Archivio Istituzionale della RicercaThe design of a control maintenance system (CMs) deeply deals with the mission, the on–board systems interfaces and the identification of their behaviour in operation. This paper describes how the Model Based Systems Engineering (MBSE) was applied to an industrial test case to perform the functional design of an innovative CMs to be integrated with the aircraft fuel system (Fs). The impact of different approaches applied when modelling the two systems through the SysML on their integration was investigated. As the IBM Rational Rhapsody® tool was used, the Harmony® methodology was applied to the CMs, while a MBSE customized approach was implemented for the Fs, even to cope with some differences in coupling an avionic system to a physical one.
Integration of different MBSE approaches within the design of a control maintenance system applied to the aircraft fuel system / C., Pessa; M., Cifaldi; Brusa, Eugenio; Ferretto, Davide; K., Malgieri; Viola, Nicole. - ELETTRONICO. - 1:(2016), pp. 120-127. (Intervento presentato al convegno IEEE Int. Symposium on Systems Engineering tenutosi a Edinburgh nel October 4-5,2016).
Integration of different MBSE approaches within the design of a control maintenance system applied to the aircraft fuel system
BRUSA, Eugenio;FERRETTO, DAVIDE;VIOLA, Nicole
2016
Abstract
The design of a control maintenance system (CMs) deeply deals with the mission, the on–board systems interfaces and the identification of their behaviour in operation. This paper describes how the Model Based Systems Engineering (MBSE) was applied to an industrial test case to perform the functional design of an innovative CMs to be integrated with the aircraft fuel system (Fs). The impact of different approaches applied when modelling the two systems through the SysML on their integration was investigated. As the IBM Rational Rhapsody® tool was used, the Harmony® methodology was applied to the CMs, while a MBSE customized approach was implemented for the Fs, even to cope with some differences in coupling an avionic system to a physical one.
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[18] IEEE ISSE 2016 Fuel.pdf
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https://hdl.handle.net/11583/2662182
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