• DocumentCode
    2549272
  • Title

    Test Execution Control Tool: automating testing in spacecraft integration and test environments

  • Author

    Levesque, Michael ; Louis, Julien ; Guerrero, Ana Maria

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    2
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    389
  • Abstract
    In the era of faster, better, cheaper, JPL aims to develop and integrate an ever increasing number of spacecraft. One of the problems JPL faces is to quickly, efficiently and accurately test these spacecraft in a diverse set of environments from the breadboard, to environmental simulation and through launch preparation. The Test Execution Control Tool was developed using a Tool Command Language (Tcl) based test script interpreter to aid engineers in automating test procedures. Using the TECT, a tester can make the diverse collections of ground software, ground support equipment and flight systems work together through automated scripts. By allowing the tester to access and coordinate all the components of the complex testing environment, you not only achieve broader test coverage, leading to higher product assurance, but you achieve more speed and efficiency, leading to lower costs and faster results
  • Keywords
    aerospace testing; automatic testing; environmental testing; ground support systems; JPL; TECT; Tool Command Language; automatic testing; efficiency; environmental simulation; flight systems; ground software; ground support equipment; launch preparation; product assurance; spacecraft test environments; test execution control tool; test script interpreter; Automatic control; Automatic testing; Command languages; Costs; Instruments; Life testing; Propulsion; Space missions; Space vehicles; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.878246
  • Filename
    878246