A New Test Bench Design Supporting Lifecycle Activities of Civil Aircraft Integrated Electrical Mechanical Control System

Lei Zhang; Tian Xiang Xiong; Rui Jie Fan

doi:10.4028/www.scientific.net/AMM.644-650.175

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650A New Test Bench Design Supporting Lifecycle...

A New Test Bench Design Supporting Lifecycle Activities of Civil Aircraft Integrated Electrical Mechanical Control System

Abstract:

A simulation and test based approach intended to support whole lifecycle activities of IEMS development is proposed. A new test bench design philosophy including its hardware and software as well as its support for each IEMS development phase are described in detail. Finally, further considerations on bench application for IEMS certification are also proposed.

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Periodical:

Applied Mechanics and Materials (Volumes 644-650)

Pages:

175-178

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.644-650.175

Citation:

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Online since:

September 2014

Authors:

Lei Zhang*, Tian Xiang Xiong, Rui Jie Fan

Keywords:

Certification, Civil Aircraft, Integrated Electrical Mechanical Control System, Integrated Modular Avionics, Life Cycle

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* - Corresponding Author

References

[1] J. Wang, Y.J. Liu, and S.J. Dong, Advanced technologies of the integrated aircraft utility system and ECS, Journal of Beijing University of aeronautics and astronautics. 29(11), pp.959-963, 2003. (in Chinese).

Google Scholar

[2] T. Liu, Z.L. Wang, and L.H. Qiu, Survey on the onboard utility management system, Measurement & Control Technology. 25(6) pp.1-6, 23, 2005. (in Chinese).

Google Scholar

[3] C.B. Watkins, R. Walter, and G. Rapids, Transitioning from federated avionics architectures to integrated modular avionics, 26th Digital Avionics Systems Conference (DASC 2007), IEEE: Dallas, Texas, p.2. A1-1-2.A. 1-10, (2007).

DOI: 10.1109/dasc.2007.4391842

Google Scholar

[4] C.B. Watkins, R. Walter, and G. Rapids, Design considerations for systems hosted on integrated modular avionics platforms, 27th Digital Avionics Systems Conference (DASC 2008), IEEE: St. Paul, Minnesota, p.1.A. 2-1-1.A. 2-7, (2008).

DOI: 10.1109/dasc.2008.4702747

Google Scholar

[5] L. Zhang, N. Shan, and M.H. Zhang, Application of integrated electrical mechanical control system technology for civil transportation aircraft design and development, Applied Mechanics and Materials. 299, pp.83-88, (2013).

DOI: 10.4028/www.scientific.net/amm.299.83

Google Scholar

[6] RTCA Special Committee 200, European Organization for Civil Aviation Equipment (EUROCAE) Working Group 60, Nov, 2005, DO-297: Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations, Washington, DC, RTCA, Inc, www. rtca. org/downloads/ListofAvailableDocs_WEB_MAR2007. htm#_Toc162689949.

DOI: 10.1201/9781315222233-14

Google Scholar