Title :
Control configuration design for the aircraft gas turbine engine
Abstract :
UK research into the design of multivariable controllers for gas turbines has been under way for several years. The results of simulation and engine test evaluations have been reported by Sutton (1991), and Shutler and Betteridge (1994). This article focuses on one aspect of multivariable controller design which is that of selecting outputs for closed-loop feedback control; this process is often referred to as control configuration design.<>
Keywords :
aerospace engines; aircraft control; closed loop systems; feedback; gas turbines; multivariable control systems; process control; aircraft gas turbine engine; closed-loop feedback control; control configuration design; engine test evaluations; gas turbines; multivariable controller design; simulation; Aircraft control; Closed loop systems; Feedback; Gas turbines; Multivariable systems; Process control;
Journal_Title :
Computing & Control Engineering Journal
DOI :
10.1049/cce:19950109
