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Research of Model-based Aeroengine Control System Design Structure and Workflow
Shenyang Engine Design and Research Institute, China.
KTH, School of Industrial Engineering and Management (ITM), Machine Design (Dept.), Mechatronics. Shenyang Engine Design and Research Institute, China.
2015 (English)In: Procedia Engineering, ISSN 1877-7058, E-ISSN 1877-7058, Vol. 99, 788-794 p.Article in journal (Refereed) Published
Abstract [en]

The control system of aeroengine design is a complex system engineeringincludingmany procedure of different subsystems. To improve the efficiency of areoengine control system design and reduce the cost and development period of research procedure, model-based areoengine control system design method can be used for integrating systems, collaborative design and optimizing design. Model-based aeroengine control system design workflow consists of the phases from analysis of system requirements to semi-physics simulation verification. The managementapproach and designprocedure can help to separate the whole design workflow into different sub-phases which can help to scheme the concurrent design procedure of complex control system in order to improve the efficiency of aeroenginedesign and optimize the performance of aeroengine control system.

Place, publisher, year, edition, pages
Elsevier, 2015. Vol. 99, 788-794 p.
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:kth:diva-181081DOI: 10.1016/j.proeng.2014.12.603ISI: 000384483200099Scopus ID: 2-s2.0-84978127867OAI: oai:DiVA.org:kth-181081DiVA: diva2:898467
Conference
2014 Asia-Pacific International Symposium on Aerospace Technology, APISAT2014 September 24-26, 2014 Shanghai, China
Note

QC 2016-02-12

Available from: 2016-01-28 Created: 2016-01-28 Last updated: 2017-11-14Bibliographically approved

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