Title :
A decentralized control scheme for a high performance turbine
Author :
Perez, Ronald A.
Author_Institution :
Dept. of Mech. Eng., Wisconsin Univ., Milwaukee, WI, USA
Abstract :
The problem of improving the performance and stability of a gas turbine engine operating throughout the whole flight envelope in the presence of predominantly destructive dynamical interactions is addressed in this paper. The controller structure aimed for in this work is decentralized, thus making the system tolerant to soft and/or hard failures while at the same time allowing the tuning of every loop separately
Keywords :
aerospace engines; aerospace propulsion; aircraft; decentralised control; gas turbines; stability; aircraft engine; decentralized control scheme; destructive dynamical interactions; failure tolerance; gas turbine engine; high performance turbine; loop tuning; stability; Aircraft propulsion; Clocks; Control systems; Distributed control; Jet engines; Mechanical engineering; Military aircraft; Packaging; Stability; Turbines;
Conference_Titel :
Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
Conference_Location :
San Antonio, TX
Print_ISBN :
0-7803-1298-8
DOI :
10.1109/CDC.1993.325110
