DocumentCode :
2112629
Title :
An IVHM systems analysis & optimization process
Author :
Datta, Koushik ; Jize, Nicholas ; Maclise, Dougal ; Goggin, David
Author_Institution :
NASA Ames Res. Center, Moffett Field, CA, USA
Volume :
6
fYear :
2004
fDate :
6-13 March 2004
Firstpage :
3706
Abstract :
The paper describes a systems analysis and optimization (SA&O) process that has been developed at NASA to quantify the effects of IVHM on Reusable Launch Vehicle (RLV) designs and to target areas for potential IVHM technology development. The process incorporates cost, operations, safety, reliability, false alarm rate, performance, and testability models in a modular fashion that allows individual models to be easily swapped out and another model inserted in its place. This IVHM SA&O process has been used to examine a representative MPS feed subsystem on a generic two-stage to orbit RLV. The results from the optimization analysis show that by examining relevant system figures of merit, the method developed allows for better, targeted utilization of IVHM that optimizes the benefit to system wide figures of merit rather than a local optimization based on engineering judgment. Although the paper examines an optimum application of IVHM to an RLV, the SA&O process presented can be generalized by system engineers/architects for optimizing the application of virtually any technology to a system design.
Keywords :
aerospace propulsion; condition monitoring; design for testability; fault diagnosis; optimisation; reliability; space vehicles; NASA; Reusable Launch Vehicle designs; design for testability; false alarm rate; feed subsystem; integrated vehicle health monitoring system; main propulsion system; optimization process; reliability; safety; systems analysis; Costs; Design optimization; Feeds; NASA; Optimization methods; Paper technology; Safety; Space technology; Testing; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN :
1095-323X
Print_ISBN :
0-7803-8155-6
Type :
conf
DOI :
10.1109/AERO.2004.1368186
Filename :
1368186
Link To Document :
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