Application of a direct adaptive control method for non-ASPR aeroengine

Huacong Li, Jiangfeng Fu, Xiang Gao, Shu Hong Wang

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

Aimed at the non-ASPR model of aeroengine, a new kind of direct adaptive controller of turbofan engine control system is put forward. The structure of a Command Generator Tracker (CGT)-based direct adaptive controller is simple, and no filter is needed. However, the controlled plants are required to be almost strictly positive real(ASPR), which limits its applications. For this, a Parallel Feedback Compensator (PFC)is designed to transfer non-ASPR model to ASPR model, and makes the non-ASPR model to meet the requirement of CGT-based direct adaptive control. The method has no need to identify and the parameters of th plant, so the structure of the system is simple. It also has a strong adaptive ability to variations of the parameters. Finally, the proposed approach is applied to the design of a non-ASPR model turbofan engine control system, and simulations are performed to show that the method is correct and feasible.

Original languageEnglish
Title of host publicationProceedings of the 32nd Chinese Control Conference, CCC 2013
PublisherIEEE Computer Society
Pages3059-3063
Number of pages5
ISBN (Print)9789881563835
StatePublished - 18 Oct 2013
Event32nd Chinese Control Conference, CCC 2013 - Xi'an, China
Duration: 26 Jul 201328 Jul 2013

Publication series

NameChinese Control Conference, CCC
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference32nd Chinese Control Conference, CCC 2013
Country/TerritoryChina
CityXi'an
Period26/07/1328/07/13

Keywords

  • aeroengine control
  • CGT
  • non-ASPR model
  • PFC

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