Turbofan engine control design using robust multivariable control technologies
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[1] M. Safonov,et al. SIMPLIFYING THE H" THEORY VIA LOOP SHIFTING* , 1988 .
[2] B. Anderson,et al. Model reduction for control system design , 1984 .
[3] Shrider Adibhatla,et al. Intelligent Engine Control (IEC) , 1992 .
[4] Sanjay Garg. Integrated Flight/Propulsion Control Design for a STOVL Aircraft using H-Infinity Control Design Techniques , 1991, 1991 American Control Conference.
[5] Sanjay Garg. A Simplified Scheme for Scheduling Multivariable Controllers and its Application to a Turbofan Engine , 1996 .
[6] Michel Kinnaert,et al. Conditioning technique, a general anti-windup and bumpless transfer method , 1987, Autom..
[7] Sanjay Garg,et al. An Optimized Integrator Windup Protection Technique Applied to a Turbofan Engine Control , 1996 .
[8] Shrider Adibhatla. Propulsion control law design for the NASA STOVL Controls Technology program , 1993 .
[9] J. M. Edmunds,et al. Control system design and analysis using closed-loop Nyquist and Bode arrays , 1979 .
[10] M. Safonov,et al. Simplifying the H∞ theory via loop-shifting, matrix-pencil and descriptor concepts , 1989 .
[11] Andrew C. W. Grace,et al. Control system toolbox for use with Matlab , 1995 .
[12] S. Adibhatla,et al. Multivariate Turbofan Engine Control for Full Flight Envelope Operation , 1989 .