Bounds are established on the probability of system failure for fault-tolerant systems of the type used, for example, in aviation control. Event series leading to system failure are assumed to follow a semi-Markov model in which the potential sojourn times associated with component failures have exponential distributions and those associated with system responses have distributions with unspecified form. A product form of the bounds is derived by using a model that provides for multiple competing system responses to component failures
The CARE 3 reliability model for aircraft avionics and control systems is described by utilizing a n...
AbstractSystem reliability is an important aspect of real-time systems, because the result of a real...
This paper discusses the modeling and analysis of three major fault-tolerant software system archite...
Bounds are established for the probability of failure of fault-tolerant systems. The underlying fail...
This paper determines the information required about system recovery to compute the reliability of a...
The current tendency of flight control system designs is towards increased integration of applicatio...
Upper and lower bounds are derived for the probability of failure for a class of highly reliable pro...
A methodology for performing fault tolerant system reliability analysis is presented. The method dec...
A way of considering a small but often used class of reliability model and approximating algebraical...
Reliability modeling for fault tolerant avionic computing systems was developed. The modeling of lar...
Two methodologies for the reliability assessment of fault tolerant digital computer based systems ar...
The rule-based Computer-Aided Markov Evaluator (CAME) program was expanded in its ability to incorpo...
The randomization technique for computing transient probabilities of Markov processes is presented. ...
The analysis and evaluation of reliability measures using time-varying Markov models is required for...
CARE III (Computer-Aided Reliability Estimation, version three) a computer program designed to help ...
The CARE 3 reliability model for aircraft avionics and control systems is described by utilizing a n...
AbstractSystem reliability is an important aspect of real-time systems, because the result of a real...
This paper discusses the modeling and analysis of three major fault-tolerant software system archite...
Bounds are established for the probability of failure of fault-tolerant systems. The underlying fail...
This paper determines the information required about system recovery to compute the reliability of a...
The current tendency of flight control system designs is towards increased integration of applicatio...
Upper and lower bounds are derived for the probability of failure for a class of highly reliable pro...
A methodology for performing fault tolerant system reliability analysis is presented. The method dec...
A way of considering a small but often used class of reliability model and approximating algebraical...
Reliability modeling for fault tolerant avionic computing systems was developed. The modeling of lar...
Two methodologies for the reliability assessment of fault tolerant digital computer based systems ar...
The rule-based Computer-Aided Markov Evaluator (CAME) program was expanded in its ability to incorpo...
The randomization technique for computing transient probabilities of Markov processes is presented. ...
The analysis and evaluation of reliability measures using time-varying Markov models is required for...
CARE III (Computer-Aided Reliability Estimation, version three) a computer program designed to help ...
The CARE 3 reliability model for aircraft avionics and control systems is described by utilizing a n...
AbstractSystem reliability is an important aspect of real-time systems, because the result of a real...
This paper discusses the modeling and analysis of three major fault-tolerant software system archite...