Application of Integrated Electrical Mechanical Control System Technology for Civil Transportation Aircraft Design and Development

Lei Zhang; Nan Shan; Miao Huan Zhang

doi:10.4028/www.scientific.net/AMM.299.83

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 299Application of Integrated Electrical Mechanical...

Application of Integrated Electrical Mechanical Control System Technology for Civil Transportation Aircraft Design and Development

Abstract:

Integrated electrical mechanical control system (IEMS) technology applied on civil transportation aircraft is firstly introduced in the article. Besides, from the standpoint of airframer, detailed analysis of design and development risks is conducted and relevant mitigation suggestions are proposed accordingly. Finally, the importance and strategy for the construction of a simulation and test all-in-one bench by airframer are also discussed.

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Periodical:

Applied Mechanics and Materials (Volume 299)

Pages:

83-88

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.299.83

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Online since:

February 2013

Authors:

Lei Zhang, Nan Shan, Miao Huan Zhang

Keywords:

Civil Transportation Aircraft, Integrated Electrical Mechanical Control System, Integrated Modular Avionics (IMA), Simulation All-in-One Bench, Test All-in-One Bench

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References

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