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Cites:

Information Journal Paper

Title

Vibrational Response of the Pilot Biodynamic Models in Various Flight Maneuver

Pages

  44-56

Abstract

 In this paper, the Vibrational response of the pilot biodynamic models in various flight Maneuvers is investigated. In this regard, the common discrete models, i. e. four degrees of freedom and the seven degrees of freedom, are used. The dynamic model and equations of the motion are derived based on Newton method and they are solved numerically by Runge-Kutta method in Matlab software. The validation of the proposed models is performed by comparing with results of the previously published related works. The variation of the Acceleration g in the various flight test that comprises seven common training Maneuvers, are applied to the above mentioned models. The Transmissibility of the seat to each of the Pilot body components are used as a criterion to do the analysis. The results of the three models studied in different Maneuvers show that the greatest contribution of Transmissibility is in the torso region (up and down) and then in the pelvis region. Also, based on the amount of Transmissibility and maximum Acceleration g in various Maneuvers, the effect of acceleration rate on Transmissibility and pilot comfort is more than the maximum acceleration in each Maneuver.

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  • Cite

    APA: Copy

    Mohamad Khanlo, Heshmatalah, & TAGHIZADEH, MOHAMAD REZA. (2019). Vibrational Response of the Pilot Biodynamic Models in Various Flight Maneuver. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 21(1 ), 44-56. SID. https://sid.ir/paper/371415/en

    Vancouver: Copy

    Mohamad Khanlo Heshmatalah, TAGHIZADEH MOHAMAD REZA. Vibrational Response of the Pilot Biodynamic Models in Various Flight Maneuver. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2019;21(1 ):44-56. Available from: https://sid.ir/paper/371415/en

    IEEE: Copy

    Heshmatalah Mohamad Khanlo, and MOHAMAD REZA TAGHIZADEH, “Vibrational Response of the Pilot Biodynamic Models in Various Flight Maneuver,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 21, no. 1 , pp. 44–56, 2019, [Online]. Available: https://sid.ir/paper/371415/en

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