EXPERIMENTAL CHECKING OF GAS-DYNAMIC METHOD OF UAV LANDING

Authors

  • N. F. Tupitsin National Aviation University, Kyiv
  • H. O. Massalova National Aviation University, Kyiv

DOI:

https://doi.org/10.18372/1990-5548.57.13245

Keywords:

Experimental gas-dynamic system, artificial airstream, fan propeller, mechanical belt drive

Abstract

In the paper construction of the experimental gas-dynamic stand for checking of the gas-dynamic method of unmanned aerial vehicle landing is developed. Characteristics of this stand were calculated and choose. Series of experiments for given model of unmanned aerial vehicle were conducted. Experiments reveal that at braking of unmanned aerial vehicle into artificial airstream on its motion act next main factors: 1) the angle of attack; 2) uniformity, velocity, and the artificial airstream motion direction. Moreover, obtained results allow more carefully ground requirements to equipment for implement new experiments.

Author Biographies

N. F. Tupitsin, National Aviation University, Kyiv

Aviation Computer-Integrated Complexes Department

Candidate of Science. (Engineering). Associate Professor

H. O. Massalova, National Aviation University, Kyiv

Aviation Computer-Integrated Complexes Department

Master

References

N. F. Тupitsin and A. V. Bondarchuk, ”Calculation of the characteristics of gas-dynamic landing gear,” Electronic and control systems. no. 2(28), pp. 161–164, 2011.

N. F. Тupitsin and V. S. Yatskivskiy, ”Gas-dynamic method for taking off aircraft's,” Electronic and control systems. no. 1(27), pp. 122–127, 2011.

N. F.Tupitsin, S. O. Malakhov, and Y. O. Krymov, “Calculation of the gas-dynamic complex sizes,” Electronic and control systems. no. 1(55), pp. 87–93, 2018.

State Standard SU 10616-90 (Standard CMEA 4483-84) Radial and axial fans. Dimensions and parameters. Validity from 01.01.91 to 01.01.2001.

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Issue

Vol. 3 No. 57 (2018)

Section

TRANSPORT SYSTEMS

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