• DocumentCode
    1401397
  • Title

    Integrated systems for detecting and managing acceleration-induced loss of consciousness

  • Author

    Cammarota, J.P.

  • Author_Institution
    US Naval Air Dev. Center, Warminster, PA, USA
  • Volume
    10
  • Issue
    1
  • fYear
    1991
  • fDate
    3/1/1991 12:00:00 AM
  • Firstpage
    52
  • Lastpage
    55
  • Abstract
    The requirements for an acceleration-induced loss of consciousness (G-LOC) warning and recovery system (G-WARS) are discussed, and the approach being pursued is described. A combination of sensors will work together with an acceleration monitor to formulate an accurate assessment of pilot consciousness. Warnings will be issued to prevent G-LOC from occurring, possibly in the form of a slight pulsing of the pressure exerted by the anti-G suit. If the physiologic insult continues beyond the limits of the G-limit warning system, an auto-recovery sequence will be initiated. Timing constraints are addressed, and the testing of a G-WARS system is considered. The use of G-WARS in tactical aircraft is discussed.<>
  • Keywords
    aerospace biophysics; biomechanics; biomedical equipment; acceleration monitor; acceleration-induced loss of consciousness; anti-G suit; auto-recovery sequence; integrated systems; physiologic insult; pilot consciousness; sensors; tactical aircraft; warning; Acceleration; Accelerometers; Aerospace control; Aerospace electronics; Biomedical measurements; Biomedical monitoring; Displays; Military aircraft; Protection; Stress;
  • fLanguage
    English
  • Journal_Title
    Engineering in Medicine and Biology Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0739-5175
  • Type

    jour

  • DOI
    10.1109/51.70041
  • Filename
    70041