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International Journal of Systems Science Volume 26, 1995 - Issue 3
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Original Articles

A control design procedure for plants with random initial conditions and constraints on the mean square actuator rates

C. FRANGOS Laboratory for Decision and Control, Department of Electrical and Electronic Engineering, University of Pretoria, Pretoria, 0002, South AfricaView further author information
&
Y. YAVTN Laboratory for Decision and Control, Department of Electrical and Electronic Engineering, University of Pretoria, Pretoria, 0002, South Africa
Pages 515-524 | Received 16 Sep 1993, Published online: 16 May 2007

REFERENCES

  • BRYSON , A. E. , and Ho , Y.-C. , 1975 , Applied Optimal Control ( New York Hemisphere ).
  • ELLIOT , J. R. , 1977 , NASA's advanced control law program for the F-8 digital fly-by-wir aircraft . IEEE Transactions on Automatic Control , 22 , 753 – 757 .
  • FRANCOS , C. , 1987 , Robust multivariable control for an aircraft using a modern synthesis methodology . Ph.D. dissertation , Faculty of Engineering, University of Pretoria , Pretoria , South Africa .
  • GRACE , A. , 1990 , User's Guide of the PC-MATLAB Optimization Toolbox ( Natick , Mass : The MathWorks Inc ).
  • HARVEY , C. A. , and STEIN , G. , 1978 , Quadratic weights for asymptotic regulator properties . IEEE Transactions on Automatic Control , 23 , 378 – 387 .
  • HASHtMOTO , Y. , YONEYA , A. , and TOGARI , Y. , 1989 , Design method of a quadratic performance index using a reference model. International Journal of Control, 50 , 1169 – 1184 .
  • KREISSELMEJER , G. , and STEINHAUSER , R. , 1983 , Application of vector performance optimization to a robust control loop design for a fighter aircraft. International Journal of Control , 7 , 251 – 284 .
  • LEWIS , F. L. , 1992 , Applied Optimal Control and Estimation ( Englewood Cliffs , NJ Prentice-Hall ).
  • ROGERS , W. L. , and COLLINS , D. J. , 1992 , X-29 Hm controller synthesis . AIAA Journal of Guidance, Control and Dynamics, 15 , 962 – 967 .

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