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Case Study of the Psychophysical State of Student-Operators During UAVO Training, Based on Heart Rate Parameter. JOURNAL OF KONBIN 2022. [DOI: 10.2478/jok-2022-0033] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Journal Information] [Subscribe] [Scholar Register] [Indexed: 11/21/2022] Open
Abstract
Abstract
This article focuses on the human factor in UAV operations. In the manuscript, research on the psychophysical state of student-operators under the license of UAVO VLOS <4 kg. For the analysis of the psychophysical state, the pulse parameter was used, which is one of the values that describe the work of the cardiovascular system and is one for the objective methods of assessing the psychophysical state of a human being. The data collected were analyzed using the STATISTICA software. The article focuses on the above aspect and analyzes the psychophysical state of the student-operator during flight training. The obtained results were also related to research on similar topics in the chapter discussion section.
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Influence of the Bird Model Shape on the Results of Numerical Analyses of Bird Models Impact Against a Rigid Plate. JOURNAL OF KONBIN 2022. [DOI: 10.2478/jok-2022-0024] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Journal Information] [Subscribe] [Scholar Register] [Indexed: 11/20/2022] Open
Abstract
Abstract
This paper presents results of numerical analyses of different bird models impacting a rigid plate. The results of the study were compared with findings derived from experimental research. The experimental studies were conducted using a dedicated gas gun kit. A gelatine projectile was used as a bird model, giving it a speed of 116 m/s. For the purpose of the numerical investigations, the authors used the LS-DYNA software package. It is a computational code for the analysis of fast-variable phenomena using different methods, such as Lagrange, Arbitrary Lagrange-Euler (ALE), Smoothed Particle Hydrodynamics (SPH). Three cylindrical bird models with different endings were developed using the SPH method. The shape of the end of the bird model was found to exert a significant effect on the Hugoniot pressure values. However, it does not affect the maximum value of the impact force. The differences only occurred at the initial moment of impact, which was related with the area of contact between the model end and the target.
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