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Volumn 23, Issue 5, 2000, Pages 837-843

Adaptive autopilot design for guided munitions

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; AMMUNITION; APPROXIMATION THEORY; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; DEGREES OF FREEDOM (MECHANICS); ERROR ANALYSIS; FLIGHT DYNAMICS; INVERSE PROBLEMS; NEURAL NETWORKS;

EID: 0034276432     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4612     Document Type: Article
Times cited : (93)

References (10)
  • 2
    • 0029754366 scopus 로고    scopus 로고
    • A different look at output tracking: Control of a VTOL aircraft
    • Martin, P., Devasia, S., and Paden, B., "A Different Look at Output Tracking: Control of a VTOL Aircraft," Automatica, Vol. 32, No. 1, 1996, pp. 101-107.
    • (1996) Automatica , vol.32 , Issue.1 , pp. 101-107
    • Martin, P.1    Devasia, S.2    Paden, B.3
  • 5
    • 0030732624 scopus 로고    scopus 로고
    • Nonlinear flight control using neural networks
    • Kim, B. S., and Calise, A. J., "Nonlinear Flight Control Using Neural Networks," Journal of Guidance,Control, and Dynamics, Vol. 20, No. 1, 1997, pp. 26-33.
    • (1997) Journal of Guidance,Control, and Dynamics , vol.20 , Issue.1 , pp. 26-33
    • Kim, B.S.1    Calise, A.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.