Title : 
An error bound for instantaneous coverage
         
        
        
            Author_Institution : 
NASA Langley Res. Center, Hampton, VA, USA
         
        
        
        
        
        
            Abstract : 
An error bound is derived for a reliability model approximation method. The approximation method is appropriate for the semi-Markov models of reconfigurable systems that are designed to achieve extremely high reliability. The reliability model approximation method consists of replacing a detailed description of a reconfiguration process with the probabilities of the possible outcomes of the reconfiguration process. These probabilities are included in the model as instantaneous jumps from the fault-occurrence state. Since little time is spent in the reconfiguration states, instantaneous jumps are a close approximation to the original model. This approximation procedure is shown to produce an overestimation for the probability of system failure, and an error bound is derived for this overestimation
         
        
            Keywords : 
error analysis; failure analysis; reliability; approximation method; error bound; fault-occurrence state; reconfigurable systems; reliability model; semi-Markov models; Aerospace control; Aircraft; Approximation methods; Computer architecture; Digital control; Digital systems; Life testing; NASA; Redundancy; System recovery;
         
        
        
        
            Conference_Titel : 
Reliability and Maintainability Symposium, 1991. Proceedings., Annual
         
        
            Conference_Location : 
Orlando, FL
         
        
            Print_ISBN : 
0-87942-661-6
         
        
        
            DOI : 
10.1109/ARMS.1991.154503