Application of linear multivariable control design for the GE-21 turbofan jet engine

Novel designs are proposed for use in the multivariable control of the GE-21 engine. The designs utilize linear multivariable control theory to generate a new linear quadratic regulator (LQR) followed by loop transfer recovery (LTR) to obtain a robust linear quadratic Gaussian (LQG) controller. The...

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Published in[1989] Proceedings. The Twenty-First Southeastern Symposium on System Theory pp. 167 - 171
Main Authors Dellinger, W.F., Alouani, A.T.
Format Conference Proceeding
LanguageEnglish
Published IEEE Comput. Soc. Press 1989
Subjects
Actuators
Control design
Control theory
Incineration
Jet engines
Process design
Robust control
Steady-state
Temperature
Turbines
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Abstract Novel designs are proposed for use in the multivariable control of the GE-21 engine. The designs utilize linear multivariable control theory to generate a new linear quadratic regulator (LQR) followed by loop transfer recovery (LTR) to obtain a robust linear quadratic Gaussian (LQG) controller. The engine control problem and the design process are described. The design techniques involve the analysis of the singular values of the return ratio at both the plant input and output. LQR/LTR compensators are designed to meet the required robustness and performance specifications. Step response analysis utilizing these designs is presented.< >
AbstractList Novel designs are proposed for use in the multivariable control of the GE-21 engine. The designs utilize linear multivariable control theory to generate a new linear quadratic regulator (LQR) followed by loop transfer recovery (LTR) to obtain a robust linear quadratic Gaussian (LQG) controller. The engine control problem and the design process are described. The design techniques involve the analysis of the singular values of the return ratio at both the plant input and output. LQR/LTR compensators are designed to meet the required robustness and performance specifications. Step response analysis utilizing these designs is presented.< >
Author Dellinger, W.F.
Alouani, A.T.
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  organization: Dept. of Electr. Eng., Tennessee Technol. Univ., Cookeville, TN, USA
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Snippet Novel designs are proposed for use in the multivariable control of the GE-21 engine. The designs utilize linear multivariable control theory to generate a new...
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StartPage 167
SubjectTerms Actuators
Control design
Control theory
Incineration
Jet engines
Process design
Robust control
Steady-state
Temperature
Turbines
Title Application of linear multivariable control design for the GE-21 turbofan jet engine
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