Du Zhen-hua, Chen Jin-dun, Zhao Yu, Wang Li-dong
Reliability Engineering Institute, Beijing University of Aeronautics and Astronautics, Beijing, China.
Space Med Med Eng (Beijing). 2003 Aug;16(4):300-3.
To define the lower confidence limit of the system reliability of the space metabolism simulation device by using the test data of the comprising units in their development phases.
A new method for defining the environmental conversion factors of failure times has been given basing on the AMSAA model, and the MTBF point evaluated values and lower confidence limits of the units were defined, at last, the lower confidence limit of the system reliability was obtained using L-M method.
The lower confidence limit of the system reliability under confidence level of 0.8 is 0.9281, which is consistent with the result obtained by the classic system reliability evaluation method.
Integrated system reliability evaluation using the proposed method can well satisfy the need in engineering.