H∞ control of gas turbine engines for helicopters

Ryo Watanabe; Masahiro Kurosaki; Takeshi Kusakawa; Kenko Uchida; Masayuki Fujita

doi:10.23919/acc.1993.4793041

H^∞ control of gas turbine engines for helicopters

Ryo Watanabe^*, Masahiro Kurosaki, Takeshi Kusakawa, Kenko Uchida, Masayuki Fujita

^*Corresponding author for this work

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

2 Citations (Scopus)

Abstract

Engine tests were conducted in order to demonstrate effectiveness and practicability of H^∞ control theory to helicopter engines. An engine control algorithm is designed by H^∞ control theory, which meets robust stability requirements and nominal performance requirements described in frequency domain. Simulation and engine test results show that H^∞ controllers with feedforward element have better control performance than PI controller with feedforward element, especially, less power turbine speed overshoots are observed in rapid torque decreasing tests.

Original language	English
Title of host publication	American Control Conference
Publisher	Publ by IEEE
Pages	1123-1127
Number of pages	5
ISBN (Print)	0780308611, 9780780308619
DOIs	https://doi.org/10.23919/acc.1993.4793041
Publication status	Published - 1993
Externally published	Yes
Event	Proceedings of the 1993 American Control Conference Part 3 (of 3) - San Francisco, CA, USA Duration: 1993 Jun 2 → 1993 Jun 4

Publication series

Name	American Control Conference

Other

Other	Proceedings of the 1993 American Control Conference Part 3 (of 3)
City	San Francisco, CA, USA
Period	93/6/2 → 93/6/4

ASJC Scopus subject areas

Electrical and Electronic Engineering

Access to Document

10.23919/acc.1993.4793041

Cite this

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title = "H∞ control of gas turbine engines for helicopters",

abstract = "Engine tests were conducted in order to demonstrate effectiveness and practicability of H∞ control theory to helicopter engines. An engine control algorithm is designed by H∞ control theory, which meets robust stability requirements and nominal performance requirements described in frequency domain. Simulation and engine test results show that H∞ controllers with feedforward element have better control performance than PI controller with feedforward element, especially, less power turbine speed overshoots are observed in rapid torque decreasing tests.",

author = "Ryo Watanabe and Masahiro Kurosaki and Takeshi Kusakawa and Kenko Uchida and Masayuki Fujita",

year = "1993",

doi = "10.23919/acc.1993.4793041",

language = "English",

isbn = "0780308611",

series = "American Control Conference",

publisher = "Publ by IEEE",

pages = "1123--1127",

booktitle = "American Control Conference",

note = "Proceedings of the 1993 American Control Conference Part 3 (of 3) ; Conference date: 02-06-1993 Through 04-06-1993",

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AU - Watanabe, Ryo

AU - Kurosaki, Masahiro

AU - Kusakawa, Takeshi

AU - Uchida, Kenko

AU - Fujita, Masayuki

PY - 1993

Y1 - 1993

N2 - Engine tests were conducted in order to demonstrate effectiveness and practicability of H∞ control theory to helicopter engines. An engine control algorithm is designed by H∞ control theory, which meets robust stability requirements and nominal performance requirements described in frequency domain. Simulation and engine test results show that H∞ controllers with feedforward element have better control performance than PI controller with feedforward element, especially, less power turbine speed overshoots are observed in rapid torque decreasing tests.

AB - Engine tests were conducted in order to demonstrate effectiveness and practicability of H∞ control theory to helicopter engines. An engine control algorithm is designed by H∞ control theory, which meets robust stability requirements and nominal performance requirements described in frequency domain. Simulation and engine test results show that H∞ controllers with feedforward element have better control performance than PI controller with feedforward element, especially, less power turbine speed overshoots are observed in rapid torque decreasing tests.

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EP - 1127

BT - American Control Conference

PB - Publ by IEEE

T2 - Proceedings of the 1993 American Control Conference Part 3 (of 3)

Y2 - 2 June 1993 through 4 June 1993

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