Systems often operate over a set of time periods, known as phases, in which
their reliability structure varies and many include both repairable and nonrepairable
components. Success for such systems is defined as the
completion of all phases, known as a phased mission, without failure. An
example of such a system is an aircraft landing gear system during a flight.
The Binary Decision Diagram (BDD) method provides the most efficient
solution to the unreliability of non-repairable systems whilst for repairable
systems Markov or other state-space based methods have been most widely
applied. For systems containing both repairable and non-repairable
components the repairable modelling methods are normally used, despite
having far higher computational expense than the non-repairable methods,
since only they are able to handle the dependencies involved. This paper
introduces improvements to the BDD method for analysing non-repairable
systems as well as an entirely new method that utilises a new modelling
technique involving both BDD and Markov techniques.
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
Department
Aeronautical and Automotive Engineering
Citation
REED, S., DUNNETT, S.J. and ANDREWS, J.D., 2009. High performance reliability analysis of phased mission systems. IN: Bartlett, L. (ed.). Proceedings of the 18th Advances in Risk and Reliability Technology Symposium (AR2TS), Loughborough, 21-23 April, pp.228-255.
Publisher
Loughborough University Department of Aeronautical & Automotive Engineering & Transport Studies