The reliability design and optimization of flight control system based on DEMO

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

1 Scopus citations

Abstract

Considering the traditional problems in reliability design, such as the large computational complexity and the difficulty to solve the reliability-cost model, the Multi-Objective Optimization Algorithm is applied in order to solve the traditional problems in the reliability-cost optimization. In this paper, a model based on the Differential Evolution for Multi-Objective Optimization (DEMO) is built to realize the reliability design of system redundancy. Under the restriction of the cost, volume and weight, the model can achieve an optimum design of the flight control system reliability. In the end, the reliability optimization model is verified by the examples and it is shown that the design results given by the system reliability optimized model are valuable for the design of the flight control system.

Original languageEnglish
Title of host publicationProceedings of the 32nd Chinese Control Conference, CCC 2013
PublisherIEEE Computer Society
Pages8028-8031
Number of pages4
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

  • MEDO
  • Multi-objective optimization
  • reliability
  • system redundancy

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