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Volumn , Issue , 1997, Pages 1155-1165

Fuzzy logic based forebody vortex flow control

Author keywords

[No Author keywords available]

Indexed keywords

BANG BANG CONTROL SYSTEMS; COMPUTER CIRCUITS; DESIGN; FEEDBACK; FLOW CONTROL; FUZZY INFERENCE; FUZZY LOGIC; FUZZY RULES; MEMBERSHIP FUNCTIONS; RECONFIGURABLE HARDWARE; RUDDERS; STATE FEEDBACK; VORTEX FLOW;

EID: 84959076242     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (23)
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    • Valasek, J.1
  • 4
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    • A Unified Controller Design Methodology for Systems with Continuous and Bang-Bang Control Effectors
    • Seattle, WA, 21-23 June
    • Valasek, John, and Downing, D.R., “A Unified Controller Design Methodology for Systems with Continuous and Bang-Bang Control Effectors,” ACC95-AIAA-060, Proceedings of the 1995 American Control Conference, Seattle, WA, 21-23 June 1995.
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    • Valasek, J.1    Downing, D.R.2
  • 5
    • 0030375093 scopus 로고    scopus 로고
    • A Robust Variable Structure Controller For Mixed Continuous/Bang- Bang Systems
    • Dearborn, MI, 15-18 September
    • Valasek, John, “A Robust Variable Structure Controller For Mixed Continuous/Bang- Bang Systems,” WA05 10:50, Proc. IEEE International Conference on Control Applications, Dearborn, MI, 15-18 September 1996.
    • (1996) WA05 10:50, Proc. IEEE International Conference on Control Applications
    • Valasek, J.1
  • 7
    • 0026866952 scopus 로고
    • Fighter Agility Metrics, Research and Test
    • May-June
    • Liefer, Randall K., Valasek, John, Eggold, David P., and Downing, David R., “Fighter Agility Metrics, Research and Test,” AIAA Journal of Aircraft, Vol. 29, No. 3, May-June 1992, pp. 452-457.
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  • 8
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    • (1988) Applied Airfoil and Wing Theory
    • Lan, C.E.1
  • 9
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    • Nov.-Dec
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    • (1993) AIAA Journal of Aircraft , vol.30 , Issue.6 , pp. 803-804
    • Eggold, D.P.1    Valasek, J.2    Downing, D.R.3
  • 10
    • 84959133152 scopus 로고
    • Aerodynamic Control of Fighter Aircraft by Manipulation of Forebody Vortices
    • Nov
    • Malcolm, Gerald N., and Ng, T. Terry, “Aerodynamic Control of Fighter Aircraft by Manipulation of Forebody Vortices,” AGARDCP- 497, Maneuvering Aerodynamics, Nov. 1991, pp. 15-1 to 15-22.
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  • 14
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.