DocumentCode
2698158
Title
Numerical analysis on the reliability of space tracking, telemetering and command system based on the sparse matrix storage schemes
Author
Li, Lirong ; Yan, Hua ; Wu, Xiaoyue
Author_Institution
Automobile Manage. Inst., Bengbu, China
fYear
2012
fDate
15-18 June 2012
Firstpage
240
Lastpage
244
Abstract
Space tracking, telemetry and command (TT&C) system is essentially a dynamic structure system with multiple mission phases. When there are a large number of equipments in a system, the transition matrix of the Markov model of the system is a large sparse matrix whose solution is hard to gain directly. This paper suggests a Runge Kutta method based on the sparse matrix storage scheme to numerically solve and analyze the reliability model. Examples with numerical results show the effectiveness of the solution method. The efficiency of the proposed method is also proved through an analysis on its storage space and solving time.
Keywords
Markov processes; Runge-Kutta methods; aircraft control; attitude control; numerical analysis; reliability; telemetry; Markov model; Runge Kutta method; command system; dynamic structure system; multiple mission phase; numerical analysis; reliability; space tracking; sparse matrix storage; telemetering; transition matrix; Algorithm design and analysis; Analytical models; Arrays; Markov processes; Reliability; Space missions; Sparse matrices; Runge Kutta method; reliability; space TT&C system; sparse matrix storage;
fLanguage
English
Publisher
ieee
Conference_Titel
Quality, Reliability, Risk, Maintenance, and Safety Engineering (ICQR2MSE), 2012 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4673-0786-4
Type
conf
DOI
10.1109/ICQR2MSE.2012.6246228
Filename
6246228
Link To Document