• DocumentCode
    1228441
  • Title

    Acceleration Stress Effects on Pilot Performance and Dynamic Response

  • Author

    Sadoff, Melvin ; Dolkas, Constantine B.

  • Author_Institution
    The Ames Research Center, National Aeronautics and Space Administration, Moffett Field, Calif.
  • Issue
    2
  • fYear
    1967
  • fDate
    6/1/1967 12:00:00 AM
  • Firstpage
    103
  • Lastpage
    112
  • Abstract
    Several brief studies were conducted to assess the effects of a wide range of acceleration environments, varying from zero gravity to high sustained accelerations, on pilot performance and dynamic response. The results indicated that the control performance decrements observed at high sustained accelerations were attributable to decreased pilot gains and corresponding reductions in open-loop system crossover frequency. Limited results for extreme vibratory accelerations suggested that performance deterioration was associated with a reduction in pilot lead equalization (and a corresponding reduction in open-loop crossover). Under short-term weightless conditions, performance in a simulated control task was appreciably poorer than under comparable 1 g conditions for one of two sets of simulated vehicle dynamics investigated. The reason was attributed primarily to increased pilot excitation of the vehicle´s lightly damped short-period mode. Soviet data, available from Voskhod flights, indicated that cosmonauts did not perform as well in a simulated control system as during ground training sessions.
  • Keywords
    Acceleration; Aerospace simulation; Control systems; Frequency; Gravity; Open loop systems; Performance gain; Stress; Vehicle dynamics; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Human Factors in Electronics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0096-249X
  • Type

    jour

  • DOI
    10.1109/THFE.1967.233627
  • Filename
    1698249