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Volumn 28, Issue 1, 2007, Pages 187-190

Adaptive control allocation between aerodynamic fin and side thruster and controller design using multi-objective optimization

Author keywords

Adaptive control; Control allocation; Evolutionary strategies; Fuzzy logic

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; CONTROL SYSTEMS; DYNAMIC MODELS; FUZZY LOGIC; OPTIMIZATION; TRACKING (POSITION);

EID: 34249848059     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (19)

References (10)
  • 2
    • 33846595590 scopus 로고    scopus 로고
    • Augmentation of high-altitude maneuver performance of tail-controlled missile using lateral thrust
    • ADA-328973
    • Chadwick K A. Augmentation of high-altitude maneuver performance of tail-controlled missile using lateral thrust[R]. ADA-328973, 1997.
    • (1997)
    • Chadwick, K.A.1
  • 3
    • 33748205273 scopus 로고    scopus 로고
    • Autopilot design for agile missile with aerodynamic fin and side thruster
    • Japan, Fukui: IEEC Press
    • Yong S C, Choi C L, Jae W C. Autopilot design for agile missile with aerodynamic fin and side thruster[C]//SICE Annual Conference. Japan, Fukui: IEEC Press, 2003: 1476-1481.
    • (2003) SICE Annual Conference , pp. 1476-1481
    • Yong, S.C.1    Choi, C.L.2    Jae, W.C.3
  • 5
    • 33748159886 scopus 로고    scopus 로고
    • Side jet and aerodynamics compound control system design of air defense missiles
    • in Chinese
    • Cheng F Z, Wan Z M, Chen S L, et al. Side jet and aerodynamics compound control system design of air defense missiles[J]. Flight Dynamics, 2003, 21(2): 49-52. (in Chinese)
    • (2003) Flight Dynamics , vol.21 , Issue.2 , pp. 49-52
    • Cheng, F.Z.1    Wan, Z.M.2    Chen, S.L.3
  • 6
    • 3042677139 scopus 로고    scopus 로고
    • Adaptive techniques for multiple actuator blending
    • AIAA 98-4494
    • Menon P K, Iragavarapu V R. Adaptive techniques for multiple actuator blending[R]. AIAA 98-4494, 1998.
    • (1998)
    • Menon, P.K.1    Iragavarapu, V.R.2
  • 7
    • 0032071047 scopus 로고    scopus 로고
    • A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering
    • Thukral A, Innocenti M. A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering[J]. IEEE Transactions on Control Systems Technology, 1998, 6(3): 359-371.
    • (1998) IEEE Transactions on Control Systems Technology , vol.6 , Issue.3 , pp. 359-371
    • Thukral, A.1    Innocenti, M.2
  • 8
    • 0028710584 scopus 로고
    • An appropriate application of fuzzy logic: Missile autopilot for dual control implementation
    • Columbus: IEEE Press
    • Schroeder W K, Liu K. An appropriate application of fuzzy logic: missile autopilot for dual control implementation[C]//IEEE International Symposium on Intelligent Control. Columbus: IEEE Press, 1994: 93-98.
    • (1994) IEEE International Symposium on Intelligent Control , pp. 93-98
    • Schroeder, W.K.1    Liu, K.2
  • 9
    • 85087593877 scopus 로고    scopus 로고
    • Autopilot design for a missile with reaction jet using coefficient diagram
    • Canada, Montreal: AIAA Press
    • Hirokawa R, Sato K. Autopilot design for a missile with reaction jet using coefficient diagram[C]//AIAA Guidance, Navigation and Control Conference and Exhibit. Canada, Montreal: AIAA Press, 2001: 1-8.
    • (2001) AIAA Guidance, Navigation and Control Conference and Exhibit , pp. 1-8
    • Hirokawa, R.1    Sato, K.2
  • 10
    • 0034230327 scopus 로고    scopus 로고
    • A new mutation rule for evolutionary programming motivated from back propagation learning
    • Choi D H, Oh S Y. A new mutation rule for evolutionary programming motivated from back propagation learning[J]. IEEE Transaction on Evolutionary Computation, 2000, 4(2): 188-190.
    • (2000) IEEE Transaction on Evolutionary Computation , vol.4 , Issue.2 , pp. 188-190
    • Choi, D.H.1    Oh, S.Y.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.