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Performance evaluation of fault-tolerant systems with application to the IUSA new method for quantitatively evaluating the performance of fault-tolerant systems is developed and applied to an example. The method assumes that the random failure and diagnostic decision behavior of the system can be modeled by a finite state Markov process. A performance value must be assigned to each of the states of the model. The method then generates the moments of the probability mass function of the cumulative performance and uses these to generate a maximum entropy approximation to the performance PMF. Some computational considerations are discussed. The method is applied to a typical mission for the Inertial Upper Stage to examine the attitude accuracy performance of the inertial system.
Document ID
19880062987
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Missana, J.-O.
(Forces Armees Francaises Paris, France)
Walker, Bruce K.
(Cincinnati, University OH, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 88-4110
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 15, 1988
End Date: August 17, 1988
Sponsors: AIAA Guidance
Accession Number
88A50214
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-84-0160
CONTRACT_GRANT: NAG1-126
Distribution Limits
Public
Copyright
Other

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