Airworthiness Certification Requirements Analysis for Reusable Software Components of Integrated Modular Avionics

ZHAO Chang-xiao; YAN Fang; ZHANG Fan; WANG Peng

doi:10.3969/j.issn.1671-637x.2016.09.013

Journals >Electronics Optics & Control >Volume 23 >Issue 9 >Page 63 > Article

Electronics Optics & Control
Vol. 23, Issue 9, 63 (2016)

Airworthiness Certification Requirements Analysis for Reusable Software Components of Integrated Modular Avionics

ZHAO Chang-xiao¹, YAN Fang², ZHANG Fan³, and WANG Peng¹

Author Affiliations

¹[in Chinese]

²[in Chinese]

³[in Chinese]

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DOI: 10.3969/j.issn.1671-637x.2016.09.013 Cite this Article

ZHAO Chang-xiao, YAN Fang, ZHANG Fan, WANG Peng. Airworthiness Certification Requirements Analysis for Reusable Software Components of Integrated Modular Avionics[J]. Electronics Optics & Control, 2016, 23(9): 63 Copy Citation Text

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References

[3] RTCA. DO-297 Integrated Modular Avionics(IMA) development guidance and certification considerations［S］. Washington: RTCA, 2005.

[4] RTCA. DO-178B Software considerations in airborne systems and equipment certification［S］. Washington: RTCA, 1992.

[5] Certification Authorities Software Team. Certification Authorities Software Team (CAST) position paper 22: reuse of software tool qualification data across company boundaries (applying the reusable software component concept to tools)［R］. USA: FAA, 2005.

[6] WEIDE B W, OGDEN W F, ZWEBEN S H. Reusable software components［J］. Advances in Computers, 1991, 33(1): 1-65.

[7] GULAN S, HARNISCH J, JOHR S, et al. Model-based analysis for safety critical software［C］//Computer Safety, Reliability, and Security, 2015: 111-120.

[8] AC 20-148, reusable software components［R］. USA: FAA, 2004.