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Volumn , Issue , 1999, Pages 1-9

Adaptive flight control using dynamic inversion and neural networks

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SURFACES; CONTROLLERS; DEGREES OF FREEDOM (MECHANICS); DYNAMICS; TRACKING (POSITION); TWO TERM CONTROL SYSTEMS;

EID: 84959090044     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (9)

References (9)
  • 1
    • 0030290057 scopus 로고    scopus 로고
    • Stability and flying qualities robustness of a dynamic inversion aircraft control law
    • Brinker, J. S. and K. A. Wise, Stability and flying qualities robustness of a dynamic inversion aircraft control law. Journal of Guidance, Control, and Dynamics, 1996. 19(6): p. 1270-11277.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.6 , pp. 1270-11277
    • Brinker, J.S.1    Wise, K.A.2
  • 8
    • 84959138889 scopus 로고    scopus 로고
    • Adaptive Nonlinear Control of Missilès using Neural Networks
    • 1997, Georgia Institute of Technology: Atlanta, GA
    • McFarland, M. B., Adaptive Nonlinear Control of Missilès using Neural Networks, in Aerospace Engineering. 1997, Georgia Institute of Technology: Atlanta, GA. p. 157.
    • Aerospace Engineering , pp. 157
    • McFarland, M.B.1
  • 9
    • 85031982285 scopus 로고    scopus 로고
    • PI Control of a Tailless Fighter Aircraft with Dynamic Inversion and Neural Networks, to appear in the, American Control Conference
    • Schumacher, C., and Johnson, J. D., PI Control of a Tailless Fighter Aircraft with Dynamic Inversion and Neural Networks, to appear in the 1999 American Control Conference.
    • (1999)
    • Schumacher, C.1    Johnson, J.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.