System Reliability Estimation of Divert Attitude Control System of a Launch Vehicle using Bayesian Networks

Divert attitude and control system (DACS) is a one-shot system and provides attitude correction and translation of the Launch vehicle. DACS consists of many flight critical sub systems which are arranged in a series configuration. The traditional Reliability block diagram and Fault tree diagram meth...

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Bibliographic Details
Published in:	Defense science journal Vol. 70; no. 1; pp. 90 - 94
Main Authors:	Muthukumar, S., Srivardhan, R. A., Bose, P. Subhash Chandra
Format:	Journal Article
Language:	English
Published:	New Delhi Defence Scientific Information & Documentation Centre 01.01.2020
Subjects:	Algorithms Attitude control Bayesian analysis Block diagrams Component reliability Computer simulation Conditional probability Control systems Fault trees Launch vehicles Markov chains Network reliability Reliability analysis Reliability aspects Subsystems System reliability
ISSN:	0011-748X, 0976-464X
Online Access:	Get full text
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