Distributed control of turbofan engines

Mehrdad Pakmehr; Marion Mounier; Nathan Fitzgerald; George Kiwada; James D. Paduano; Eric Feron; Alireza Behbahani

doi:10.2514/6.2009-5532

Distributed control of turbofan engines

Mehrdad Pakmehr, Marion Mounier, Nathan Fitzgerald, George Kiwada, James D. Paduano, Eric Feron, Alireza Behbahani

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

16 Scopus citations

Abstract

The purpose of this paper is to develop control theoretic concepts for distributed control of gas turbine engines, and develop a dynamic engine model incorporating distributed components in compressor dynamics, engine cycles, and engine control. The latest results in distributed control combined with adaptive control theory are extended for turbofan engine distributed control. Concepts and architectures for distributed control are developed that create tangible benefits from the distribution of closed-loop feedback around the engine. © 2009 by the American Institute of Aeronautics and Astronautics, Inc.

Original language	English (US)
Title of host publication	45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Publisher	American Institute of Aeronautics and Astronautics Inc.
ISBN (Print)	9781563479762
DOIs	https://doi.org/10.2514/6.2009-5532
State	Published - Jan 1 2009
Externally published	Yes

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10.2514/6.2009-5532

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title = "Distributed control of turbofan engines",

abstract = "The purpose of this paper is to develop control theoretic concepts for distributed control of gas turbine engines, and develop a dynamic engine model incorporating distributed components in compressor dynamics, engine cycles, and engine control. The latest results in distributed control combined with adaptive control theory are extended for turbofan engine distributed control. Concepts and architectures for distributed control are developed that create tangible benefits from the distribution of closed-loop feedback around the engine. {\textcopyright} 2009 by the American Institute of Aeronautics and Astronautics, Inc.",

author = "Mehrdad Pakmehr and Marion Mounier and Nathan Fitzgerald and George Kiwada and Paduano, {James D.} and Eric Feron and Alireza Behbahani",

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year = "2009",

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doi = "10.2514/6.2009-5532",

language = "English (US)",

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TY - GEN

T1 - Distributed control of turbofan engines

AU - Pakmehr, Mehrdad

AU - Mounier, Marion

AU - Fitzgerald, Nathan

AU - Kiwada, George

AU - Paduano, James D.

AU - Feron, Eric

AU - Behbahani, Alireza

N1 - Generated from Scopus record by KAUST IRTS on 2021-02-18

PY - 2009/1/1

Y1 - 2009/1/1

N2 - The purpose of this paper is to develop control theoretic concepts for distributed control of gas turbine engines, and develop a dynamic engine model incorporating distributed components in compressor dynamics, engine cycles, and engine control. The latest results in distributed control combined with adaptive control theory are extended for turbofan engine distributed control. Concepts and architectures for distributed control are developed that create tangible benefits from the distribution of closed-loop feedback around the engine. © 2009 by the American Institute of Aeronautics and Astronautics, Inc.

AB - The purpose of this paper is to develop control theoretic concepts for distributed control of gas turbine engines, and develop a dynamic engine model incorporating distributed components in compressor dynamics, engine cycles, and engine control. The latest results in distributed control combined with adaptive control theory are extended for turbofan engine distributed control. Concepts and architectures for distributed control are developed that create tangible benefits from the distribution of closed-loop feedback around the engine. © 2009 by the American Institute of Aeronautics and Astronautics, Inc.

UR - http://arc.aiaa.org/doi/abs/10.2514/6.2009-5532

UR - http://www.scopus.com/inward/record.url?scp=77957850117&partnerID=8YFLogxK

U2 - 10.2514/6.2009-5532

DO - 10.2514/6.2009-5532

M3 - Conference contribution

SN - 9781563479762

BT - 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

PB - American Institute of Aeronautics and Astronautics Inc.

ER -

Distributed control of turbofan engines

Abstract

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