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http://dx.doi.org/10.7471/ikeee.2015.19.3.415

A Study on Applying The DO-178C to The Control SW Development of The Military Aircraft Intercom Based on CMMI  

Yoon, In-Bok (SW(C4I) Group, Yongin R&D Center, HanWhaThales)
Publication Information
Journal of IKEEE / v.19, no.3, 2015 , pp. 415-423 More about this Journal
Abstract
The DO-178C guide, which is referenced as the software development guide when a certification of the airworthiness in the commercial airplane is acquired by FAA in US, is recently referenced for the local military aircraft airworthiness. This indicates that when the auditor of the military aircraft airworthiness looks over the software development documents, the auditor reviews if all of the documents are verified in accordance with the DO-178C guide. However, when we developed the military aircraft intercom, We developed its control software in accordance with the CMMI level 3, since there were no requirements for the compliance of the DO-178C guide. Therefore, When we consider the airworthiness of this intercomm system, The analysis for how much the software development based on the CMMI level 3 is different from the DO-178C guide is needed to prepare the essential software documents additionally. Thus, This study analyzes the differences between CMMI level 3 and DO-178C guide and provides that which data on the CMMI level 3 is necessary for the compliance of the aircraft airworthiness comparing with the DO-178C. The analyzed result can be applied at the software development of the other military aircraft avionics equipment based on the CMMI model environment considering the compliance of the military aircraft airworthiness.
Keywords
CMMI; DO-178C; Military Aircraft; Intercom; Airworthiness; Control; Software;
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