published).
    • Journal of Guidance, Control, and Dynamics
    • DeSouza, C.1    Schumacher, D.2
  • 11
    • 0030241128 scopus 로고    scopus 로고
    • Gain-Scheduled Bank-to-Turn Autopilot Design Using Linear Parameter Varying Transformations
    • Carter, L. H., and Shamma, J. S., "Gain-Scheduled Bank-to-Turn Autopilot Design Using Linear Parameter Varying Transformations," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 5, 1996, pp. 1056-1063.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.5 , pp. 1056-1063
    • Carter, L.H.1    Shamma, J.S.2
  • 12
    • 11744255943 scopus 로고    scopus 로고
    • Ph.D. Thesis, Dept. of Aerospace Engineering, Univ. of Michigan, Ann Arbor, MI
    • ∞ Control and Dynamic Inversion," Ph.D. Thesis, Dept. of Aerospace Engineering, Univ. of Michigan, Ann Arbor, MI, 1997.
    • (1997) ∞ Control and Dynamic Inversion
    • Schumacher, C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.