An intelligent parameter space approach applicable to engineering design of missile autopilot

Jing Mei Lou, Ke Zhang

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

2 Scopus citations

Abstract

Intelligent control is one of the development directions of control theory. The parameter space approach is used to solve robust stability problem of the system with uncertain parameters. This paper presents an intelligent parameter space approach that applied to design the missile autopilot. The method combines parameter space approach with intelligent PID. In order to research and prove the approach by computer simulation, multi-mode models are set channel control augmentation loop of missile. The conclusion is that this approach can improve control quality.

Original languageEnglish
Title of host publicationProceedings - 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009
DOIs
StatePublished - 2009
Event2009 International Conference on Information Engineering and Computer Science, ICIECS 2009 - Wuhan, China
Duration: 19 Dec 200920 Dec 2009

Publication series

NameProceedings - 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009

Conference

Conference2009 International Conference on Information Engineering and Computer Science, ICIECS 2009
Country/TerritoryChina
CityWuhan
Period19/12/0920/12/09

Keywords

  • Intelligent PID
  • Missile autopilot
  • Parameter space approach

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