• 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