Title : 
Simulating faults in integrated systems and their impact on the aircraft
         
        
            Author : 
Kansal, Aparna ; Pritchett, Amy
         
        
            Author_Institution : 
Georgia Institute of Technology, Atlanta, GA
         
        
        
        
        
        
            Abstract : 
Outcomes from Case Study • Component failures can be simulated by violating component axioms to identify their impact on the integrated system and the aircraft. • Such simulations can identify requirements for other components • The timing of components executing a task is an important criteria to consider WMC Simulation Environment • Ability to allow a range of component models • Allows each component to specify its own update time • Using shared format for storing data as resources allows for simple models to be generated quickly • Incorporating simple representations of component models is sufficient to obtain an initial understanding of the effects of violating axioms • Its streamlined form allows for a large number of runs examining a number of test cases in lesser time • As the design and test program progresses, potential also exists to include progressively detailed — and ultimately complete — models of the components
         
        
        
        
            Conference_Titel : 
Digital Avionics Systems Conference (DASC), 2014 IEEE/AIAA 33rd
         
        
            Conference_Location : 
Colorado Springs, CO, USA
         
        
            Print_ISBN : 
978-1-4799-5002-7
         
        
        
            DOI : 
10.1109/DASC.2014.6979578