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Volumn , Issue , 1996, Pages 1-8

Neural-adaptive nonlinear autopilot design for an agile anti-air missile

Author keywords

[No Author keywords available]

Indexed keywords

AGILE MANUFACTURING SYSTEMS; AIR NAVIGATION; CLOSED LOOP SYSTEMS; CONTROL THEORY; DESIGN; E-LEARNING; LEARNING SYSTEMS; MISSILES;

EID: 84959178592     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3914     Document Type: Conference Paper
Times cited : (13)

References (11)
  • 1
    • 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
  • 11
    • 0004243870 scopus 로고
    • John Wiley & Sons, Inc., New York
    • Etkin, B., Dynamics of Atmospheric Flight, John Wiley & Sons, Inc., New York, 1972, pp. 148-150.
    • (1972) Dynamics of Atmospheric Flight , pp. 148-150
    • Etkin, B.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.