H control of gas turbine engines for helicopters

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

*この研究の対応する著者

研究成果: Conference contribution

2 被引用数 (Scopus)

抄録

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.

本文言語English
ホスト出版物のタイトルAmerican Control Conference
出版社Publ by IEEE
ページ1123-1127
ページ数5
ISBN(印刷版)0780308611, 9780780308619
DOI
出版ステータスPublished - 1993
外部発表はい
イベントProceedings of the 1993 American Control Conference Part 3 (of 3) - San Francisco, CA, USA
継続期間: 1993 6 21993 6 4

出版物シリーズ

名前American Control Conference

Other

OtherProceedings of the 1993 American Control Conference Part 3 (of 3)
CitySan Francisco, CA, USA
Period93/6/293/6/4

ASJC Scopus subject areas

  • 電子工学および電気工学

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